Flight Standardization Board (FSB) Report GIV-x, G-V ... - Code7700

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/12REVISION RECORDRevision No. Section Page #s DateOriginal All All 7/21/971 1.2, 1.4 5 3/26/021 1.7 6 3/26/021 1.9.1, 2.1 7 3/26/021 6.5.2, 7.1, 7.3 9 3/26/021 9.2, 9.3 10 3/26/021 13.1 12 3/26/021 14.1 12 3/26/021 Appendix 3 17 3/26/021 Appendix 4 18-34 3/26/021 Appendix 5 35-36 3/26/021 Appendix 6 37-38 3/26/022 Appendix 6 37-38 6/03/023 All All 6/17/034 Highlights 6 9/29/044 1.1-1.5 7-8 9/29/044 1.7 9-10 9/29/044 1.9.3 11 9/29/044 2 11-12 9/29/044 3 12-14 9/29/044 4 14 9/29/044 5.1, 5.4 14 9/29/044 6.1, 6.4, 6.5 15-16 9/29/044 7.1 16 9/29/044 8.1 17 9/29/044 9.1 17-18 9/29/044 9.2 – 9.3 18 9/29/044 14.1 20 9/29/044 MDR Table 22 9/29/044 Appendix 2 24-50 9/29/044 Appendix 6 102 9/29/044 Appendix 7 104 9/29/044 Appendix 8 105-139 9/29/045 Highlights 7 05/05/085 1.1, 1.3 9 05/05/081.7 11, 12 05/05/085 1.9.2, 1.9.3 13 05/05/085 1.9.6, 1.9.7, 1.9.8 14 05/05/085 1.9.9, 1.9.10, 2.1 15 05/05/085 9.3 22 05/05/085 ODR Tables 37-38, 42-43, 45, 48-50, 53 05/05/085 Appendix 3 54, 55 05/05/085 Appendix 4 64 05/05/08

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/125 Appendix 5 71, 79, 97 05/05/085 Appendix 6 104 05/05/085 Appendix 7 105-106 05/05/08Appendix 8 107, 112, 135 05/05/085 Appendix 9 142 05/05/08Appendix 10 143 05/05/085 Appendix 11 144 05/05/086 Contents 4-5 10/14/096 Revision Record 6-7 10/14/096 Highlights 8 10/14/096 1.7 12 10/14/096 1.9.2 13 10/14/096 1.9.11, 1.9.12 15 10/14/096 Appendix 3 54 10/14/096 Appendix 6 104-105 10/14/096 Appendix 9 143 10/14/096 Appendix 10 144 10/14/096 Appendix 12 146-147 10/14/097 Contents 5 11/01/117 Revision Record 7 11/01/117 Highlights 8 11/01/117 1.7 12 11/01/117 1.9.8 14 11/01/117 1.9.13 15 11/01/117 Appendix 6 104 11/01/117 Appendix 7 106 11/01/117 Appendix 13 148 11/01/118 Contents 5 09/01/128 Revision Record 7 09/01/128 Highlights 8 09/01/128 1.9.14 16 09/01/128 Appendix 14 150 09/01/12

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/12HIGHLIGHTS OF REVISION 8 CHANGESThe primary purpose of this revision is to document the FSB evaluation of, and the pilottraining/checking/currency requirements for, the Display Unit DU-885 modification to the G-V.This modification includes: 1) replacement of six Honeywell DU-880 cathode ray tubes (CRT)with six Honeywell Primus Elite Display Unit (DU)-885 liquid crystal displays (LCD), 2)installation of two cursor control devices (CCD), and 3) new associated functions. This newinformation can be found in Section 1.9, “Background”, and in “Appendix 14”.

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/12MANAGEMENT COORDINATION SHEET/s/ 4/20/2012Eugene F. HuettnerDate:Manager, LGB AEGLong Beach Aircraft Evaluation Group/s/ 4/19/2012Peter NeffDate:Assistant Manager, LGB AEGLong Beach Aircraft Evaluation GroupLeslie SmithManager, AFS-200Air Transportation Division/s/ Robert Davis for 7/11/2012Date:/s/ 5/9/2012Mel CintronDate:Manager, AFS-800General Aviation and Commercial Division

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/12PURPOSE AND APPLICABILITY1.1 The Gulfstream GIV-X, G-V, and GV-SP are listed on FAA Type Certificate DataSheet A12EA, and are hereafter referred to as the “GIV-X”, “GV”, and “GV-SP”.The GIV-X may be modified by Gulfstream Aerospace Corp. (GAC) throughAircraft Service Changes (ASC) to be identified as either a “G450” (ASC 005) or a“G350” (ASC 004). The G450 ASC is simply a change of the aircraft data plate.The G350 ASC changes the data plate, reduces the amount of fuel the aircraft willcarry, and makes the VGS (HUD) and EVS optional equipment. The GV-SP maybe modified by GAC through ASCs to be identified as either a “G550” (ASC 011)or a “G500” (ASC 010). The G550 ASC is simply a change of the aircraft dataplate. The G500 ASC changes the data plate and reduces the amount of fuel theaircraft will carry, and makes the VGS (HUD) and EVS optional equipment.1.2 The primary purpose of this report is to specify FAA master training, checking, andcurrency requirements applicable to crews operating GIV-X, G-V, and GV-SPmodel airplanes. The GV-SP is a variant of the G-V. Major changes from the GV tothe GV-SP are the addition of a Honeywell Primus Epic avionics suite, whichconsists of 4 multi-function 14-inch Flat Panel LCD units, 2 cockpit side mountedCursor Control Devices (CCD), triple MC-850 Multi-Function Control DisplayUnits (MCDU), main entry door relocation approximately 2 feet forward, additional7 th cabin window, new cockpit observer’s seat, drag reduction modifications on theairframe, increased engine thrust, and a 500 pound increase in maximum ramp andtakeoff weights.1.3 The GIV-X is essentially a G-IV airframe with a GV-SP cockpit. It has aHoneywell Primus Epic avionics suite, which consists of 4 multi-function 14-inchFlat Panel LCD units, 2 cockpit side mounted Cursor Control Devices (CCD), tripleMCU-850 Multi-Function Control Display Units (MCDU), Visual GuidanceSystem (VGS), Enhanced Vision System (EVS), Tay 611-8C FADEC engines, aHoneywell 36-150 APU, a cockpit observer’s seat, and drag reductionmodifications on the airframe. The flight control hydraulic boost ratios have beenmodified to replicate the handling characteristics of the GV and GV-SP.1.4 This report will aid 14 CFR part 135 Operators, FAA Principal OperationsInspectors (POIs), and 14 CFR part 142 training centers and their FAA TrainingCenter Program Managers (TCPMs) in the development and approval of 14 CFRpart 135 and 142 training programs. Provisions of this report are effective untilamended, superseded, or withdrawn by subsequent FSB determinations.

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/121.5 This report also addresses certain issues regarding the operation of the GIV-X,G-V, and GV-SP other than under 14 CFR part 135. Provisions of the reportinclude:1.5.1 Defining pilot "type rating",1.5.2 Description of "Master Common Requirements" (MCRs),1.5.3 Description of "Master Differences Requirements" (MDR's) for crewsrequiring differences qualification for mixed-fleet-flying or transition,1.5.4 Examples of acceptable "Operator Difference Requirement (ODR)" Tables,1.5.5 Description of an acceptable training program, special emphasis items, andtraining device characteristics when necessary to establish compliance withpertinent Master Differences Requirements (MDRs),1.5.6 Setting checking and currency standards, including specification of thosechecks that must be administered by FAA or operators, and1.5.7 A listing of regulatory compliance status (compliance checklist) for 14 CFRparts 91 and 135, Advisory Circulars, and other operationally related criteriathat was reviewed and evaluated by the Aircraft Evaluation Group (AEG) orFlight Standardization Board (FSB).

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/121.6 This report also provides:1.6.1 Minimum pilot training, checking and currency requirement that must beapplied by: FAA field offices (i.e. MCRs, MDRs, ODRs, etc.), AviationSafety Inspectors, 14 CFR part 135 Air Carrier Check Airmen andInstructors, Airline Transport Pilots instructing in air transportation service,Certificated Flight Instructors, Certificated Ground Instructors, DesignatedPilot Examiners, Pilot Proficiency Examiners, and Training CenterEvaluators.1.6.2 Information which is advisory in nature, but may be mandatory forparticular operators if the designated configurations apply and if approvedfor that operator (i.e. MDR footnotes and acceptable ODR Tables).1.6.3 Information which is used to facilitate FAA review of an airplane typeproposed for use by an operator.Various sections of this report are qualified as to whether compliance (considering the provisionsof FAA Advisory Circular 120-53) is required or is advisory in nature.1.7 Relevant acronyms are defined as follows:ACACOAFMAPASCCCDCHDODCEDMEECEFBEFISEFVSEGPWSEICASEVSEVS IIFADECFGSFMAFMSFSBAdvisory CircularAircraft Certification OfficeAirplane Flight ManualAutopilotAircraft Service ChangeCursor Control DeviceCertificate Holding District OfficeDisplay ControllerEmergency Descent ManeuverEmergency Evacuation CrewmemberElectronic Flight BagElectronic Flight Instrument SystemEnhanced Flight Vision SystemEnhanced Ground Proximity Warning SystemEngine Indicating and Crew Alerting SystemEnhanced Vision SystemEnhanced Vision System (Second Generation EVS)Full Authority Digital Engine ControlFlight Guidance SystemFlight Mode AnnunciatorFlight Management SystemFlight Standardization Board

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/12FTD Flight Training DeviceGAC Gulfstream Aerospace CorporationHUD Honeywell Head Up Guidance Display (Model 2020).HUD II Rockwell-Collins Head Up Guidance System (HGS Model 6250)I-NAV Integrated Navigation DisplayIRS Inertial Reference SystemMMELMaster Minimum Equipment ListMCDU Multi-Function Control Display UnitsMCR Master Common RequirementsMDR Master Differences RequirementsND Navigation DisplayODR Operator Differences RequirementsPFD Primary Flight DisplayPOI Principal Operations InspectorQRH Quick Reference HandbookRAAS Runway Awareness Advisory SystemRFMU Radio Frequency Management UnitRNP SAAR Required Navigation Performance –Special Aircraft and Aircrew Authorization Required.SV PFD Synthetic Vision Primary Flight DisplayTAWS Terrain Awareness and Warning SystemTCAS Traffic Alert and Collision Avoidance SystemTCE Training Center EvaluatorTCPM Training Center Program ManagerVGS Visual Guidance SystemVNAV Vertical NavigationWOW Weight on Wheels1.8 TerminologyThe term "must" is used in this report, even though it is recognized that this report,and the Advisory Circular AC 120-53 on which it is based, provides one acceptablemeans, but not necessarily the only means, of compliance with 14 CFR part 135Subpart H requirements. The term "must" acknowledges the need for operators tofully comply with the FSB report provisions if AC-120-53 is to be used by theoperator as its means of complying with 14 CFR part 135, Subpart H.1.9 Background1.9.1 In August-September, 1996 and January-February 1997, the G-V FlightStandardization Board (FSB) received a G-V initial pilot ground schoolutilizing the training facilities of Flight Safety International and Gulfstreamlocated in Savannah, GA. Training was conducted in classrooms, and anIntegration Test Facility (ITF). The ITF was not designed as a trainingdevice. It was an engineering mockup of the G-V cockpit used to validate

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/12aircraft hardware interface. In addition a newly manufactured simulator,which was under development, but not qualified by the FAA, was utilized.The FSB then received aircraft training in theG-V (N505GV) in Savannah, GA. It then conducted AC 120-53 test T5,which is essentially an evaluation of the maneuvers listed in the FAA ATPPractical Test Standards (PTS) for a pilot type rating. It also participated infour Function and Reliability Test flights to validate proposed AFM normal,abnormal, and emergency procedures.1.9.2 In September 1997 the G-V FSB participated in an in-flight evaluation ofthe Honeywell Head Up Guidance Display (Model 2020), during itsdevelopment, using Gulfstream’s G-V aircraft. In November 1997, the FSBconducted certification flight tests, along with the Los Angeles AircraftCertification Office (ACO), in Gulfstream's G-V aircraft in Savannah, GA.Flight testing consisted of approximately 30 HUD approaches at 3 differentairports, using CAT 1 and CAT II procedures, during day, night, VisualMeteorological Conditions (VMC) and Instrument MeteorologicalConditions (IMC). The FSB also evaluated Gulfstream’s proposed G-VAirplane Flight Manual (AFM) Supplement for HUD Operations andGulfstream's proposed HUD CAT II appendix to the G-V AFM Supplementfor Category II Operations. The FSB found the HUD operationally suitablefor all phases of flight and for U.S. CAT I and CAT II operations. HUDTraining, checking and currency requirements are listed in Appendix 6.1.9.3 From February 1998 to August 2001 the G-V FSB Chairman participatedwith the FAA Los Angeles Aircraft Certification Office in EVSdevelopment, proof of concept, and certification flight tests. Those flightsincluded over 50 EVS approaches conducted at approximately 15 differentairports during day, night, Visual Meteorological Conditions (VMC) andInstrument Meteorological Conditions (IMC). Gulfstream’s G-V EVSAirplane Flight Manual Supplement was evaluated and found acceptableduring the certification flight tests. In September 2001 two G-V FSBmembers received EVS ground school, simulator, and airplane training fromGulfstream Aerospace Corp. (GAC), in Savannah, GA. It was found to beoperationally suitable. EVS meets the requirements of EFVS (EnhancedFlight Vision System) as defined in FAR 91.175. EVS Training, checkingand currency requirements are listed in Appendix 7.1.9.4 In January-February, 2003, the GV-SP Flight Standardization Board (FSB)conducted an evaluation of the GV-SP in accordance with the processoutlined in AC 120-53. One group of 3 pilots received a GV-SP initial pilotground school utilizing the training facilities of Flight Safety Internationaland a GV-SP aircraft owned by Gulfstream, both located in Savannah, GA.Another group of 4 previously qualified G-V pilots received G-V refreshertraining. One group then performed handling qualities comparison flighttestingin the GV-SP. The test was successfully passed. Each group of pilots

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/12checking and currency requirements are listed in Appendix 101.9.9 In April and November 2007 the FSB conducted flight evaluations ofPlaneView Avionics Software version “E” in a GIV-X. This software addedSynthetic Vision Primary Flight Display (SV PFD). It, as well as theassociated AFM change, was found to be operationally suitable. Trainingchecking and currency requirements are listed in Appendix 11.1.9.10 In November and December 2007 the FSB conducted an evaluation of EVSII. It was found to be functionally equivalent to EVS. All training, checkingand currency requirements for EVS apply to EVS II, and are listed inAppendix 7.1.9.11 In June 2009 the FSB conducted flight evaluations of PlaneView AvionicsSoftware version “F” in a GIV-X. This software added map functionalityand 3 other options for operators to purchase: 1) Enhanced Navigation 2)Enhanced SV PFD, and 3) XM Weather. Software version “F”, as well asthe associated AFM change, was found to be operationally suitable.Training checking and currency requirements are listed in Appendix 12.1.9.12 In June 2009 the FSB conducted flight evaluations of HUD II which is theRockwell-Collins Head Up Guidance System (HGS Model 6250).It was found to be functionally equivalent to HUD which is the HoneywellHead Up Display (Model 2020). All training, checking and currencyrequirements for HUD apply to HUD II, and are listed in Appendix 6.1.9.13 In April 2011 the FSB conducted flight evaluations of PlaneView AvionicsSoftware version “G” in a GIV-X. This software added the followingfeatures:Early Missed Approach activation with the MCDU and TO/GA,LPV Approach capture from above, Maximum descent angle improvements,Datalink recording on the Cockpit Voice Recorder, Path-based TCASGuidance on the SV PFD, listing of multiple localizer approaches to thesame runway, and update to Fuel Tank Temperature CAS message andrelated Synoptics for the GIV-X only. Software version “G”, as well as theassociated AFM change, was found to be operationally suitable. Trainingchecking and currency requirements are listed in Appendix 13.1.9.14 In November 2011 the FSB conducted flight evaluations of the Display UnitDU-885 modification to the G-V. This modification includes: 1)replacement of six Honeywell DU-880 cathode ray tubes (CRT) with sixHoneywell Primus Elite Display Unit (DU)-885 liquid crystal displays(LCD), 2) installation of two cursor control devices (CCD), and 3) newassociated functions. The functions include: charts, maps, video, databaseand DU maintenance. The LCDs, CCDs and associated functions, as well as

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/12the associated AFM change, was found to be operationally suitable.Training checking and currency requirements are listed in Appendix 14.2 PILOT "TYPE RATING" REQUIREMENTS2.1 In accordance with the provisions of 14 CFR parts 1, 61, and 135, the same pilottype rating is assigned to the GIV-X (G350/G450), G-V, and theGV-SP (G500/G550), and is designated “G-V”.2.2 The Gulfstream GIV-X, G-V, and GV-SP have not been issued a new TypeCertificate (TC) Data Sheet. They were all added to the existing G-II throughG-IV TC Data Sheet issued by the Atlanta Aircraft Certification Office (ACO). TheGIV-X, G-V, and GV-SP aircraft however, are not considered variants orderivatives of the Gulfstream G-IV aircraft for pilot type rating purposes. The FSBdid not conduct a comparison between the G-IV and any other model aircraft forpilot type rating purposes; therefore, no credit may be given between the G-IV andany other model aircraft for training, checking, or currency.3 “MASTER COMMON REQUIREMENTS" (MCRs)3.1 Master Common Requirement for all GIV-X, G-V and GV-SP airplanes:3.1.2 Normal ‘Final’ Landing Flap Setting:The normal ‘final’ landing flap is 39 degrees for the GIV-X, G-V, and theGV-SP.3.1.3 Automatic Flight Control System (AFCS):The AFCS pilot/machine interface is the same for the GIV-X, G-V and GV-SP.3.1.4 Electronic Flight Instrument System (EFIS):The EFIS/pilot interface is essentially the same for the GIV-X, GV andGV-SP aircraft. All three airplanes use the EFIS display controller as theinitial interface.3.1.5 Engine Indicating and Crew Alerting System (EICAS):The EICAS philosophy is the same in the GV and the GV-SP aircraft. Onlyminor changes to crew alerting messages and the “look and feel” of the

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/12synoptic and system pages have been made.3.1.6 Navigation and Communication:All three aircraft share the same navigation and communication equipment.Pilot operation of the equipment is the same for the GIV-X, GV, and GV-SPaircraft.3.1.7 Primary and Secondary Flight Controls:Pilot operation of the primary and secondary flight controls is the same forthe GIV-X, G-V and the GV-SP under normal conditions.3.1.8 Procedure Knowledge:Takeoff Climb and Descent Profiles:The takeoff, climb, and descent Profiles for the GIV-X, G-V and GV-SP areidentical.3.1.9 Landing Minima Category (FAR 97.3)The following straight-in approach minima (based on Maximum Landing Weight(MLW) and 1.3 times Vso) for the GIV-X, G-V, and the GV-SP are as follows:Aircraft Landing Flap CategoryGIV-X 39 degrees DG-V 39 degrees CGV-SP 39 degrees CFor the purpose of determining circling approach minima, the minimums are basedon the highest speed used during a circling maneuver. As depicted in the tablebelow, the highest speed to be flown (speed category) during the circling maneuvermust be used to determine the appropriate minimums. This will ensure that theaircraft will remain within the designated maneuver area and assure obstacleclearance.Speed CategoryVisibility in Statute MilesLess than 91 Kts.1 Mile91 to 120 Kts. 1 Mile121 to 140 Kts. 1 ½ Miles141 to 165 Kts. 2 Miles

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/12Above 165 Kts.3 Miles3.1.10 Approach Profiles and Speed:The approach profiles are the same for the GIV-X, G-V, and the GV-SP.Approach speeds are dependent upon aircraft weight. All critical speeds areautomatically presented to the pilot in a standardized manner for the GIV-X, G-V,and the GV-SP aircraft.3.1.11 Abnormal & Emergency Procedures:Abnormal and emergency procedures are presented in Quick Reference Handbooksof an identical format for all three aircraft. Although some individual steps maydiffer or use different acronyms, these steps are carried out under the guidance ofthe handbook in a logical decision-making manner.There are no memory items in the AFM for the GIV-X, GV, or the GV-SP.4 “MASTER DIFFERENCE REQUIREMENTS" (MDRs)4.1 Master Difference Requirements (MDRs) for the GIV-X, G-V, and GV-SP areshown in Appendix 1. Appendix 1 provisions apply when differences betweenvariants exist which affect crew knowledge, skills, or abilities related to flightsafety (e.g. Level A or greater differences).5 ACCEPTABLE "OPERATOR DIFFERENCE REQUIREMENTS" (ODRs)TABLES5.1 Operator Difference Requirement (ODR) tables are used to show an operator'scompliance method. ODR tables for operators conducting mixed fleet operations,using the GIV-X, G-V, and GV-SP are shown in Appendix 2. The ODR tablesrepresent an acceptable means to comply with MDR provisions based on thosedifferences and compliance methods shown. The tables do not necessarilyrepresent the only acceptable means of compliance for operators with airplaneshaving other differences, where compliance methods (e.g., devices, simulators, etc.)are different. For operators flying the GIV-X, G-V, and the GV-SP the ODR tablesin Appendix 2 have been found acceptable, and therefore, may be approved by aPOI for a particular operator.5.2 Operator Preparation of ODR Tables:Operators seeking different means of compliance must prepare and seek FAA

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/12approval from their POI of specific ODR tables pertinent to their fleet. The POIshould coordinate this with the FSB Chairman and AFS-200.5.3 ODR Table Coordination:New ODR tables proposed by operators should be coordinated with the FSB priorto FAA approval and implementation. Through this coordination, the FSB canensure consistent treatment of variants between various operators’ ODR tables andcompatibility of the MDR table with MDR provisions.5.4 ODR Table Distribution:Originally approved ODR tables are retained by the operator. Copies of approvedGIV-X, G-V, and GV-SP tables are retained by the Certificate Management Office(CMO). Copies of all approved ODR tables should be forwarded to the FSBChairman, Long Beach Aircraft Evaluation Group (AEG).6 FSB SPECIFICATIONS FOR TRAINING6.1 General:6.1.1 The provisions of this training section apply to the GIV-X, G-V, andGV-SP, to programs for airmen having previous experience in 14 CFR part91 or 14 CFR part 135 air carrier operations, and multi-engine turbojet orturboprop aircraft. Additional requirements, as determined by theoperator’s POI, the FSB, and AFS-200, may be necessary for airmen nothaving such experience. Appendix 3 contains a list of special emphasisitems to be included in an approved training program.6.2 Initial, Transition and Upgrade Training:6.2.1 Pilot Initial, Transition, and Upgrade Ground Training is accomplished inaccordance with 14 CFR part 135.343, 135.345, and SFAR 14 CFR SFAR58, Advanced Qualification Program (AQP).6.2.2 Pilot Initial, Transition, and Upgrade Flight Training is accomplished inaccordance with 14 CFR part 135.347.6.3 Recurrent Training:6.3.1 Recurrent Ground Training is accomplished in accordance with 14 CFRpart 135.351 and SFAR part 58 (AQP).6.3.2 Recurrent Flight Training is accomplished in accordance with 14 CFR part135.351 and requires that the pilot be proficient in those maneuvers and

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/12procedures that are required for the original issuance of the pilot certificate.6.4 Differences Training:Differences training is accomplished in accordance with 14 CFR part 135.347.When any combination of the GIV-X, G-V and GV-SP are flown, appropriateinstruction in design and systems differences will be required for both airplanes,consistent with MDR provisions listed in Appendix 1.6.5 Other Training:6.5.1 Flight Attendant Training is accomplished in accordance with 14 CFR part135.341 if a flight attendant is utilized. The GIV-X, G-V, and GV-SP havea maximum seating capacity of 19 seats and therefore, do not require aFlight Attendant.6.5.2 Aircraft Dispatcher Training, Flight Engineer Training, and FlightNavigator Training are not applicable.6.5.3 Emergency Evacuation Crewmember (EEC) Training – During the GV-SPcertification process Gulfstream asked the FAA to make an equivalent safetyfinding on the overwing exits because they did not meet current FAAcertification standards. Gulfstream requested, and the FAA accepted, thatanytime more than 9 passengers are carried, an additional crewmembertrained in Emergency Evacuation for the Gulfstream elliptical exits berequired onboard. The FAA found that this provides an equivalent level ofsafety to overwing emergency exits that would meet current FAAcertification standards. Therefore, the GV-SP will require an EmergencyEvacuation Crewmember on the aircraft any time more than 9 passengers arecarried. The specific training that EEC is required to undergo is specified inGulfstream Operating Manual Supplements numbersG550-OMS-1 for the G550 and G500-OMS-1 for the G500.The GIV-X does not require an EEC. The FAA certified the GIV-Xoverwing exits at an earlier certification rule amendment level, based on theG-IV certification.7 FSB SPECIFICATIONS FOR CHECKING7.1 General7.1.1 The provisions of this checking section apply to the GIV-X, G-V, andGV-SP. Testing, Checking and Evaluations specified by 14 CFR parts61.57, 61.58, 61.63, 61.67, 61.157, 61.159, 135.293, 135.297, SFAR58, and FAA Practical Test Standards (PTS) apply.

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/127.1.2 The following areas of emphasis must be demonstrated during checking:a. Proficiency in manual and automatic (including FMS) flight in normal,abnormal, and emergency situations must be demonstrated at eachproficiency/competency check by all crewmembers.b. The use of manual modes to operate systems such as electrical, hydraulic,pressurization, environmental, etc. and emergency equipment must bedemonstrated at each proficiency/competency check by all crewmembers.c. Demonstration of a no flap approach and landing during a pilot type rating or 14CFR part 135 check is required per the Airline Transport Pilot and/or TypeRating Practical Test Standards - FAA-S-8081 Area of Operation VI, Task F. Inaccordance with Order 8400.10, when the flight demonstration is conducted inan airplane, verses a simulator, touchdown from a no flap approach is notrequired. The approach should be flown to the point where the inspector orexaminer can determine whether a touchdown at an acceptable point on therunway and a safe landing to a full-stop could be made.7.2 Type Ratings:Type rating Practical Tests are administered in accordance with 14 CFR parts61.63, 61.157, 61.159, SFAR 58 and the Practical Test Standards.7.3 Competency/Proficiency Checks and Evaluations:Competency/Proficiency checks and evaluations are administered in accordancewith 14 CFR parts 61.58, SFAR 58, 135.293, and 135.297.8 FSB SPECIFICATIONS FOR CURRENCY8.1 Currency (Recency of Experience):Currency is considered to be common for the GIV-X, G-V and GV-SP. Separatetracking of currency for the GIV-X, G-V and GV-SP is not necessary or applicable.Currency will be maintained, or re-established, in accordance with 14 CFR parts61.57, 61.58, 135.247 and/or 135.351.9 AIRCRAFT REGULATORY COMPLIANCE CHECKLIST9.1 Operating Rules Compliance Checklist:The Operating Rules Compliance Checklists are provided as an aid to FAACertificate Holding District Offices (CHDOs) to identify those specific rules orpolicies for which compliance has already been demonstrated to the FAA for aparticular aircraft. The checklist also notes rules or policies, which must bedemonstrated to CHDOs by the operator. Not all rules or policies are necessarily

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/12listed or addressed. It continues to be the responsibility of the CHDO to reviewcompliance with pertinent rules or policies not already satisfactorily addressed inthe Operating Rules Compliance Checklist, prior to 14 CFR part 135 approval foran operator to use the GIV-X, G-V, or GV-SP in service. The Operating RulesCompliance Checklist in Appendix 4 reflects the status of the first production G-Vaircraft flown by the FSB on February 6, 1997. The aircraft serial number was 505and bore U.S. Registration number N505GV.The Operating Rules Compliance Checklist in Appendix 5 reflects the status of aGV-SP flight test aircraft flown by the FSB on February 18, 2003. The aircraftserial number was 5001 and bore U.S. Registration number N5SP.The Operating Rules Compliance Checklist in Appendix 8 reflects the status of aGIV-X flight test aircraft flown by the FSB on May 3-4, 2004. The aircraft serialnumber was 4003 and bore U.S. Registration number N403SR.9.2 Aircraft Proving Tests:Proving tests in accordance with 14 CFR part 135.145 and FAA Order 8400.10,Vol. 3, Chapter 9, are appropriate when the GIV-X, G-V, or GV-SP is new to aparticular operator. When an operator is currently operating either the G-IV, GIV-X, G-V or GV-SP, and the operator introduces the G-IV, GIV-X, G-V, or GV-SPinto the same operations, proving tests are not required. The G-IV,GIV-X, G-V, and GV-SP have similar type powerplants, and alterations betweenthe G-IV, GIV-X, G-V, and GV-SP do not materially affect flight characteristics forpurposes of proving tests.9.3 Forward Observer’s Seat:14 CFR part 135.75(b) requires that a forward observer’s seat on the flight deck beprovided for use by the Administrator while conducting enroute inspections. It isalso required for conducting airman certification (checkrides).G-V aircraft produced in accordance with Gulfstream V product specification, Rev.C, dated 12/19/96, have a forward observer’s seat installed that the FSB foundoperationally acceptable for conducting cockpit enroute inspections.The FSB evaluated the GIV-X and GV-SP observer seats for compliance with AC120-83 and found them to be operationally acceptable for conducting cockpitenroute inspections.

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/1210 FSB SPECIFICATIONS FOR DEVICES AND SIMULATORS10.1 Device and Simulator Characteristics:10.1.1 Device and simulator characteristics are designated in AC 120-40 and 120-45 (as amended).10.1.2 The acceptability of differences between devices, simulators, and aircraftmust be addressed by the POI.10.2 Device Approval:10.2.1 Requests for device approval should be made to the POI. The POI mayapprove these devices for that operator if their characteristics clearly meet theestablished FAA criteria and have been approved by the National SimulatorProgram (NSP).11 APPLICATION OF FSB REPORT11.1 All relevant parts of this report are applicable to operators on the effective date ofthis report.12 ALTERNATE MEANS OF COMPLIANCE TO THIS REPORT12.1 Approval Level and Criteria12.1.1 The FSB chairman should be consulted by the POI when alternate means ofcompliance, other than those specified in this report, are proposed. Alternatemeans of compliance must be approved by the FAA Air TransportationDivision, AFS-200, Washington Headquarters. If an alternate means ofcompliance is sought, operators will be required to submit a proposedalternate means for approval that provides an equivalent level of safety tothe provisions of AC 120-53 and this FSB report. Analysis, demonstrations,proof of concept testing, differences documentation, and/or other evidencemay be required.12.1.2 In the event that alternate compliance is sought, training program hourreductions, simulator approvals, and device approvals may be significantlylimited and reporting requirements may be increased to ensure an equivalentlevel of training, checking, and currency. FAA will generally not considerrelief through alternate compliance means unless sufficient lead-time hasbeen planned by an operator to allow for any necessary testing andevaluation.

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/1213 MISCELLANEOUSReserved14 SUPPLEMENTAL BOARD REPORT - PART II14.1 Part II of the FSB report contains historical development information used todevelop Part I. This information is kept on file at the Long Beach AircraftEvaluation Group, (LGB AEG), 3960 Paramount Boulevard, Suite 100, Lakewood,CA 90712-4137.Documents kept on file are as follows:GIV-X / G-V / GV-SP Master Minimum Equipment ListGIV-X / G-V / GV-SP Operational ManualsGIV-X / G-V / GV-SP Training syllabus of FSB membersGIV-X / G-V / GV-SP Original Aircraft Flight ManualGIV-X / G-V / GV-SP FAA FSB Order (FSB member list)GIV-X / G-V / GV-SP Operational Issue Papers

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/12Appendix 1 - MDR TABLE

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/12Airplane Type Rating: GVToAirplaneMaster Differences RequirementsFrom AirplaneGV-SP GV GIV-XGIV-X C/B/A C/B/AGVGV-SPC/B/ANOTAPPLICABLENOTAPPLICABLEC/B/ANOTAPPLICABLEC/B/AC/B/A

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/12Appendix 2 - ACCEPTABLE ODR TABLES

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/12Definitions“HO” = Handout“ST” = Slide/tape presentations“TCBI” = Tutorial computer based instruction“SU” = Stand-up Instructors“VT” = Video tapes“ICBI” = Interactive computer based instruction“CSS” = Cockpit system simulators“CPT” = Cockpit procedures trainers“PTT” = Part task trainers“FTD 2-5” = Flight training devices (level 2-5)“FTD 6-7” = Flight training devices (level 6-7)“SIM A-B” = Simulators (level A or B)“SIM C-D” = Simulators (level C or D)“ACFT” = AircraftODRTrainingLevelABCDENOTESAn “X” in an ODR table column indicates thatany of the training methods listed for that levelare acceptable. If a specific instruction methodis specified in an ODR table column, it must beused.“ C* ” in the Checking column of the ODR tablesrequires use of training devices specified in“TRAINING LVL C” column of ODR tableMore ODR Checking and Currency level definitionsmay be found in AC 120.53.

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/12DIFFERENCE AIRCRAFT: GV-SPBASE AIRCRAFT: GIV-XAPPROVED BY(POI)____________________________DESIGNREMARKS20 Aircraft General PerformanceMax T.O. Weight91,000 lbIncrease of 17,100 lb23 Communications Selcal Test and CVRTest switches relocated27 Flight Controls Split flight controls addedFLTCHARPROCCHNGLVLACOMPLIANCE METHODTRAININGLVL LVLB CLVLDCHK / CURRCHKCURRNo No X A ANo Minor X A AYes27 Flight Controls Trailing edge contours(TECs) added to inboard No No X A Atrailing edge of flaps27 Flight Controls No Alternate Flap Switch No Minor X A A27 Flight Controls Standby rudder and nosewheel steering on AUX No Minor X A Apump capability27 Flight Controls Spoiler Control switchadded. Lateral Control Yes Minor X B ASwitch deleted.27 Flight Controls Vortex generators addedto lower horizontalstabilizer surfaces andNo Minor X A Aupper elevator surfaces28 Fuel Heated Fuel ReturnSystemNo Minor X A A29 Hydraulic Power Aux Hydraulic BoostPump addedNo No X A A30 Ice and Rain Pitot Probe Heat Systemchanged.No Minor X A A32 Landing Gear 4 brake wear indicatorpins vs. 2 and WOW No Minor X A Aswitches49 APU Different APU installed.RE220 vs. 36-150 both No Minor X A Asupplied by Honeywell.49 APU Bleeds off takeoffcapability added.No Major X A A70 Powerplant BR710 installed vs.Tay 611-8CNo Minor X A A78 Engine Exhaust Thrust Reverser ManualStow switches (2)installedNo Minor X A AMinorCSSorCPTorPTTorFTD5AA

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/12DIFFERENCE AIRCRAFT: GV-SPBASE AIRCRAFT: GIV-XAPPROVED BY(POI)____________________________DESIGNLimitationsREMARKSMax Takeoff Weightincreased to 91,000 lbfrom 73,900 lb. MaxLanding Weightincreased to 75,300 lbfrom 66,000 lb.Fuel quantity 41,300 lbvs. 29,500 lbAPU and Enginelimitations differences.FLTCHARPROCCHNGLVLACOMPLIANCE METHODTRAININGLVL LVLB CLVLDCHK / CURRCHKCURRNo No X A A

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/12DIFFERENCE AIRCRAFT: GV-SPBASE AIRCRAFT: GIV-XCOMPLIANCE METHODAPPROVED BY(POI)____________________________TRAINING CHK / CURRFLT PROC LVL LVL LVL LVLMANEUVER REMARKSCHK CURRCHAR CHNG A B C DNormal Takeoff Bleeds Off No Minor X A A

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/12DIFFERENCE AIRCRAFT: GV-SPBASE AIRCRAFT: GIV-XAPPROVED BY(POI)____________________________SYSTEMREMARKS23 Communications Selcal and CVR testswitches different testmethodology27 Flight Controls Spoiler Control switchadded. Lateral ControlSwitch deleted.30 Ice and Rain Pitot Probe Heat Systemchanged.49 APU Different APU installed.RE220 vs. 36-150 bothsupplied by Honeywell.49 APU Starter assisted airstartcapability for mainengines49 APU Bleeds off takeoffcapability added70 Powerplant Thrust increased by1,535 lb to 15,385 lbFLTCHARPROCCHNGLVLACOMPLIANCE METHODTRAININGLVL LVLB CLVLDCHK / CURRCHKCURRNo Minor X A AYes Minor X B ANo Minor X A ANo Minor X A ANo Major X A ANo No X A ANo No X A A

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/12DIFFERENCE AIRCRAFT: GIV-XBASE AIRCRAFT: GV-SPAPPROVED BY(POI)____________________________DESIGNREMARKSFLTCHARPROCCHNGLVLACOMPLIANCE METHODTRAININGLVL LVLB CLVLDCHK / CURR20 Aircraft General PerformanceMax T.O. Weight17,100 lb decrease toNo No X A A73,900 lb23 Communications Selcal Test and CVRTest switches relocatedNo Minor X A A27 Flight Controls Alternate Flap Controlswitch addedNo Minor X A A27 Flight Controls No split flight controls Yes Minor X A A27 Flight Controls Trailing Edge Contoursnot installedNo No X A A27 Flight Controls No standby rudder andno nose wheel steeringon AUX pumpYes Minor X A Acapability27 Flight Controls Lateral Control switchadded. Spoiler Control Yes Minor X B ASwitch deleted.27 Flight Controls Vortex generatorsdeleted from lowerhorizontal stabilizer No Minor X A Asurfaces and upperelevator surfaces28 Fuel No Heated Fuel ReturnSystem installedNo Minor X A A29 Hydraulic Power Aux Hydraulic BoostPump deletedNo No X A A30 Ice and Rain Pitot Probe HeatSystem changed.No Minor X A A32 Landing Gear 2 brake wear indicatorpins vs. 4No Minor X A A49 APU Different APU installed.RE220 vs. 36-150 both No Minor X A Asupplied by Honeywell.49 APU No Bleeds Off takeoffcapabilityNo No X A A70 Powerplant Tay 611-8C installedvs. BR710.No Minor X A A78 Engine Exhaust No Manual ThrustReverser Stowswitches installed.No Minor X A ACHKCURR

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/12DIFFERENCE AIRCRAFT: GIV-XBASE AIRCRAFT: GV-SPAPPROVED BY(POI)____________________________DESIGNLimitationsREMARKSMax T.O. Weightdecreased by 17,100 lbto 73,900 lb. Maxlanding weightdecreased to 66,000 lb.Fuel quantity 29,500 lbvs. 41,300 lbAPU and enginelimitations differences.FLTCHARPROCCHNGLVLACOMPLIANCE METHODTRAININGLVL LVLB CLVLDCHK / CURRCHKCURRNo No X A A

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/12DIFFERENCE AIRCRAFT: GIV-XBASE AIRCRAFT: GV-SPAPPROVED BY(POI)____________________________FLT PROCMANEUVER REMARKSCHAR CHNGNone None No NoLVLACOMPLIANCE METHODTRAININGLVL LVLB CLVLDCHK / CURRCHKCURR

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/12DIFFERENCE AIRCRAFT: GIV-XBASE AIRCRAFT: GV-SPAPPROVED BY(POI)____________________________SYSTEMREMARKS23 Communications Selcal and CVR testswitches different testmethodology27 Flight Controls Lateral Control switchadded. Spoiler ControlSwitch deleted.30 Ice and Rain Pitot Probe HeatSystem changed.49 APU Different APU installed.RE220 vs. 36-150 bothsupplied by Honeywell.49 APU No Bleeds Off takeoffcapability70 Powerplant Thrust decreased 1,535lb to 13,850 lbFLTCHARPROCCHNGLVLACOMPLIANCE METHODTRAININGLVL LVLB CLVLDCHK / CURRCHKCURRNo Minor X A AYes Minor X B ANo Minor X A ANo Minor X A ANo Minor X A ANo No X A A

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/12DIFFERENCE AIRCRAFT: GVBASE AIRCRAFT: GIV-XAPPROVED BY(POI)____________________________DESIGNREMARKS20 Aircraft General PerformanceMax T.O. Weight90,500 lbIncrease of 16,600 lb20 Aircraft General Observer seat andlocation changed.21 ECS Outflow valve changed tobutterfly valve.24 Electrical Power Revised Location of PDBcircuit breaker panels27 Flight Controls Split flight controls addedFLTCHARPROCCHNGLVLACOMPLIANCE METHODTRAININGLVL LVLB CLVLDCHK / CURRCHKCURRNo No X A ANo No VT A ANo Minor X A ANo Minor X A AYes27 Flight Controls No Alternate Flap Switch No Minor X A A27 Flight Controls Standby Rudder installedwith nose wheel steeringon the AUX pumpcapability (including AUXYes Minor X A APUMP ground spoilerpressure)27 Flight Controls Spoiler Control switchadded. Lateral Control Yes Minor X B ASwitch deleted.27 Flight Controls Vortex generators addedto lower horizontalstabilizer surfaces andNo Minor X A Aupper elevator surfaces28 Fuel Heated Fuel ReturnSystem addedNo Minor X A A29 Hydraulic Power Aux Hydraulic BoostPump addedNo No X A A30 Ice and Rain Pitot Probe Heat Systemchanged.No Minor X A A32 Landing Gear 4 brake wear indicatorpins vs. 2 and WOW No Minor X A Aswitches49 APU Different APU installedwith capability for APUassisted main engineairstart and differentelectrical loadcapabilities.No Minor X A AMinorCSSorCPTorPTTorFTD5AA

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/12DIFFERENCE AIRCRAFT: GVBASE AIRCRAFT: GIV-XAPPROVED BY(POI)____________________________DESIGNREMARKS52 Doors Main Door moved aft 24inches52 Doors Aft Lav Dump Doorrelocated70 Powerplant BR710 vs. Tay 611-8CInstalled78 Engine Exhaust Thrust Reverser ManualStow Switches (2)installed.LimitationsMax Takeoff Weightincreased to 90,500 lbfrom 73,900 lb.FLTCHARPROCCHNGLVLACOMPLIANCE METHODTRAININGLVL LVLB CLVLDCHK / CURRCHKCURRNo No X A ANo No X A ANo Minor X A ANo Minor X A ANo No X A A

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/12DIFFERENCE AIRCRAFT: GVBASE AIRCRAFT: GIV-XAPPROVED BY(POI)____________________________FLT PROCMANEUVER REMARKSCHAR CHNGNone None No NoLVLACOMPLIANCE METHODTRAININGLVL LVLB CLVLDCHK / CURRCHKCURR

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/12DIFFERENCE AIRCRAFT: GVBASE AIRCRAFT: GIV-XAPPROVED BY(POI)____________________________SYSTEMREMARKSFLTCHARPROCCHNGLVLACOMPLIANCE METHODTRAININGLVL LVLB CLVLDCHK / CURR22 Autoflight TOGA Flight DirectorCommand Bars initiate at12 degrees vs. 8 degreesNo No X A Aon GIV-X.23 Communications New Audio System No No X A A23 Communications Radio Tuning ThroughRFMUNo Yes X A A27 Flight Controls Spoiler Control switchadded. Lateral Control Yes Minor X B ASwitch deleted.30 Ice and Rain Pitot Probe Heat Systemchanged.No Minor X A A31 Indicating /Recording Systems31 Indicating /Recording Systems31 Indicating /Recording Systems31 Indicating /Recording SystemsStandby EngineInstrument on RFMUDAU (Data AcquisitionUnit) and FWC (FaultWarning Computer)replaces MAU (ModularAvionics Unit)Display ControllerElectronic Checklist AutoPop-up Feature enabled No MinorCHKCURRNo Minor X A ANo Minor X A ANo Minor X A A34 Navigation IRS ON/OFF switchesdeleted and replaced with No Minor X A AMSU switches34 Navigation EICAS FMS JoystickPanelNo None X A A34 Navigation 6 Display Units vs. 4Display UnitsNo Minor X B A34 Navigation No CCDs Used inConjunction with DisplaysNo Minor X B A34 Navigation HSI on RFMU No Minor X A A34 Navigation LaserTrack No Minor X B A34 Navigation Standby Flight instrumentshave different design and No Minor X A Alocation49 APU Different APU installedwith capability for APUassisted main engine No Minor X A Aairstart and differentelectrical load capabilities.70 Powerplant Thrust increased by900 lb to 14,750 lbNo No X A AST,TCBIorVTAA

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12DIFFERENCE AIRCRAFT: GIV-XBASE AIRCRAFT: GVAPPROVED BY(POI)____________________________DESIGNREMARKSFLTCHARPROCCHNGLVLACOMPLIANCE METHODTRAININGLVL LVLB CLVLDCHK / CURR20 Aircraft General PerformanceMax T.O. Weight73,900 lbNo No X A ADecrease of 16,600 lb20 Aircraft General Observer seat and locationchanged.No No VT A A21 ECS Outflow valve changed tothrust recovery outflow No Minor X A Avalve.23 Communications Selcal test and CVR testswitches relocatedNo Minor X A A24 Electrical Power Revised Location of PDBcircuit breaker panelsNo Minor X A A27 Flight Controls No Standby Rudderinstalled or nose wheelsteering on the AUX pumpYes Minor X A Acapability27 Flight Controls No split flight controls Yes Minor X A A27 Flight Controls Lateral Control switchadded. Spoiler Control Yes Minor X B ASwitch deleted.27 Flight Controls Vortex generators deletedfrom lower horizontalstabilizer surfaces andNo Minor X A Aupper elevator surfaces27 Flight Controls Alternate Flap SwitchaddedNo Minor X A A28 Fuel No Heated Fuel ReturnSystemNo Minor X A A29 Hydraulic Power No Aux Hydraulic BoostPumpNo No X A A30 Ice and Rain Pitot Probe Heat Systemchanged.No Minor X A A49 APU Different APU installedwith no capability for APUassisted main engine No Minor X A Aairstart and differentelectrical load capabilities.52 Doors Main Door moved forward24 inchesNo No X A A52 Doors Aft Lav Dump DoorrelocatedNo No X A ALimitationsMax Takeoff Weightdecreased to 73,900 lbfrom 90,500 lb.Fuel Quantity 29,500 lb vs.41,300 lbAPU and enginelimitations differencesNo Minor X A ACHKCURR

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12DIFFERENCE AIRCRAFT: GIV-XBASE AIRCRAFT: GVAPPROVED BY(POI)____________________________FLT PROCMANEUVER REMARKSCHAR CHNGNone None No NoLVLACOMPLIANCE METHODTRAININGLVL LVLB CLVLDCHK / CURRCHKCURR

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12DIFFERENCE AIRCRAFT: GIV-XBASE AIRCRAFT: GVAPPROVED BY(POI)____________________________SYSTEMREMARKSFLTCHARPROCCHNGLVLACOMPLIANCE METHODTRAININGLVL LVLB CLVLDCHK / CURR22 Autoflight TOGA Flight DirectorCommand Bars initiate at8 degrees vs. 12 degreesNo No X A Aon GV.23 Communications New Audio System No Minor X A A23 Communications Radio Tuning ThroughMCDU and graphicallyNo Minor X AA27 Flight Controls Lateral Control switchadded. Spoiler Control Yes Minor X B ASwitch deleted.30 Ice and Rain Pitot Probe Heat Systemchanged.No Minor X A A31 Indicating /Recording Systems31 Indicating /Recording Systems31 Indicating /Recording Systems31 Indicating /Recording SystemsElectronic Checklist AutoPop-up Feature deletedStandby EngineInstruments on MCDUDAU (Data AcquisitionUnit) and FWC (FaultWarning Computer)replaced by MAU(Modular Avionics Unit)Display ControllerCHKCURRNo Minor X A ANo Minor X A ANo Minor X A ANo Minor X A A34 Navigation IRS MSU switchesdeleted and replaced No Minor X A Awith ON/OFF switches34 Navigation 4 Display Units vs. 6Display UnitsNo Minor X B A34 Navigation Added Dual CCDs usedin Conjunction withNo Minor X B ADisplays34 Navigation LaserTrack removed No Minor X A A34 Navigation Standby Flightinstruments havedifferent design andNo Minor X A Alocation34 Navigation MCDU on EmergencyPowerNo Minor X B A49 APU Different APU installedwith no capability forAPU assisted mainengine airstart andNo Minor X A Adifferent electrical loadcapabilities.70 Powerplant Thrust decreased by900 lb to 13,850 lbNo No X A A

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12DIFFERENCE AIRCRAFT: GV-SPBASE AIRCRAFT: G-VAPPROVED BY(POI)____________________________DESIGNREMARKS20 Aircraft General PerformanceMax T.O. Weight91,000 lbIncrease of 500 lb21 ECS Outflow valve changed tothrust recovery outflowvalve.24 Electrical Power Revised Location of PDBcircuit breaker panels25 Equipment /FurnishingsRedesign and relocationof cockpit observer’s seatto behind Co-Pilot’s seat27 Flight Controls Trailing edge contours(TECs) added to inboardtrailing edge of flaps38 Water & Waste Fuselage conformal freshwater tank38 Water & Waste Relocation of vacuumlavatory waste tank frombaggage compartment toabove APU49 APU Bleeds off takeoffcapability added52 Doors Main Door movedforward 24 inches52 Doors Aft Lav Dump Doorrelocated53 Fuselage 27Boundary LayerEnergizers added abovethe canopy56 Windows Addition of 7 th cabinwindow57 Wings 7 Vortex Generatorsrelocated outboard oneach wingLimitationsMax Takeoff Weightincreased to 91,000 lbfrom 90,500 lb.FLTCHARPROCCHNGLVLACOMPLIANCE METHODTRAININGLVL LVLB CLVLDCHKG/CURRCHKCURRNo No X A ANo No X A ANo Minor X A ANo No X A ANo No X A ANo Minor X A ANo No X A ANo Major X A ANo No X A ANo No X A ANo No X A ANo No X A ANo No X A ANo No X A A

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12DIFFERENCE AIRCRAFT: GV-SPBASE AIRCRAFT: G-VAPPROVED BY(POI)____________________________COMPLIANCE METHODTRAINING CHKG/CURRFLT PROC LVL LVL LVL LVLMANEUVER REMARKSCHK CURRCHAR CHNG A B C DNormal Takeoff Bleeds Off No Minor X A A

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12DIFFERENCE AIRCRAFT: GV-SPBASE AIRCRAFT: G-VAPPROVED BY(POI)____________________________COMPLIANCE METHODSYSTEMREMARKSFLTCHARPROCCHNGLVLATRAININGLVL LVLB CLVLDCHKG/CURR22 Autoflight TOGA Flight DirectorCommand Bars initiate at8 degrees vs. 12 degreesNo No X A Aon GV.23 Communications New Audio System No Minor X A A23 Communications Radio Tuning ThroughMCDU and graphically31 Indicating/Recording Systems31 Indicating/Recording Systems31 Indicating/Recording Systems31 Indicating/Recording SystemsElectronic Checklist AutoPop-up Feature deletedDAU (Data AcquisitionUnit) and FWC (FaultWarning Computer)replaced by MAU(Modular Avionics Unit)Standby EngineParameters available on#1 MCDU onlyDifferent formatting onsome synoptic displays34 Navigation IRS MSU switchesdeleted and replacedwith ON/OFF switches34 Navigation 4 Display Units Vs 6Display Units withdifferent formatting.34 Navigation Added Dual CCD’s Usedin Conjunction withDisplays34 Navigation Display controllers havedifferent menus.34 Navigation Standby Flightinstruments havedifferent design andlocationCHKNo No X ANoMinorNonNormalCURRX A ANo Minor X A ANo Minor X A ANo Minor X A ANo Minor X A ANo Major X B ANo Minor X B ANo Minor X A ANo Major X B AA

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12DIFFERENCE AIRCRAFT: GV-SPBASE AIRCRAFT: G-VAPPROVED BY(POI)____________________________COMPLIANCE METHODSYSTEMREMARKSFLTCHARPROCCHNG34 Navigation Display Unit Controllerhas 4 overhead switchesinstead of 3 No Major X B ALVLALVLBLVLCLVLDCHKCURR34 Navigation RNP and EstimatedPosition Uncertainty(EPU) is displayed onPFD34 Navigation MCDU on EmergencyPower49 APU Bleeds off takeoffcapability added No Minor70 Powerplant Thrust increased by635 lb to 15,385 lbNo Minor X A ANo Minor X B AST,TCBI, SUVTNo No HO AAAA

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12DIFFERENCE AIRCRAFT: G-VBASE AIRCRAFT: GV-SPAPPROVED BY(POI)____________________________DESIGNREMARKS20 Aircraft General PerformanceMax T.O. Weight 500 lb.decrease to 90,500 lb21 ECS Outflow valve changedto butterfly style.24 Electrical Power Revised location ofPDB's and associatedcircuit breakers.25 Furnishings Redesign and relocationof cockpit observer’sseat to behind Captain’sseat27 Flight Controls Trailing Edge Contoursnot installed38 Water & Waste Non-fuselage conformalfresh water tank38 Water “& Waste Relocation of vacuumlavatory waste tank fromabove APU to baggagecompartment49 APU No Bleeds Off takeoffcapability52 Doors Main Door moved aft 24inches52 Doors Aft Lav Dump Doorrelocated53 Fuselage 27 Boundary LayerEnergizers removedfrom the canopy56 Windows Removal of 7 th cabinwindow57 Wings 7 Vortex generatorsrelocated inboard oneach wingLimitationsMax T.O. Weightdecreased by 500 lb to90,500 lbFLTCHARPROCCHNGLVLACOMPLIANCE METHODTRAININGLVL LVLB CLVLDCHKG/CURRCHKNo No X ACURRNo No X A ANo Minor X A ANo No X A ANo No X A ANo No X A ANo No X A ANo Minor X A ANo No X A ANo No X A ANo No X A ANo No X A ANo No X A ANo No X A AA

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12DIFFERENCE AIRCRAFT: G-VBASE AIRCRAFT: GV-SPAPPROVED BY(POI)____________________________COMPLIANCE METHODFLT PROCMANEUVER REMARKSCHAR CHNGNone No NoLVLATRAININGLVL LVLB CLVLDCHKG/CURRCHKCURR

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12DIFFERENCE AIRCRAFT: G-VBASE AIRCRAFT: GV-SPAPPROVED BY(POI)____________________________COMPLIANCE METHODSYSTEMREMARKSFLTCHARPROCCHNGLVLATRAININGLVL LVLB CLVLDCHKG/CURR22 Autoflight TOGA Flight DirectorCommand Bars initiateat 12 degrees vs. 8No No X A Adegrees on GV-SP.23 Communications New audio system No Minor X A A23 Communications Radio tuningaccomplished throughRFMU'sNo Minor X A A31 Indicating/Recording Systems31 Indicating/Recording31 Indicating/Recording Systems31 Indicating/Recording SystemsElectronic Checklist hasAuto pop-up Feature vs.passive checklist onGV-SPMAU replaced by DAUand FWCEngine Parametersavailable on eitherRFMUDifferent formatting onsome synoptic displaysCHKCURRNo Minor X A ANo Minor X B ANo Minor X A ANo Minor X A A34 Navigation EICAS FMS JoystickPanelNo None X A A34 Navigation LaserTrack No Minor X B A34 Navigation IRS ON/OFF switchesreplaced with IRS MSU No Minor X A Aswitches34 Navigation 6 Display Units Vs 4Display Units withNo Minor X B Adifferent formatting34 Navigation No CCD's installedXNo MinorB A

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12DIFFERENCE AIRCRAFT: GV-SPBASE AIRCRAFT: G-VAPPROVED BY(POI)____________________________SYSTEMREMARKS34 Navigation Display controllers havedifferent menus34 Navigation Standby Flightinstruments havedifferent design andlocation34 Navigation Display Unit Controllerhas 3 overheadswitches instead of 434 Navigation RNP and EstimatedPosition Uncertainty(EPU) are not displayedon PFD49 APU No bleeds off takeoffcapability70 Powerplant Thrust reduced 635 lbto 14,750 lbFLTCHARPROCCHNGLVLACOMPLIANCE METHODLVLBLVLCLVLDCHKCURRNo Minor x B ANo Minor X A ANo Minor X B ANo Minor X B ANo Minor X ANo No X A AA

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12Appendix 3 - TRAINING PROGRAM SPECIAL EMPHASIS ITEMSThe FSB has identified several aircraft systems and/or procedures that should receive specialemphasis in a GIV-X, G-V or GV-SP Training Program:Ground Training:1) EGPWS2) Flight Management System (FMS)3) Traffic Collision and Avoidance System (TCAS)4) Automatic mode of wing and cowl anti-ice systems5) Head-Up Display System (HUD) (See Appendix 6)6) Enhanced Vision System (EVS) (See Appendix 7)7) PlaneView System (GIV-X and GV-SP)8) Cursor Control Device (GIV-X and GV-SP)Systems Integration Training:1) Flight Guidance System (FGS)2) Primary Flight Display mode annunciators3) Flight Management System (FMS)4) Display Controllers (DC)5) Head-Up Display System (HUD) (See Appendix 6)6) Enhanced Vision System (EVS) (See Appendix 7)7) PlaneView System (GIV-X and GV-SP)8) Cursor Control Device (CCD)(GIV-X and GV-SP)Flight Training (Full Flight Simulator - Level C or D and/or aircraft):1) Dual hydraulic system malfunctions2) Aileron/elevator disconnect (jammed controls in each axis)3) ILS approach on standby instruments4) Primary Flight Display (PFD), Navigation Display (ND), EICAS reversionary modes.5) Integrated use of EICAS messages, switch positions and synoptic pages to determineaircraft system status.6) Using autopilot for completion of the emergency descent maneuver (EDM)7) Delayed engine response to full power applications at various altitudes (especially highaltitude stalls, touch and go landings, and any maneuvers with flaps less than 22 degrees.)8) Head-Up Display System (HUD) (See Appendix 6)9) Enhanced Vision System (EVS) (See Appendix 7)10) PlaneView System (GIV-X and GV-SP)11) Lateral Control Switch Function (GIV-X)

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12The FSB also found that early exposure to the FGS and FMS is important, especially for pilotswith no previous EFIS or FMS experience. Establishing early confidence in manually flying theaircraft, converting from manual to automatic (FMS controlled) flight mode and back is equallyimportant due to heavy reliance on the FGS. In the event of a flight path deviation due to inputerror or system malfunction, the flight crew must be able to comfortably transition fromautomatic to manual mode and back in an orderly fashion. Crew awareness and understanding ofthe flight mode(s) annunciated on the FMA is important during all phases of flight.The FSB found only one Special Flight Characteristic; the engine “spool-up” time is longer thanmost transport category jet aircraft. It can range from 8 seconds at sea level to 30 seconds at51,000 ft. to move from idle thrust to maximum continuous thrust. At low altitudes, i.e. circling,the spool-up time will be considerably longer than 8 seconds if flaps are less than 22 degrees.Training should emphasize this.The FSB strongly recommends that a thorough preflight briefing, highlighting engine spool-uptime, is accomplished prior to conducting training or checking in the following areas: stalls,touch & go landings, and simulated one-engine inoperative maneuvers. Also, touch and golandings at flaps zero are not recommended.

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12Appendix 4 – G-V OPERATING RULES COMPLIANCE CHECKLISTThe first production aircraft, serial number 505, was utilized by the FSB to conduct itsevaluation on February 7, 1997. This aircraft was, except for a few items, representative of anaircraft that could be issued a U.S. Airworthiness Certificate. It enabled the FSB to determinecompliance with the appropriate 14 CFR part 91 and part 135 operating requirements. Theattached checklist provides the FSB’s findings on those operating requirements. A FAR 125compliance checklist was not developed for this aircraft. Gulfstream has designed this aircraft tooperate with less than 6,000 pounds payload. Since the aircraft are delivered “green” from thefactory, the completion center will determine final payload capacity of the airplane. It may bepossible that individual aircraft may be outfitted to operate in excess of 6,000 pound payload.That operator would then have to show compliance with FAR 125 requirements, unless adeviation is obtained.Any U.S. operator wishing to operate the G-V aircraft will have to demonstrate to the FAA thatthe aircraft fully complies with all applicable 14 CFR parts prior to that aircraft entering service.This checklist may be used by the operator to show compliance with those items listed in it.

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAA OPERATIONAL REQUIREMENTS/COMPLIANCE for Gulfstream G-VPART 91 - GENERAL OPERATING AND FLIGHT RULESSUBPART A – GENERAL9 Civil Aircraft Flight Manual, Marking and Placardrequirements(a) Compliance with Flight Manual, Operator responsibility N/A(b)(1)Markings, and Placard MarkingsAvailability of current Airplane FlightManual in AircraftOperator responsibility(b)(2) Airplane Flight Manual requirement An approved Airplane Flight Manualcomplying with FAR 25.1581 isprovided with each aircraft(c)(d)Identification of Aircraft in Accordancewith FAR 45Helicopters: operation outside ofheight/speed envelopeAircraft are delivered “green” byGulfstream. Registration numbersmeet requirements when delivered.An approved Airplane Flight Manualcomplying with FAR 25.1581 isprovided with each aircraft.Completion center will be responsiblefor compliance with all other requiredexterior and interior markings.N/A N/AProvisional AFM has beenissued in December, 1996COMPLIESCould not determine fullcompliance.SUBPART B - FLIGHT RULES191 Category II Manual Operator responsibility The aircraft systems have not beenproved capable of Category IIoperations.Gulfstream will seek Cat IIequipment approval at a laterdateSUBPART C - EQUIPMENT, INSTRUMENTAND CERTIFICATE REQUIREMENTS203 Civil Aircraft: Certifications required(a) Valid C of A, Flight Permit,Registration CertificateAirworthiness certificate will be issuedfor each aircraft delivered fromproduction. Registration Certificate isowners responsibilityAircraft are issued Provisional A/WCertificates at the time of this reportCOMPLIES(b) Display of C of A Flight Permit Operator responsibility Completion Center will furnish holderand determine locationCould not determinecompliance(c) Fuel Tanks in the PassengerCompartmentN/A N/A

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAA OPERATIONAL REQUIREMENTS/COMPLIANCE for Gulfstream G-VPART 91 - GENERAL OPERATING AND FLIGHT RULESSUBPART C - EQUIPMENT, INSTRUMENTAND CERTIFICATE REQUIREMENTS(d) Compliance with FAR 34 (fuel ventingand emissions)Compliance with FAR 34 has beendemonstrated during TypeCertificationCOMPLIES205 Instrument and Equipment requirements(a) General Operator responsibility N/A(b) Day VFR All equipment specified for Day VFR, Exceptions are operator responsibility COMPLIESas applicable to a turbine engineaircraft is included in aircraftproduced under G-V ProductSpecification REV-C, except for:Item (12) – Pyrotechnic signaldevices are not provided. Flotationgear for crew only is provided.Item (13) - Crew Seats onlyItem (14) - N/AItem (15) - N/AItem (16) - N/A(c) Night VFR All equipment specified for Night VFR, Exceptions are operator responsibility COMPLIESItems (2) thru (6) are included inaircraft produced under G-V ProductSpecification REV-C , except for:Item (6) - Spare fuses are notCOMPLIESprovided since all re-settable circuitsare protected by circuit breakers.(d) IFR All equipment specified for IFR flight,COMPLIESItems (2) thru (9) are included inaircraft produced under G-V ProductSpecification REV-C .(e) Flight at and above FL240 DME equipment is included in aircraftproduced under G-V ProductSpecification REV-C .COMPLIES

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12SUBPART C - EQUIPMENT, INSTRUMENTAND CERTIFICATE REQUIREMENTSFAA OPERATIONAL REQUIREMENTS/COMPLIANCE for Gulfstream G-VPART 91 - GENERAL OPERATING AND FLIGHT RULES(f) Category II Operations All equipment as prescribed inparagraph (d) and Appendix A areprovided included in aircraft producedunder G-V Product SpecificationREV-C ,COMPLIANCE NOTDETERMINED215 ATC Transponder and Altitude reporting Equipment andUse(a)Transponder performance andenvironmental requirementsTwo Collins TDR94d Mode STransponders conforming to TSO-C112 is included in aircraft producedunder G-V Product SpecificationREV-C(b)(c) Transponder operationsTransponder operation is an operatorN/A(d)responsibility217 Data Correspondence between Automatically-Reportedpressure Altitude Data and Pilot's Reference(a) ATC-directed deactivation Operator responsibility N/A(b) Encoded altitude accuracy Mode C altitude-encoding equipmentcapable of transmitting altitude with atleast 125-foot accuracy is included inaircraft produced under G-V ProductSpecification REV-C(c)Altimeter-encoding equipmentspecificationsAltimeters conform to TSO-C10b andtransponders meet TSO-C112 whichaddresses the comments of TSO-C88Periodic testing and calibration is anoperator responsibilityCOMPLIESCOMPLIESCOMPLIES

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAA OPERATIONAL REQUIREMENTS/COMPLIANCE for Gulfstream G-VPART 91 - GENERAL OPERATING AND FLIGHT RULES219 Altitude Alerting System or Device: Turbo-Jet PoweredCivil Airplanes(a) Operational requirement for system Operator responsibility N/A(b) Altitude alerting system Requirements An altitude alerting system whichCOMPLIEScomplies with Requirements (1) thru(5) is included in aircraft producedunder G-V Product SpecificationREV-C(c)(d) Operational procedures Operator responsibility N/A(b)(c)(d)Transponder operationsTransponder operation is an operatorresponsibilityN/ASUBPART E - MAINTENANCE, PREVENTIVEMAINTENANCE, AND ALTERATIONS409 Inspections An maintenance schedule iscontained in the Gulfstream G-VMaintenance Program (derived fromthe MSG-3 process) was FAAaccepted in August, 1996Operator responsible foraccomplishing required maintenanceMAINTENANCEDOCUMENTS COMPLETEDBY GULFSTREAM411 Altimeter System and AltitudeReporting Equipment Tests and Inspections413 ATC Transponder Tests andInspectionsThe Maintenance Manuals includesthe tests and inspections required byFAR 43 and Appendices. The FAR 43tests and inspections are conductedby Gulfstream prior to delivery of theaircraft..Operator responsible for conductingtest and inspectionsCOMPLIES*** As above for 91.411 *** (as above) AS ABOVE

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAA OPERATIONAL REQUIREMENTS/COMPLIANCE for Gulfstream G-VPART 91 - GENERAL OPERATING AND FLIGHT RULESSUBPART F - LARGE AND TURBINE-POWEREDMULTI-ENGINE AIRPLANES503 Flying Equipment and Operating Information(a)(1) Flashlights Operator responsibility N/A(a)(2) Cockpit checklist Checklists are provided in theAirplane Flight Manual/OperatingManual.(a)(3)(4)(a)(5)Aeronautical charts Operator responsibility N/AOne engine inoperative climbperformance dataThe Airplane Flight Manual andOperating Manual contain therequired data.COMPLIES-BASED ONPROVISIONAL AFM DATAONLYCOMPLIES -PERFORMANCE DATABASED ON PROVISIONALAFM(b)(c) Cockpit checklist contents SAME AS (A)(2)(d) Use of data by crew Operator responsibility N/ASUBPART G - ADDITIONAL EQUIPMENT ANDOPERATING REQUIREMENTS FOR LARGE ANDTRANSPORT CATEGORY AIRCRAFT603 Aural Speed Warning Device Speed warning devices which complyCOMPLIESwith FAR 25.1303(c)(1) are includedin aircraft produced under G-VProduct Specification REV-C609 Flight Recorders and Cockpit voice Recorders(a) Operation with inactive flight recorder Operator responsibility N/Aor cockpit voice recorder(b) Operation by other than older of air Operator responsibility N/Acarrier or commercial certificate(c) Requirements for flight recorder An Flight Data Recorder is includedCOMPLIESwith aircraft produced under G-VProduct Specification REV C(d) Flight recorder operation Operator responsibility N/A

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12(e)Requirement for cockpit voicerecorderFAA OPERATIONAL REQUIREMENTS/COMPLIANCE for Gulfstream G-VPART 91 - GENERAL OPERATING AND FLIGHT RULESAn approved Cockpit Voice Recorderis included in aircraft produced underG-V Product Specification REV-C.Operation is continuous from starting(before starting engine) until the finalchecklist at the termination of theflight.COMPLIES(f) Erasure feature At least 30 minutes of CVR recordingCOMPLIESwill be retained(g) Erasure of flight recorder data orcockpit voice recordingOperator responsibility N/AFAA OPERATIONAL REQUIREMENTS/COMPLIANCE for Gulfstream G-VPART 135 – COMMUTER AND ONDEMAND OPERATIONSAPPENDIX CSUBPART A – GENERAL21 Manual Requirements Operator responsibility N/A23 Manual Contents(a) Authorized management Operator responsibility N/A(b) Weight & balance Operator responsibility An approved weight and balancemanual, is provided with each aircraft.Completion center will supplyadditional information uponcompletion of interior/exterior.(c) Operations Spec Operator responsibility N/A(d) Accident notification Operator responsibility N/A(e) Return to service approved Operator responsibility N/A(f) Defects Operator responsibility N/A(g) Defect rectification Operator responsibility N/A(h) Pilots maintenance, requestOperator responsibility N/Aprocedures(i) M.E.L. Operator responsibility A Master Minimum Equipment Listhas been developed by the FAACOMPLIES for “green”aircraftCompliance not determined

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAA OPERATIONAL REQUIREMENTS/COMPLIANCE for Gulfstream G-VPART 135 – COMMUTER AND ONDEMAND OPERATIONS(j) Re-fueling procedures Operator responsibility N/A(k) Pilots briefing Operator responsibility N/A(l) Flight locating procedures Operator responsibility N/A(m) Emergency procedures compliance Operator responsibility N/A(n) On route qualification procedures Operator responsibility N/A(o) Approved aircraft inspection program Operator responsibility A G-V Maintenance Program wasdeveloped by Gulfstream andaccepted by the FAA . This programmeets this requirement.(p) Procedures for hazardous materiel Operator responsibility N/A(q) Procedures for evacuation Operator responsibility N/A(r) Other procedures & policies Operator responsibility N/ASUBPART C - AIRCRAFT AND EQUIPMENT(a) Regulations Noted N/A(b) Approved/Operable instruments andequipmentOperator responsibilityCOMPLIES(c)ATC transponder performance andenvironmental conditionsATC transponders included in aircraftproduced under G-V ProductSpecification REV-C meet applicableTSO conditions149 Equipment Requirements: General(a) Altimeter Sensitive altimeter is included inaircraft produced under G-V ProductSpecification REV-CAll equipment and instrumentsincluded in aircraft produced under G-V Product Specification REV-C(b) Carburetor deicing N/A N/A(c) Third artificial horizon Third artificial horizon is included inaircraft produced under G-V ProductSpecification REV-C(d) (Reserved)(e) Any other equipment NotedCompliance to be determinedfor each operatorCOMPLIESCOMPLIESCOMPLIES - Powered byEmergency Electrical Powerupon complete generatorfailure

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAA OPERATIONAL REQUIREMENTS/COMPLIANCE for Gulfstream G-VPART 135 – COMMUTER AND ONDEMAND OPERATIONS151 Cockpit Voice Recorders(a) Requirement effectivity An approved cockpit voice recorder isCOMPLIESincluded in aircraft produced under G-V Product Specification REV-C.Operation is continuous from startingthe crew checklist, (before startingengine) until after final check list atthe termination of the flight.(b) Requirement effectivity N/A(c) Recorded information Operator responsibility N/A(d) Use of boom microphone Operator responsibility N/A(e) Erasure Feature At least 30 minutes of CVR.Recording will be retainedCOMPLIES152 Flight Recorders Operator responsibility Flight Data Recorder meeting all COMPLIESrelevant parts of 135.152 is includedin aircraft produced under G-VProduct Specification REV-C(a) Requirement effectivity Operator responsibility N/A(b) Requirement effectivity Operator responsibility N/A(c) Continuous operation Operator responsibility N/A(d) Retention of recorded data Operator responsibility N/A(e) Recorded information Operator responsibility N/A(f) Installation requirements Operator responsibility N/A(g) Recorder locator Operator responsibility N/A153 Ground Proximity Warning System(a) Approved G.P.W.S. equipment Operator responsibility Enhanced G.P.W.S. is included inaircraft produced under G-V ProductSpecification REV-C(b) Alternate system N/ACOMPLIES

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAA OPERATIONAL REQUIREMENTS/COMPLIANCE for Gulfstream G-VPART 135 – COMMUTER AND ONDEMAND OPERATIONS(c) Airplane flight manual The G-V Airplane Flight ManualCOMPLIES(Provisional) did not contain thenecessary information. The G-VOperating Manual contains thenecessary information(d) Deactivation of G.P.W.S. Operator responsibility N/A(e) Recording deactivation Operator responsibility N/A155 Fire Extinguishers: Passenger CarryingAircraft(a) Type and suitability of agent Operator responsibility Extinguishing agent in flight deck COMPLIESextinguisher is suitable for use incompartments(b) Flight deck Operator responsibility A flight deck fire extinguisher (halon) COMPLIESis included in aircraft produced underG-V Product Specification REV-C(c) Passenger compartment Operator responsibility N/A157 Oxygen Equipment Requirements(a) Unpressurized aircraft Owners responsibility Oxygen supply in passengercompartment is operatorsresponsibilityN/A(b) Pressurized aircraft Operator responsibility A flight crew oxygen system withsufficient quantity for operations up to51,000 FT certified in accordancewith applicable requirements of FAR25.1441 thru 1453 is provided.Oxygen supply for passengers is aresponsibility of the completion center(c) Equipment required Operator responsibility Indication of flight crew oxygen supplyand pilots use of undiluted oxygen isprovided as part of aircraft producedunder G-V Product SpecificationREV-CCOMPLIES for Crew OxygenCompliance for passengeroxygen could not bedeterminedCOMPLIES

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAA OPERATIONAL REQUIREMENTS/COMPLIANCE for Gulfstream G-VPART 135 – COMMUTER AND ONDEMAND OPERATIONS158 Pitot Heat Indication Systems(a) Compliance date 12/04/81 A pitot heat system with indicationscertified in accordance with FAR 25 isincluded in aircraft produced under G-V Product Specification REV-C(b) Compliance extension N/ACOMPLIES159 Equipment requirements: Passengersunder VFR at Night or under VFR Over-thetop161 Radio and Navigational Equipment:Carrying Passengers under VFR at Night orunder VFR over-the-top163 Equipment requirements: AircraftCarrying Passengers under IFR165 Radio and Navigational Equipment:Extended overwater or IFR Operations167 Emergency Equipment: Extendedoverwater Operation169 Additional Airworthiness Requirements(a1) 121.213 through 283. Specialairworthiness requirementsAll equipment required by thissection, with exception of (f)(3)(Flashlight) are provided as part ofthe aircraft produced under G-VProduct Specification REV-C.Note: With the exception of standbyinstruments, gyroscopic instrumentsare replaced by electronic equivalentAll radio and navigation equipmentrequired by this section is provided aspart of aircraft produced under G-VProduct Specification REV-CAll equipment and applicablerequirements of this section areincluded and provided for as part ofthe aircraft produced under G-VProduct Specification REV-C, with theexception of sub section (e).All dual radio and navigationequipment required by this section isprovided as part of aircraft producedunder G-V Product SpecificationREV-C, with the exception ofheadsetsFlashlight: Per 159(f)(3) is a operatorresponsibilityOxygen supply in passengercompartment is operatorsresponsibilityHeadsets are an operatorresponsibilityOperator responsibility N/AN/A Aircraft certified to FAR 25requirementsCOMPLIESCOMPLIESCompliance was not able tobe fully determined. at thetime of this reportCOMPLIESCOMPLIES

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAA OPERATIONAL REQUIREMENTS/COMPLIANCE for Gulfstream G-VPART 135 – COMMUTER AND ONDEMAND OPERATIONS(a2) 121.307 Engine instruments COMPLIES121.307 (a) Piston engine/propeller N/A N/A(b) (f) (h) (l) aircraft121.307 (c)121.307 (d)121.307 (e)121.307 (g)121.307 (i)121.307 (j)121.307 (k)Fuel pressureFuel flowmeterFuel quantityOil pressureOil temperatureTachometerFuel pressure warningIndication of these parametersrequired by (c) (d) (e) (g) (i) (j) (k) isprovided for in the aircraft producedunder G-V Product SpecificationREV-C, together with other engineparameters required by FAR 25(a3) 121.309 Emergency equipment Operator responsibility N/A(b) Reciprocating or turbo prop N/A N/A(c) Small airplane N/A N/A(d) Cargo of baggage compartments Operator responsibility N/A170 Materials for Compartment Interiors Materials for compartment interiorsper an STC are operatorsresponsibility171 Shoulder Harness Installation at FlightCrew Stations(a) Approved shoulder harness Approved shoulder harness for eachflight crew member is provided aspart of the aircraft produced under G-V Product Specification REV-CInterior materials used in flight deckare certified to FAR 25.853 standards(b) Use of shoulder harness Operator responsibility N/A173 Airborne Thunderstorm DetectionRequirements(a) Airborne thunderstorm detectionequipmentDigital airborne weather radarequipment is provided as part ofaircraft produced under G-V ProductSpecification REV-C(b) Helicopter requirements N/A N/A(c) Flight under IFR or night VFR N/A N/A(d) Equipment inoperative en route Operator responsibility N/A(e) Applicability Noted N/ACOMPLIES - direct indicatorof fuel pressure not providedto crewCOMPLIESCOMPLIESCOMPLIES

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAA OPERATIONAL REQUIREMENTS/COMPLIANCE for Gulfstream G-VPART 135 – COMMUTER AND ONDEMAND OPERATIONS(f) Power supply Noted N/A175 Airborne Weather Radar EquipmentRequirements(a) Airborne weather radar equipment Digital airborne weather radarCOMPLIESequipment is provided as part ofaircraft produced under G-V ProductSpecification REV-C(b) Flight under IFR or night VFR Operator responsibility N/A(c) Equipment inoperative on route Operator responsibility N/A(d) Applicability Noted(e) Power supply Noted177 Emergency Equipment Requirements N/Afor aircraft Having a Passenger SeatingConfiguration of More than 19 PassengersAircraft is not certified for passengerseating of more than 19180 Traffic Alert and Collision AvoidanceSystem(a) Effectivity Operator responsibility COMPLIES(b) Flight manual requirements G-V Airplane Flight Manual(Provisional) does not contain thisinformation. Operating Manualcontain required informationN/ACOMPLIES181 Performance Requirements: AircraftOperated over-the-top or in IFR Conditions(a) Climb requirements Operator responsibility Aircraft climb performance data isprovided in aircraft flight manual(b) Helicopters N/A N/A(c) Weather considerations Operator responsibility N/A(d) Continued flight VFR Operator responsibility N/ACompliance based on data inG-V Provisional AirplaneFlight Manual

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAA OPERATIONAL REQUIREMENTS/COMPLIANCE for Gulfstream G-VPART 135 – COMMUTER AND ONDEMAND OPERATIONS183 Performance Requirements: LandAircraft Operated Overwater(a) Engine failure Operator responsibility N/A(b) Take-off or landing Operator responsibility N/A(c) Climb requirements Operator responsibility Aircraft climb performance data isprovided in aircraft flight manual(d) Helicopters N/A N/A185 Empty weight and center of gravity:Currency Requirement(a) Aircraft weighing Operator responsibility Actual weight and balance manualprovided with each aircraft. Finalweight and balance information isprovided by the completion center.(b) Applicability Operator responsibility N/ACompliance based on data inG-V Provisional AirplaneFlight ManualCompliance determined for“green” aircraft only deliveredfrom the manufacturerSUBPART F - FLIGHT CREWMEMBER FLIGHT TIMELIMITATIONS AND REST REQUIREMENTS269 (b)(5) Flight Time Limitations and Rest Operator responsibilityRequirements: Unscheduled Three andFour Pilot CrewsAircraft is designed to have crew restfacilities. Completion center willdetermine configuration. Compliancemust be done on individual aircraftbasis.Compliance not determinedSUBPART J - MAINTENANCE, PREVENTATIVEMAINTENANCE, AND ALTERATIONS419 Approved Aircraft Inspection Program Operator responsibility A G-V Maintenance Program wasdeveloped by Gulfstream andaccepted by the FAA . This programmeets this requirementCompliance to be determinedfor each operator

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAA OPERATIONAL REQUIREMENTS/COMPLIANCE for Gulfstream G-VPART 135 – COMMUTER AND ONDEMAND OPERATIONS421 Additional Maintenance Requirements(a) Nine seat or less Operator responsibility (dependent oninterior seating capacity)A G-V Maintenance Program wasdeveloped by Gulfstream andaccepted by the FAA . This programmeets this requirement(b) Definition Noted427 Manual Requirements(a) Certificate holders organization Operator responsibility Operator responsible for(b)Manual requirements for maintenanceand inspectionN/Aaccomplishing required maintenanceOperator responsibility N/ACompliance to be determinedupon individual aircraftconfiguration

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12Appendix 5 – GV-SP OPERATING RULES COMPLIANCE CHECKLISTSerial number 5001, was utilized by the FSB to conduct its evaluation on February 17, 2003. 5001was a GV-SP flight test aircraft. It enabled the FSB to determine compliance with the appropriate 14CFR part 91 and 135 operating requirements. The attached checklist provides the FSB’s findings onthose operating requirements. A FAR 125 compliance checklist was not developed for this aircraftsince Gulfstream has designed this aircraft to operate with less than 6,000 pounds payload. Since theaircraft are delivered “green” from the factory, the completion center will determine final payloadcapacity of the airplane. It may be possible that individual aircraft may be outfitted to operate inexcess of 6,000 pound payload. That operator would then have to show compliance with FAR 125requirements, unless a deviation is obtained.Any U.S. operator wishing to operate the GV-SP aircraft will have to demonstrate to the FAA thatthe aircraft fully complies with all applicable 14 CFR parts prior to that aircraft entering service. Thischecklist may be used by the operator to show compliance with those items listed in it.

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark* SUBPART A - GENERAL *91. 1 91-257 Applicability Noted91. 3 Responsibility and Authority of the Not applicableOperatorPilot in CommandResponsibility91. 5 Pilot in Command Requiring More Not applicableOperatorthan One Required PilotResponsibility91. 7Civil Aircraft AirworthinessOperatorResponsibility(a)Airworthy ConditionsNotedFSB FindingOperatorResponsibilityOperatorResponsibilityOperatorResponsibility(b)91. 9(a)DeterminationCivil Aircraft Flight Manual,Marking, and PlacardRequirementsOperating Limitations---An FAA-approved Airplane FlightManual complying with 14 CFR part25.1581 is provided with eachaircraft. Additional compliance withoperational requirements recordedherein.OperatorResponsibilityOperatorResponsibilityOperatorResponsibility(b) (1)Availability of current AirplaneFlight in aircraftAn FAA-approved Airplane FlightManual complying with 14 CFR part25.1581 is provided with eachaircraft.OperatorResponsibilityOperatorResponsibility(b)(2)Airplane Flight Manual not requiredNot applicableNotApplicable(c)Identification of aircraft inaccordance with 14 CFR part 45A fireproof identification platecomplying with 14 CFR part 45 isincluded in the production airplane.Aircraft are delivered “green” byGulfstream and meet RegistrationNumber requirements whendelivered.Operatorresponsibilityat outfittingafter paint.NotApplicable(d)Not applicableCompliance with part 2991. 11 Prohibition on Interference with --- OperatorCrewmembersResponsibility91. 13 Careless or Reckless Operation --- OperatorResponsibility91. 15 Dropping Objects --- OperatorResponsibility91. 17 Alcohol or Drugs --- OperatorResponsibility91. 19 Carriage of Narcotic Drugs, --- OperatorMarihuana, and Depressant orResponsibilityStimulant Drugs or Substances91. 21 Portable Electronic Devices --- Operator91. 2391-267 Truth-in-Leasing ClauseRequirement in Leases andConditional Sales ContractsResponsibilityOperatorResponsibilityNotApplicableOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibility(a)Contract ContentNotedOperator

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemarkFSB FindingResponsibility(b)ExclusionNotedOperatorResponsibility(c)Requirements for Contract---OperatorResponsibility(d)Public inspection---OperatorResponsibility(e)Lease description---OperatorResponsibility91. 25 Aviation Safety Reporting Program:Prohibition Against Use of Reportsfor Enforcement Purposes91. 27 -91. 99* SUBPART B - FLIGHT RULES *(a)OperatorResponsibility[ Reserved ] -------91.101 Applicability Noted -------91.103Preflight ActionOperatorResponsibilityFlight under IFR---OperatorResponsibilityOperatorResponsibility(b)Take-off and landing distances An FAA-approved Airplane FlightManual complying with 14 CFR part25.1581 is provided with eachaircraft91.105 91-231 Flight Crewmembers at Stations --- Operator91.107 91-250 Use of Safety Belts, ShoulderHarnesses, and Child RestraintSystems91.109 Flight Instruction; SimulatedInstrument Flight and Certain FlightTestsNo change to the shoulder harnessinstallation from G-V. Certified as a16 ‘g’ installation.ResponsibilityProper use ofthe equipmentis operatorResponsibility--- OperatorResponsibility91.111 Operating near Other Aircraft --- OperatorResponsibility91.113 Right-of-Way Rules: Except Water --- OperatorOperationsResponsibility91.115 Right-of-Way: Water Operations --- OperatorResponsibility91.117 91-233 Aircraft Speed The information on minimum safe Operatorspeed is provided in FAA-approved ResponsibilityAirplane Flight Manual91.119 Minimum Safe Altitudes: General --- OperatorResponsibility91.121 Altimeter Settings --- OperatorResponsibility91.123 91-244 Compliance with ATC Clearances --- Operatorand InstructionsResponsibility91.125 ATC Light Signals --- OperatorResponsibility91.126 91-239 Operating On or In the Vicinity of --- Operatoran Airport in Class G AirspaceResponsibilityCompliesOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibility(a)(b)(c)Operator Responsibility(d)compliesOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark91.127 91-239 Operating On or In Vicinity of an --- OperatorAirport in Class E AirspaceResponsibility91.129 91-234 Operation in Class D Airspace --- OperatorResponsibility91.130 91-239 Operations in Class C AirspaceOperatorResponsibility(a), (b),General; Deviations---(c), (e)FSB FindingOperatorResponsibilityOperatorResponsibilityOperatorResponsibility(d)Equipment requirementsCompliance with 91.215 is outlinedbelow91.131 Operations in Class B Airspace --- OperatorResponsibility91.133 Restricted and Prohibited Areas --- OperatorResponsibility91.135 Operations in Class A Airspace --- OperatorResponsibility91.137 Temporary Flight Restrictions --- OperatorResponsibility91.138 91-270 Temporary Flight Restrictions in --- OperatorNational Disaster Areas in theResponsibilityState of Hawaii91.139 Emergency Air Traffic Rules --- Operator91.141 Flight Restrictions in the Proximityof the Presidential and OtherParties91.143 Flight Limitation in the Proximity ofSpace Flight Operations91.144 91-240 Temporary Restriction on FlightOperations During Abnormally HighBarometric Pressure Conditions91.145 Management of aircraft operationsin the vicinity of aerialdemonstrations and major sportingevents91.146-91.14991.151 Fuel Requirements or Flight in VFRConditions91.153 VFR Flight Plan: InformationRequiredResponsibility--- OperatorResponsibility--- OperatorResponsibility--- OperatorResponsibility--- OperatorResponsibility[Reserved] --- -------OperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibility--- OperatorResponsibilityOperatorResponsibility--- Operator OperatorResponsibility Responsibility91.155 91-235 Basic VFR Weather Minimums --- Operator OperatorResponsibility Responsibility91.157 91-262 Special VFR Weather Minimums --- Operator OperatorResponsibility Responsibility91.159 VFR Cruising altitude or Flight --- Operator OperatorLevelResponsibility Responsibility91.161 -[ Reserved ] -------91.16591.167 Fuel Requirements for Flight in IFR --- Operator OperatorConditionsResponsibility Responsibility91.169 91.259 IFR Flight Plan: Information --- Operator OperatorRequiredResponsibility Responsibility91.171 VOR Equipment Check For IFR Dual VOR installation meets the Operator OperatorOperationsrequirement when delivered Responsibility Responsibility91.173 ATC Clearance and Flight Plan --- Operator OperatorRequiredResponsibility Responsibility91.175 91.267 Take-off and Landing Under IFR --- Operator OperatorResponsibility Responsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark91.177 Minimum Altitudes for IFR--- OperatorOperationsResponsibility91.179 IFR Cruising Altitude or Flight Level --- OperatorResponsibility91.181 Course to be Flown --- OperatorResponsibility91.183 IFR Radio Communications --- OperatorResponsibility91.185 91-211 IFR Operations: Two-way Radio --- OperatorCommunication FailureResponsibility91.187 Operations under IFR In Controlled --- OperatorAirspace: Malfunction reportsResponsibility91.189Category II and III Operations The aircraft is not certified forCategory II operations. This willoccur in a follow-on certification.The FAA-approved Airplane FlightManual will be updated at that time.FSB FindingOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityNotDemonstrated(a)(1).(a)(2)(a)(3)Appropriate authorization &adequateknowledge of crewmembersInstrument panel and equipmentinstalled---Instrument panel meets therequirements of the section.OperatorResponsibilityThis will bedemonstratedduring theCategory IIcertificationeffort.OperatorResponsibilityNotdemonstrated91.189(b)Airborne equipmentNoted.OperatorResponsibilityOperatorResponsibility(c)-(g)---OperatorApproaches, Landing, ExceptionsResponsibility91.191 Category II Manual Gulfstream will provide a Category Operator NotII FAA-approved Airplane Flight Responsibility DemonstratedManual Supplement as a templatefor Category II Manual91.193 Certificate of Authorization for --- Operator Not ApplicableCertain Category II OperationsResponsibility91.195 -[ Reserved ] --- -------91.199* SUBPART C - EQUIPMENT, INSTRUMENT, and CERTIFICATE REQUIREMENTS*91.201 [ Reserved ] -------91.203 91-218 Civil Aircraft: CertificationsRequired(a)Valid C of A, RegistrationCertificate.C of A is issued for each aircraftdelivered from production. At thetime of this report, it is a ProvisionalC of A.OperatorResponsibilityOperatorResponsibility(b)(c)C of A displayedFuel Tanks in the passengercompartment---Not applicableOperatorResponsibilityOperatorResponsibilityNot Applicable

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemarkCompliance with 14 CFR part 34(d) Compliance with Part 34has been demonstrated duringType Certification91.205 91-251 Instrument and EquipmentRequirementsFSB FindingComplies(a)GeneralSee BelowOperatorResponsibilityOperatorResponsibility(b)Day VFRAll equipment specified forDay VFR, as applicable toa turbine engine aircraft isincluded in the productionairplane, except for Item(12) – Pyrotechnic signaldevices are not provided.Item (13) – Crew seats only.Passenger seats to be compliedwith during outfittingItem (16) - Not applicableItem (17) - Not applicableComplies(c)Night VFRAll equipment specified for NightVFR, Items (2) thru (6) are includedin the production airplane, exceptfor:Item (6) - Spare fuses are notprovided since all re-settablecircuits are protected by circuitbreakers.Complies(d)IFRAll equipment specified for IFRflight, Items (2) thru (9) areincluded per GV-SP ProductSpecification.Complies(e)Flight at and above FL240DME equipment is included per theGV-SP Product Specification.Complies(f)Category II OperationsAll equipment as prescribed inParagraph (d) and Appendix A areprovided per the GV-SP ProductSpecification.Category II is afollow-oncertificationactivity.NotDemonstrated

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark91.207 91-265 Emergency Locator TransmittersFSB Finding(a)GeneralAn emergency locator transmitterConforming to TSO-C91A isprovided as part of the productionairplane.Operatingcondition,para. (a)(1) isan operatorresponsibilityOperatorResponsibility(b)LocationThe ELT is mounted on primarystructure in the aft compartment ofthe fuselage in order to minimizethe probability of damage in theevent of crash impact.Complies(c)Battery condition---OperatorResponsibilityOperatorResponsibility(d)Periodic inspections---OperatorResponsibilityOperatorResponsibility(e)Ferrying with inoperative ELT---OperatorResponsibilityOperatorResponsibility(f)91.209Exceptions to para. 91.207(a)Aircraft LightsELT is installed in production andflight test airplanes prior to firstflightOperatorResponsibilityOperatorResponsibility(a), (b),Position and anti-collision lightsPosition lights and anti-collisionlights complying with 14 CFR part25.1381 through 25.1397 and25.1401 respectively are includedin the production airplane.Use of theselights is anOperatorresponsibility.OperatorResponsibility(c)91.211Anchor LightsSupplemental OxygenNot applicableNot applicable(a),(b)(1)(b)(2)GeneralPilot at ControlsA flight crew supplemental oxygensystem is included in the productionairplane. Crew oxygen masks areprovided for both pilots andobserver.Passenger oxygen system to beinstalled during outfitting.---OperatorResponsibilityto useequipment asrequired.OperatorResponsibilityOperatorResponsibilityOperatorResponsibility91.213 Inoperative Instruments andEquipment91.21591-267 ATC Transponder and AltitudeReporting Equipment and UseGulfstream has an approved MMELfor the baseline airplane. GV-SPspecific items have been submittedfor the next FOEB meeting.MEL LOA isOperatorResponsibilityComplies(a)Transponder performance andenvironmental requirementsTwo Honeywell Mode STransponders with ATC Modes Aand C conforming to TSO-C112 areprovided in the production airplaneComplies(b), (c),Transponder operations--- TransponderOperator

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark(d)operation isan operatorresponsibility91.217Data Correspondence betweenAutomatically - Reported PressureAltitude Data and Pilot’s ReferenceFSB FindingResponsibility(a)Deactivation directed---OperatorResponsibilityOperatorResponsibility(b)Encoded altitude accuracyMode C altitude – productionairplane is delivered with a recent(within last 30 days) air datacalibration IAW 14 CFR part 91.411and 14 CFR part 43Periodictesting andcalibration isan operatorresponsibilityComplies(c)91.219Altimeter-encoding equipmentspecificationsAltitude alerting system or device:Turbo-Jet Powered Civil AirplanesConform to TSO-C10 and C88Complies(a)Operational Requirement forsystem---OperatorResponsibilityComplies(b)Altitude Alerting SystemRequirementsThe production airplane is deliveredwith an approved altitude alertingsystem meeting the requirementsof (b)Complies(c),(d)Operational Procedures---OperatorResponsibilityOperatorResponsibility91.221(a)(b)Traffic Alert and CollisionAvoidance System Equipment andUseRequirement for an approvedTCASTCAS: operation requiredA Traffic Alert and CollisionAvoidance System (TCAS II/ACASII) is provided in the productionairplane.---OperatorResponsibilityCompliesOperatorResponsibility91.223Terrain Awareness and WarningSystem(a)A/C manufactured after March 29,2002A Class A TAWS (compliant withTSO C151) is provided in theproduction airplane.Complies(b)A/C manufactured on or beforeMarch 29, 2002Not applicableNot Applicable(c)AFMAll applicable information isprovided in the FAA-approvedAirplane Flight ManualComplies(d)ExceptionsNot applicableNot Applicable91.224 - [ Reserved ] --- -------

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position Gulfstream FSB FindingRemark91.299* SUBPART D - SPECIAL FLIGHT OPERATIONS*91.301 [ Reserved ] --- -------91.303 91-227 Aerobatics Flight --- OperatorResponsibilityOperatorResponsibility91.305 Flight Test Areas --- OperatorResponsibilityOperatorResponsibility91.307 91-268 Parachutes and Parachuting Not applicable -------91.309 91-227 Towing: Gliders --- OperatorResponsibility91.311 Towing: Other than under § 91.309 --- OperatorResponsibility91.313Restricted Category Civil Aircraft:Operating LimitationsOperatorResponsibilityOperatorResponsibilityNot Applicable(a); (b);(c); (d);(e); (f)General---OperatorResponsibilityOperatorResponsibility(g)Shoulder harness approvalNot applicable. part 23 airplanesOperatoronlyResponsibility91.315 Limited Category Civil Aircraft: --- Operator OperatorOperating LimitationsResponsibility Responsibility91.317 91-212 Provisionally Certificated Civil Provisional AFM issued December, Operator OperatorAircraft: Operating Limitations 2002Responsibility Responsibility91.319 Aircraft Having Experimental --- Operator OperatorCertificates: Operating LimitationsResponsibility Responsibility91.321 Carriage of Candidates in Federal --- Operator OperatorElectionsResponsibility Responsibility91.323 91-253 Increased Maximum Certificated Not applicableNot applicableWeights for Certain AirplanesOperated in Alaska91.325 Primary Category Aircraft:Not applicableNot applicableOperating Limitations91.326-[ Reserved ] --- -------91.399* SUBPART E - MAINTENANCE, PREVENTIVE MAINTENANCE, and ALTERATIONS *91.401 Applicability Noted -------91.403 91-267 General(a) (b)Airworthy conditions; Maintenance---OperatorResponsibilityOperatorResponsibility(c)91.405Required proceduresMaintenance RequiredAn approved maintenanceschedule derived from the MSG-3process and an AircraftMaintenance Manual complyingwith 14 CFR part 25.1529 andAppendix H is provided to eachoperator upon delivery of theairplane.OperatorResponsibility(a); (b);(d)Discrepancies; RecordsOperatorResponsibilityOperatorResponsibility(c)Inoperative instrumentsThe aircraft will have an approvedMMEL. Approval of applicable MELis the operator’s responsibility.OperatorResponsibilityOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark91.407 Operation after Maintenance, --- OperatorPreventive Maintenance,Responsibilityrebuilding, or alteration91.409 91-267 Inspections An approved maintenanceschedule derived from the MSG-3process and an AircraftMaintenance Manual complyingwith 14 CFR part 25.1529 andAppendix H is provided to eachoperator.91.410 91.266 Special maintenance programrequirements91.411 Altimeter System and AltitudeReporting Equipment Tests andInspectionsNot applicableThe Airplane Maintenance Manualincludes the tests and inspectionsrequired by 14 CFR part 43 andappendices. The 14 CFR part 43tests and inspections areconducted for each aircraft prior toC of A.Operatorresponsible foraccomplishingrequiredmaintenanceOperatorResponsibilityFSB FindingOperatorResponsibilityOperatorResponsibilityNot ApplicableOperatorResponsibility91.413 91-267 ATC Transponder Tests andInspections91.415 Changes to aircraft inspectionprogram91.417Maintenance recordsThe Airplane Maintenance Manualincludes the tests and inspectionsrequired by 14 CFR part 43 andappendices. The 14 CFR part 43tests and inspections areconducted for each aircraft prior toC of A.Operatorresponsibilityafter airplaneis in service.--- OperatorResponsibilityOperatorResponsibilityOperatorResponsibility(a), (b),(c)(d)Documents requirementsFuel tank installationAn approved maintenanceschedule derived from the MSG-3process and the AirplaneMaintenanceManual complying with 14 CFR part25.1529 and Appendix H isprovided to each operator.OperatorResponsibilityOperatorResponsibilityNot ApplicableNot applicable, since the fuel tankis not installed within the passengercompartment/baggagecompartment91.419 Transfer of maintenance records --- Operator OperatorResponsibility Responsibility91.421 Rebuilt engine maintenance Not applicableNot applicablerecords91.423 -[ Reserved ] --- -------91.499* SUBPART F - LARGE AND TURBINE-POWERED MULTIENGINE AIRPLANES*91.501 Applicability Noted. Operator91.503Flying Equipment and OperatingInformationResponsibilityOperatorResponsibility(a)(1)FlashlightsTwo rechargeable Magliteflashlights are provided as basicaircraft equipment, one for eachpilot’s station.Workingcondition isresponsibilityof operator.Complies(a)(2)Cockpit checklistChecklists are provided in theOperatorOperator

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemarkFAA-approved Airplane Flight ResponsibilityManual / Operating Manual / QRHFSB FindingResponsibility(a)(3) &(a)(4)Aeronautical charts---OperatorResponsibilityOperatorResponsibility(a)(5)One engine inoperative climbperformance dataThe FAA-approved Airplane FlightManual and Operating Manualinclude the required data.Operatorresponsibilityto use the dataComplies(b), (c)Cockpit checklist contentsThe FAA-approved Airplane FlightManual contains all requiredchecklists.OperatorresponsibilityComplies(d)Use of data by crew91.505 Familiarity with operating limitationsand emergency equipment91.507 Equipment requirements: Over-thetopor night VFR operations---An FAA-approved Airplane FlightManual complying with 14 CFR part25.1581 is provided with theairplane at delivery.All equipment specified for IFRflight and Night VFR is included inthe production airplane.OperatorResponsibilityOperatorResponsibilityOperatorresponsible foroperableequipmentOperatorResponsibilityOperatorResponsibilityComplies91.509 Survival equipment for overwateroperations91.51191-249 Radio equipment for overwateroperationsThe aircraft is equipped forExtended Over Water Operationsfor the crew only as a productionairplane. The airplane is equippedfor passengers during outfitting.---OperatorResponsibilityNotedOperatorResponsibility(a)(b)Equipment requirementsThe production airplane meets theequipment requirements.Complies(c)(d)Equipment exclusions---OperatorResponsibilityOperatorResponsibility(e)Definition of “shore”---Noted-----------------(f)Equipment requirements in specificremote oceanic areas---OperatorResponsibilityOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark91.513Emergency EquipmentFSB Finding(a)GeneralNoted----------------(b)Equipment requirementsThe production airplane isequipped with a fire extinguisher inthe cockpit, smoke goggles and lifejackets for the 2 pilots andobservers, and a portable oxygenbottle with full face mask. Theequipment meets this paragraph.OperatorResponsibility(c)(1)(2)Fire extinguishersA HALON fire extinguisher isinstalled in the cockpit as part ofthe production airplane.Complies(c)(3)(4)Fire extinguishersCabin fire extinguishers areinstalled during outfitting.OperatorResponsibilityOperatorResponsibility(d)First Aid kitFirst Aid Kits are installed duringthe outfitting processTheemergencymedical kit isoperatorresponsibilityOperatorResponsibility(e)Crash axeNot applicableOperatoroptionComplies(f)MegaphonesNot applicableOperatoroption91.515 Flight altitude rules --- OperatorResponsibility91.517Passenger InformationNot ApplicableOperatorResponsibility(a)Smoking and seat-belt signsSmoking and seat-belt signs areinstalled during the outfittingprocessOperatorResponsibilityOperatorResponsibility(b)Oral notification if no signsprovided---OperatorresponsibilityOperatorResponsibility(c)---No smoking allowed while “NoSmoking” signs lighted(d)(e)---Passenger compliance with signsand instructions91.519 91-231 Passenger briefing The applicable placards and lightedpassenger information signs areinstalled during outfitting. A videoand printed cards are also providedto the operator at delivery.91.521Shoulder HarnessOperatorresponsibilityOperatorResponsibilityOral briefing isOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityComplies(a)(1)(2)Shoulder Harness – Flight DeckThe 2 pilot seats and observer seatinstalled in the production airplanemeet these requirements.Complies(b)(1)(2)Shoulder Harness – FlightAttendant Seat in CabinIf an operator chooses to installsuch a seat(s), it will be installedOperatorOption andOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position Gulfstream FSB FindingRemarkduring outfitting and comply. Responsibility91.523 Carry-on baggage Not applicable -------91.525Carriage of Cargo(a)Carriage of cargo - RequirementsThe baggage compartment is aClass B compartment and meetsthe requirements of (a)(i) thru (v)Complies(b)91.527Accessibility of compartments forfireextinguishingOperating in Icing ConditionsThe aft baggage compartment isclassified as a Class B cargocompartmentAFMEmergencyproceduresmeet thisrequirementComplies(a)Take-off with contaminatedsurfaces---OperatorResponsibilityOperatorResponsibility(b), (c)IFR/VFR flight into known orforecasted icing conditionsThe GV-SP is a transport airplaneand is certified for FIKIOperatorresponsibility(d)---OperatorForecast icing conditions reliefResponsibility91.529 Flight Engineer requirements --- OperatorResponsibility91.531 Second in command requirements --- OperatorResponsibility91.533 Flight attendant requirements Not applicable with 9 or fewer Operatorpassengers. With 10 or more Responsibilitypassengers, a trained evacuationcrewmember is required per theEquivalent Safety Finding.91.535 Stowage of food, beverage, andpassenger service equipmentduring aircraft movement on thesurface, takeoff, and landing--- OperatorResponsibilityCompliesOperatorResponsibilityNot ApplicableOperatorResponsibilityOperatorResponsibilityOperatorResponsibility91.536 -[ Reserved ] --- -------91.599*SUBPART G - ADDITIONAL EQUIPMENT and OPERATING REQUIREMENTS FOR LARGE and TRANSPORTCATEGORY AIRCRAFT *91.601 Applicability Noted -------91.603 Aural Speed Warning Device The production airplane complies. Complies91.60591-256 Transport Category Civil AirplaneWeight Limitations(a)Conditions for aircraft certificatedbefore October 1, 1958Not applicableNot Applicable(b)Maximum take-off and landingweights for airfield elevation,ambient temperature, wind andrunway gradient.The FAA-approved Airplane FlightManual and Weight and BalanceManual contains all data necessaryto enable the operator to complywith this requirement. TheOperating Manual contains flightplanningdata to enablecomputation of fuel burned fromdeparture to destination oralternate airport. Additionally, theproduction airplane is equippedwith an on-board flight-planningOperatorResponsibilityComplies

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemarkcomputer for takeoff, en route, andlanding computations to assist thecrew in performing thesecalculations.FSB Finding91.607(a)(b)Emergency exits for airplanescarrying passengers for hire.The aircraft is equipped with fourType IV over wing exits (two oneach side). See Equivalent SafetyFinding from the Transport AirplaneDirectorate.NotApplicableComplies(c)91.60991-228 Flight Recorders and Cockpit VoiceRecordersOperatorResponsibility(a)-(b)General---OperatorResponsibilityOperatorResponsibility(c)Requirement for flight recorderThe airplane is equipped with adigital flight data recorder meetingthe requirements of 14 CFR part 91in production. The 14 CFR part135 eighty-eight (88) parameterDFDR will be certified as a followoncertification effort.Complies(d)Flight recorder operationThe flight recorder installed in theproduction airplane meets thisrequirement.Complies(e), (f)Requirement for cockpit voicerecorderThe cockpit voice recorder installedin the production airplane meetsthese requirements.Complies(g)Action required following accidentor incident – NTSB report andrecords---OperatorResponsibilityOperatorResponsibility91.611 Authorization for ferry flight with Not applicableNot Applicableone engine inoperative91.613 Materials For CompartmentInteriorsTo be addressed during theoutfitting by STCOperatorResponsibility91.615 -[ Reserved ] -------91.699*SUBPART H - FOREIGN AIRCRAFT OPERATIONS AND OPERATIONS OF US REGISTERED CIVIL AIRCRAFT OUTSIDE OFTHE UNITED STATES; AND RULES GOVERNING PERSONS ON BOARD SUCH AIRCRAFT*91.701 Applicability Noted OperatorResponsibilityOperatorResponsibility91.702 Persons on board --- OperatorResponsibilityOperatorResponsibility91.703 Operations of civil aircraft of U.S.registry outside of the UnitedStates--- OperatorResponsibilityOperatorResponsibility91.705 Operations within airspacedesignated as Minimum NavigationPerformance SpecificationAirspace--- OperatorResponsibilityOperatorResponsibility91.706 Operations within airspace --- Operator Operator

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position Gulfstream FSB FindingRemarkdesignated as Reduced VerticalResponsibility ResponsibilitySeparation Minimum Airspace91.707 Flights between Mexico or Canadaand the United States--- OperatorResponsibilityOperatorResponsibility91.709 Operations to Cuba---OperatorResponsibilityOperatorResponsibility91.711 Special rules for foreign civil aircraft --- OperatorResponsibilityOperatorResponsibility91.713 Operation of civil aircraft of Cubanregistry--- OperatorResponsibilityOperatorResponsibility91.715 Special flight authorizations forforeign civil aircraft--- OperatorResponsibilityOperatorResponsibility91.717 -[ Reserved ] --- -------91.799* SUBPART I - OPERATING NOISE LIMITS*91.801 Applicability: Relation to Part 36 Noted -------91.803 part 125 operations: Designation of NotedNot Applicableapplicable regulations91.805 Final compliance The production airplane is certifiedCompliesto 14 CFR part 36 Stage 3requirements as noted in the FAAapprovedAirplane Flight Manual.91.807Phased compliance under parts121, 125, and 135: Subsonicairplanes(a)GeneralNoted-------------(b)Compliance schedulesThe production airplane is certifiedto 14 CFR part 36 Stage 3requirements as noted in the FAAapprovedAirplane Flight Manual.Operator(c)Apportionment of airplanes---Responsibility91.809 Replacement airplanes --- OperatorResponsibility91.811 Service to small communities --- Operatorexemption: Two engine, subsonicResponsibilityairplanes91.813 Compliance plans and status: USoperations of subsonic airplanes91.815 Agricultural and fire fightingairplanes: Noise operatinglimitationsThe production airplane is certifiedto 14 CFR part 36 Stage 3requirements as noted in the FAAapprovedAirplane Flight Manual.Not applicableCompliesOperatorResponsibilityNot ApplicableNot ApplicableCompliesNot Applicable91.817 Civil aircraft sonic boom Not applicable Not Applicable91.819 Civil supersonic airplanes that do Not applicableNot Applicablenot comply with 14 CFR part 3691.821 Civil supersonic airplanes: noise Not applicableNot Applicablelimits91.823 -[ Reserved ] --- -------91.84991.851 Definitions Noted -------91.853 Final compliance: civil subsonicairplanesCompliesThe production airplane is certifiedto 14 CFR part 36 Stage 3requirements as noted in the FAAapprovedAirplane Flight Manual.91.855 Entry and non-additional rule The production airplane is certified Complies

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemarkto 14 CFR part 36 Stage 3requirements as noted in the FAAapprovedAirplane Flight Manual.91.857 Stage 2 operations outside of the The production airplane is certified48 contiguous United States and to 14 CFR part 36 Stage 3authorization for maintenance requirements as noted in the FAA-91.859 Modification to meet Stage 3 noiselevelsapproved Airplane Flight Manual.The production airplane is certifiedto 14 CFR part 36 Stage 3requirements as noted in the FAAapprovedAirplane Flight Manual.91.861 Base level --- OperatorResponsibility91.863 Transfers of Stage 2 airplanes with --- Operatorbase levelResponsibility91.865 Phased compliance for operators --- Operatorwith base levelResponsibility91.867 91-252 Phased compliance for new --- OperatorentrantsResponsibility91.869 Carry-forward compliance --- OperatorResponsibility91.871 Waivers from interim compliance --- OperatorrequirementsResponsibility91.873 Waivers from final compliance --- OperatorResponsibilityFSB FindingNot ApplicableNot ApplicableNot ApplicableNot ApplicableNot ApplicableNot ApplicableNot ApplicableNot ApplicableNot ApplicableNot Applicable91.875 Annual progress reports --- OperatorResponsibility91.877 Annual reporting of Hawaiian --- Operator Not ApplicableoperationsResponsibility91.879 -[ Reserved ] --- -------91.899* SUBPART J - WAIVERS *91.901 [ Reserved ] --- -------91.903 Policy and procedures Noted OperatorResponsibilityOperatorResponsibility91.905 91-227 List of rules subject to waivers Noted OperatorResponsibilityOperatorResponsibility91.907 -91.999[ Reserved ] --- -------

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark* SUBPART A - GENERAL *135. 1 135-58 ApplicabilityNotedOperatorResponsibility(a)General---FSB FindingOperatorResponsibility(b)[Reserved]-------------------(c)Sightseeing operator defined---OperatorResponsibility(d)Unscheduled repair requirements ---135. 2 135-66 Compliance schedule for operators --- Operatorthat transition to part 121 of thisResponsibilitychapter; certain new entrantoperators135. 3 135-65 Rules applicable to operations --- Operatorsubject to this partResponsibility135. 7 135-58 Applicability of rules to--- Operatorunauthorized operatorsResponsibility135. 12 Previously trained crewmembers --- OperatorResponsibility135. 19 Emergency operations --- OperatorResponsibility135. 21 135-66 Manual requirements --- OperatorResponsibility135. 23 135-58 Manual contentsOperatorResponsibilityOperatorResponsibilityNot ApplicableOperatorResponsibilityOperatorResponsibilityNot ApplicableOperatorResponsibilityOperatorResponsibilityOperatorResponsibility(a)Personnel roster---OperatorResponsibility(b)(c)Weight and balanceOperations specificationsA FAA-approved weight andbalance manual is provided witheach aircraft---OperatorResponsibilityOperatorResponsibility(d)Accident notification procedures---OperatorResponsibility(e)Aircraft airworthiness notification topilot in command---OperatorResponsibility(f)Procedures for reporting inflightmaintenance irregularities---OperatorResponsibility(g)Notification of corrective actions tomaintenance irregularities---OperatorResponsibility(h)Pilot in command procedures toobtain unscheduled maintenance---OperatorResponsibility(i)(j)Minimum Equipment ListRefueling proceduresA GV-SP Master MinimumEquipment List has been submittedto the FAA---OperatorResponsibilityOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemarkFSB Finding(k)Passenger briefing procedures---OperatorResponsibility(l)Flight locating procedures---OperatorResponsibility(m)Compliance with emergencyprocedures---OperatorResponsibility(n)Pilot enroute qualificationprocedures---OperatorResponsibility(o)(p)(q)(r)135. 25Approved aircraft inspectionprogramProcedures for hazardous materialhandlingEvacuation procedures forassisting another person to an exitduring an emergencyOther procedure and policyinstructions135-66 Aircraft requirementsAn MSG 3 Maintenance Programhas been developed by Gulfstreamand approved by the FAA---------OperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibility(a)Registration and airworthinesscertificateAircraft is delivered withappropriate documentationOperatorResponsibilityOperatorResponsibility(b)Aircraft usage---OperatorResponsibility(c)Aircraft usage duration---OperatorResponsibility(d)Operation in common carriage135. 41 Carriage of narcotic drugs,marihuana, and depressant orstimulant drugs or substances135. 43 Crewmember certificates:International operations* SUBPART B – FLIGHT OPERATIONS *------ OperatorResponsibility--- OperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibility135. 61 General Noted -------135. 63 135-52 Record keeping requirements --- OperatorResponsibilityOperatorResponsibility135.64 135-66 Retention of contracts andamendments: Commercialoperators who conduct intrastateoperations for compensation or hire--- OperatorResponsibilityOperatorResponsibility135.65 Reporting mechanical irregularities --- OperatorResponsibility135.67 135-1 Reporting potentially hazardous --- Operatormeteorological conditions andResponsibilityirregularities of communications ornavigation facilitiesOperatorResponsibilityOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark135.69 Restriction or suspension of --- Operatoroperations: Continuation of flight inResponsibilityan emergency135.71 135-32 Airworthiness check --- OperatorResponsibility135.73 Inspections and tests --- Operator135.75 Inspectors credentials: admissionto pilots’ compartment: Forwardobserver’s seat135.77 Responsibility for operationalcontrol(a)(b)Responsibility--- OperatorResponsibility--- OperatorResponsibility135.79 Flight locating requirements --- OperatorResponsibility135.81Informing personnel of operational ---Operatorinformation and appropriateResponsibilitychangesCertificate holder must makeavailable:Airman’s Information Manual orequivalent---Installed-equipment manuals andFAA-approved Airplane FlightManual provided with aircraftFSB FindingOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibility(c)(d)14 CFR parts 135 and 91Aircraft equipment manuals andAircraft Flight Manual---OperatorResponsibilityOperatorResponsibility135.83(a)For foreign operations, theInternational Flight InformationManual or equivalentOperating information requiredPublications accessible in cockpitA normal, abnormal, andemergency procedures checklistsand the information on one-engineinoperativeclimb performance isprovided in FAA-approved AirplaneFlight ManualOperatorResponsibilityOperatorResponsibilityOperatorResponsibility(b)Cockpit checklist requirementsOperatorResponsibilityOperatorResponsibility(c)Emergency procedures checklist135.85 Carriage of persons withoutcompliance with the passengercarryingprovisions of this part135.87Carriage of cargo including carryonbaggage(a)(b)Approved cargo rack or binSecured by approved meansOperatorResponsibility--- OperatorResponsibilityA Class B baggage compartment islocated at the aft portion of thepressure vessel and additionalstorage compartments are providedduring outfitting using customer’sspecificationsOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibility(c)(d)SpecificationsUnder-seat stowageOperatorResponsibilityOperator

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemarkFSB FindingResponsibility(e)135.89(a)Cargo compartment fireextinguishing requirementsPilot requirements: Use of oxygenUnpressurized aircraftThe normally pressurized aircraft isequipped with two 115 cubic feetoxygen cylinders plumbed into thesupplemental oxygen systemOperatorResponsibilityOperatorResponsibilityOperatorResponsibility(b)135.91(a)Pressurized aircraft135-60 Oxygen for medical use bypassengersInstallation and maintenancerequirementsA medical oxygen system may beinstalled in the aircraft duringoutfitting at customer’s requestOperatorResponsibilityOperatorResponsibilityOperatorResponsibility(b)Smoking restrictionsOperatorResponsibility(c)Personnel qualificationsOperatorResponsibility(d)ExceptionOperatorResponsibility(e)135.93(a)Exception reporting135-68 Autopilot: Minimum altitudes foruseMinimum enroute altitudeMinimum altitude for autopilotusage is defined in limitationssection of FAA-approved AirplaneFlight ManualOperatorResponsibilityOperatorResponsibilityOperatorResponsibility(b)During ILS approachOperatorResponsibility(c)ILS in degraded weatherOperatorResponsibility(d)Use to touchdownOperatorResponsibility(e)Use during takeoff and initial climbOperatorResponsibility(f)Not applicable to rotorcraft135.95 Airmen: Limitations on use ofservices135.97 Aircraft and facilities for recentflight experience135.99Composition of flight crew(a)Minimum flight crew per AircraftFlight Manual and 14 CFR part 135--- OperatorResponsibility--- OperatorResponsibilityFAA-approved Airplane Flight OperatorManual specifies a minimum of two Responsibilityflight crewmembers: pilot andcopilotOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityMinimum of 2crew; pilot andcopilot(b)Second in command requirementOperatorResponsibility135.100 Flight crewmember duties --- Operator Operator

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position Gulfstream FSB FindingRemarkResponsibility Responsibility135.101 Second in command requiredunder IFR--- OperatorResponsibilityOperatorResponsibility135.103 [Reserved] -------135.105 135-58 Exception to second in commandOperatorrequirement: Approval for use ofResponsibilityautopilot system(a)Operations during VFRFAA-approved Airplane FlightManual specifies a minimum of twoflight crewmembers: pilot andcopilotOperatorResponsibility(b)Request for amendmentOperatorResponsibility(c)Specifications for amendment135.107 Flight attendant crewmemberrequirementFAA-approved Airplane FlightManual requires a flight attendantwhen 10 or more passengers areon board.135.109 Pilot in command or second incommand: Designation required135.111 Second in command required inCategory II operations135.113 Passenger occupancy of pilot seat FAA-approved Airplane FlightManual specifies a minimum of twoflight crewmembers: pilot andcopilotOperatorResponsibility--- OperatorResponsibility--- OperatorResponsibilityOperatorResponsibility135.115 Manipulation of controls --- OperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityNotDemonstratedOperatorResponsibilityOperatorResponsibility135.117 135-44 Briefing of passengers before flight --- OperatorResponsibility135.119 Prohibition against carriage of --- OperatorweaponsResponsibility135.120 135-73 Prohibition on interference with --- OperatorcrewmembersResponsibility135.121 Alcoholic beverages --- OperatorResponsibility135.122 Stowage of food, beverage, and --- Operatorpassenger service equipmentResponsibilityduring aircraft movement on thesurface, takeoff, and landing135.123 Emergency and emergency --- Operatorevacuation dutiesResponsibility135.125 Airplane security --- Operator135.127 135-76 Passenger informationrequirements and smokingprohibitions135.128 135-62 Use of safety belts and childrestraining systemsResponsibility--- OperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibility--- OperatorResponsibility135.129 135-60 Exit seating --- OperatorResponsibility* SUBPART C – AIRCRAFT AND EQUIPMENT *135.141 Applicability Noted Operator135.143(a)135-22 General requirementsGeneralNotedOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityResponsibilityOperator

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemarkFSB FindingResponsibility(b)Required instruments andequipment in operable conditionAll instruments and equipmentincluded as part of the productionairplaneOperatorResponsibility(c)ATC transponder equipment Two ATC transponders included aspart of the production airplane andmeet applicable TSO conditions135.144 135-73 Portable electronic devices --- OperatorResponsibility135.145 Aircraft proving tests --- OperatorResponsibility135.47 Dual controls required Airplane is produced with dual flightcontrols under 14 CFR part 25135.149 135-38 Equipment requirements: General(a)Sensitive altimeterSensitive altimeter is included aspart of the production airplaneOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperators ofthe G-IV, G-V,or GV-SP neednot conductproving flightsif the G-IV, G-V or GV-SPare added totheir fleet.CompliesComplies(b)(c)(d)Carburetor heating or deicingequipmentA third gyroscopic bank-and-pitchindicator[Reserved](e)Any other equipment FAA requires135.150 Public address and crewmemberinterphone systems135.151135-60 Cockpit voice recordersNot applicableThird gyroscopic bank-and-pitchindicator is included as part of theproduction airplane---NotedFAA-approved Airplane FlightManual limits passenger load to 19peopleNot ApplicableNot ApplicableComplies----------------------------Not Applicable(a)ApplicabilityA FAA-approved cockpit voicerecorder is included as part of theproduction airplaneOperatorResponsibilityComplies135.151(b)(c)(d)(e)Multi-engine, turbine-poweredairplane having 20 to 30 passengerseatsProcedures following accident orincidentRequirements for recording fromboom or mask microphoneFAA-approved Airplane FlightManual limits passenger load to 19people---Installed CVR records theuninterrupted audio signal from aboom or mask microphone inaccordance with 14 CFR part25.1457(c)(5)Installed CVR retains at least 30Not ApplicableOperatorResponsibilityCompliesComplies

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemarkRecording duration requirements minutes of audio recording135.152 135-69 Flight recordersFSB Finding(a)ApplicabilityA FAA-approved Flight DataRecorder meeting the eighty-eightparameter requirement of 14 CFR135.152 will be a follow-oncertification effort.Complies GVASC 100 / GV-SP ASC 002(b)Multi-engine, turbine-poweredairplane having 20 to 30 passengerseatsFAA-approved Airplane FlightManual limits passenger load to 19peopleNot Applicable(c)Continuous operation requirementsSee note for (a)NotDemonstrated(d)(e)Recorded data retentionrequirementsSee note for (a)See note for (a)NotDemonstratedNotDemonstrated(f)(g)(h)Procedures following accidentRequirements with respect toaircraft manufacture dateDevice to assist in underwaterlocatingSee note for (a)See note for (a)See note for (a)NotDemonstratedNotDemonstratedNotDemonstrated(i)(j)(k)Operational parametersParameters for turbine-poweredairplanes having 20 to 30passenger seats and manufacturedafter August 18, 2000Parameters for turbine-poweredairplanes having 20 to 30passenger seats and manufacturedafter August 19, 2000FAA-approved Airplane FlightManual limits passenger load to 19peopleFAA-approved Airplane FlightManual limits passenger load to 19peopleNot applicableNotDemonstratedNot ApplicableNot Applicable135.153Exception to requirements fordeHavilland DHC-6135-75 Ground proximity warning system(a)ApplicabilityA FAA-approved enhanced groundproximity warning system isincluded as part of the productionairplaneOperatorResponsibilityComplies(b)[Reserved]----------------135.153(c)Airplane Flight ManualrequirementsFAA-approved Airplane FlightManual includes operationalprocedures for enhanced groundproximity warning systemComplies

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark(d)Operation requirements---(e)Deactivation requirements---(f)Expiration of requirementNoted135.154Terrain awareness and warningOperatorsystemResponsibilityFSB Finding(a)Airplanes manufactured afterMarch 29, 2002A FAA-approve terrain awarenesswarning system meeting therequirements for Class Aequipment in TSO-C151 is includedas part of the production airplaneComplies(b)(c)135.155Airplanes manufactured on orbefore March 29, 2002Airplane Flight ManualFire extinguishers: Passengercarryingaircraft---FAA-approved Airplane FlightManual includes operationalprocedures for enhanced groundproximity warning systemOperatorResponsibilityNot ApplicableComplies(a)Type and quantity of hand fireextinguisher extinguishing agentExtinguishing agent (halon) in flightdeck hand fire extinguisher issuitable for all fires likely to occurOperatorResponsibility(b)One hand fire extinguisherconvenient and located on flightdeckA flight deck hand fire extinguisheris included as part of the productionairplane.OperatorResponsibility(c)135.157One hand fire extinguisherconvenient and located inpassenger compartmentOxygen equipment requirementsAt least one hand fire extinguisheris mounted in the passengercompartment at a convenientlocation during outfittingOperatorResponsibilityOperatorResponsibility(a)Unpressurized aircraftThe normally pressurized aircraft isequipped with two 115 cubic feetoxygen cylinders plumbed into thesupplemental oxygen system,providing oxygen to crew and, uponaircraft outfitting, passengersOperatorResponsibility(b)Pressurized aircraftSee note for (a)Notdemonstrated(c)135.158(a)System operation135-33 Pitot heat indication systemsApplicabilityOxygen system quantity monitoringis through gauges on flight deck,three flight deck oxygen regulatingsystems readily allow monitoringand adjustmentsA pitot heat system with indicationscertified in accordance with FAR 25OperatorResponsibilityCompliesComplies

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemarkis included as part of the productionairplaneFSB Finding(b)135.159(a)(b)Extension135-38 Equipment requirements: Carryingpassengers under VFR at night orunder VFR over-the-top conditionsGyroscopic rate-of-turn indicatorSlip skid indicator--- -------All equipment required by this Operatorsection are included as part of the Responsibilityaircraft produced under GV-SPProduct SpecificationCompliesComplies(c)(d)(e)(f)(g)(h)135.161(a)Gyroscopic bank-and-pitchindicatorGyroscopic direction indicatorGeneratorNight flight requirementsContinuous in-flight electrical loaddefinedHelicopter requirementsRadio and navigational equipment:Carrying passengers under VFR atnight or under VFR over-the-topTwo-way radio communication withground facilities 25 miles awayNot applicableAll radio and navigation equipmentrequired by this section areincluded as part of the aircraftproduced under GV-SP ProductSpecificationOperatorResponsibilityCompliesCompliesCompliesCompliesCompliesNot ApplicableComplies(b)VFR over-the-top requires ability toreceive radio signals from groundfacilityComplies(c)135.163(a)(b)VFR at night requires ability toreceive radio signals from groundfacility135-73 Equipment requirements: Aircraftcarrying passengers under IFRVertical speed indicatorFree-air temperature indicatorAll equipment and applicablerequirements of this section areincluded as part of the aircraftproduced under GV-SP ProductSpecificationOperatorResponsibilityCompliesCompliesComplies(c)Heated pitot tube for each airspeedindicatorComplies(d)e)Power failure warning device forgyroscopic instrumentsAlternate source of static pressureComplies(f)Single-engine aircraft requirementsComplies(g)Multi-engine aircraft requirementsComplies(h)Two independent sources ofenergy, each of which is able todrive all required gyroscopicinstrumentsComplies

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark(i)Continuous inflight electrical loaddefined135.165 135-61 Radio and navigational equipment:OperatorExtended overwater or IFRResponsibilityoperations(a)135.165(b)(c)Specifications, 10 passenger seatsor moreSpecifications, other aircraft thanspecified in (a)Independent receiver defined(d)FAA consideration of long-rangecommunications and navigationequipment135.167 135-49 Emergency equipment: Extendedoverwater operations135.169 135-55 Additional airworthinessrequirementsAll radio and navigation equipmentrequired by this section areincluded as part of the aircraftproduced under GV-SP ProductSpecification, with the exception ofheadsets--- OperatorResponsibilityAircraft certified to 14 CFR part 25 Operatorrequirements, equipment required Responsibilityby this section are included as partof the aircraft produced under GV-SP Product Specification135.170 135-56 Materials for compartment interiors Materials used in flight deck arecertified to 14 CFR part 25.853standards, compartment materialsare per an STC and resolvedduring outfitting135.171Shoulder harness installation atflight crewmember stationsOperatorResponsibilityOperatorResponsibilityFSB FindingCompliesCompliesCompliesCompliesCompliesOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityComplies(a)Approved shoulder harnessFAA-approved shoulder harnessfor each flight crewmember stationis installed as part of the aircraftproduced under GV-SP ProductSpecificationOperatorResponsibility(b)135.173Use of shoulder harness135-60 Airborne thunderstorm detectionequipment requirements---OperatorResponsibilityOperatorResponsibility(a)ApplicabilityDigital airborne weather radarequipment is standard equipmentComplies(b)Helicopter operationsNot applicableNot Applicable(c)Flight under IFR or night VFR---OperatorResponsibility(d)(e)Procedures for Equipment failureenrouteExceptions for certain locations------OperatorResponsibilityOperatorResponsibility(f)Alternate electrical power supplynot requiredNotedOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark135.175Airborne weather radar equipmentOperatorrequirementsResponsibility(a)ApplicabilityDigital airborne weather radar isequipment is standard equipmentFSB FindingComplies(b)Flight under IFR or night VFR---OperatorResponsibility(c)Procedures for Equipment failureenroute---OperatorResponsibility(d)Exceptions for certain locations---OperatorResponsibility(e)Alternate power supply not requiredNotedOperatorResponsibility135.177 135-80 Emergency equipmentrequirements for aircraft having apassenger seating configuration ofmore than 19 passengersFAA-approved Airplane FlightManual limits passenger load to 19people135.178 Additional emergency equipment FAA-approved Airplane FlightManual limits passenger load to 19people135.179 135-60 Inoperable instruments andequipment135.180 135-54 Traffic Alert and CollisionAvoidance SystemA Master Minimum Equipment Listhas been developed by the FAAOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityNot ApplicableNot ApplicableOperatorResponsibility(a)ApplicabilityA FAA-approved TCAS II/ACAS IIsystem is included as part of theproduction airplaneComplies(b)Airplane Flight Manualrequirements135.181 135-70 Performance requirements: Aircraftoperated over-the-top or in IFRconditions135.183 Performance requirements: Landaircraft operated over water135.185 Empty weight and center of gravity:Currency requirementFAA-approved Airplane FlightManual includes operationalprocedures for traffic alert andcollision avoidance systemFAA-approved Airplane FlightManual includes applicableperformance dataFAA-approved Airplane FlightManual includes applicableperformance dataA FAA-approved weight andbalance manual is provided witheach aircraft, final weight andbalance information provided uponcompletion of outfittingOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityCompliesCompliesCompliesOperatorResponsibility* SUBPART D – VFR/IFR OPERATING LIMITATIONS AND WEATHER REQUIREMENTS *135.201 Applicability Noted ------135.203 VFR: Minimum altitudes --- OperatorResponsibilityOperatorResponsibility135.205 135-41 VFR: Visibility requirements --- OperatorResponsibilityOperatorResponsibility135.207 VFR Helicopter surface referencerequirementsNot applicableOperatorResponsibilityOperatorResponsibility135.209 VFR: Fuel supply --- OperatorResponsibilityOperatorResponsibility135.211 135-32 VFR: Over-the-top carryingpassengers: Operating limitations--- OperatorResponsibilityOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark135.213 135-60 Weather reports and forecasts --- OperatorResponsibility135.215 IFR: Operating limitations --- OperatorResponsibility135.217 IFR: Takeoff limitations --- OperatorResponsibility135.219 IFR: Destination airport weather --- OperatorminimumsResponsibility135.221 IFR: Alternate airport weather --- OperatorminimumsResponsibility135.223 135-20 IFR: Alternate airport requirements --- OperatorResponsibility135.225 IFR: Takeoff, approach and landing --- OperatorminimumsResponsibility135.227 135-60 Icing conditions: OperatingGV-SP is transport airplane Operatorlimitationscertified for FIKI. AFM hasResponsibilityoperating limitations for icingconditions.135.229 Airport requirements --- OperatorResponsibility* SUBPART E – FLIGHT CREWMEMBER REQUIREMENTS *FSB FindingOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibility135.241 135-57 Applicability Noted -------135.243 135-58 Pilot in command qualifications --- OperatorResponsibilityOperatorResponsibility135.244 135-58 Operating experience --- OperatorResponsibilityOperatorResponsibility135.245 Second in command qualifications --- OperatorResponsibilityOperatorResponsibility135.247 Pilot qualifications: Recentexperience--- OperatorResponsibilityOperatorResponsibility135.249 135-51 Use of prohibited drugs --- OperatorResponsibilityOperatorResponsibility135.251 Resting for prohibited drugs --- OperatorResponsibilityOperatorResponsibility135.253 135-48 Misuse of alcohol --- OperatorResponsibilityOperatorResponsibility135.255 135-48 Testing for alcohol --- OperatorResponsibilityOperatorResponsibility* SUBPART F – CREWMEMBER FLIGHT TIME AND DUTY PERIOD LIMITATIONS AND REST REQUIREMENTS *135.261 135-52 Applicability Noted -------135.263 Flight time limitations and restrequirements: All certificate holders--- OperatorResponsibilityOperatorResponsibility135.265 Flight time limitations and restrequirements: Scheduledoperations--- OperatorResponsibilityOperatorResponsibility135.267 135-60 Flight time limitations and restrequirements: Unscheduled oneandtwo-pilot crews135.269 Flight time limitations and restrequirements: Unscheduled threeandfour-pilot crews135.271 Helicopter hospital emergencymedical evacuation service(HEMES)--- OperatorResponsibility--- OperatorResponsibility--- OperatorResponsibility135.273 135-60 Duty period limitations and resttime requirements--- OperatorResponsibility* SUBPART G – CREWMEMBER TESTING REQUIREMENTS *135.291 Applicability Noted -------135.293 135-27 Initial and recurrent pilot testing --- OperatorrequirementsResponsibilityOperatorResponsibilityOperatorResponsibilityNot ApplicableOperatorResponsibilityOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark135.295 Initial and recurrent flight attendant --- Operatorcrewmember testing requirementsResponsibility135.297 135-15 Pilot in command: Instrument --- Operatorproficiency check requirementsResponsibility135.299 Pilot in command: Line checks: --- OperatorRoutes and airportsResponsibility135.301 Crewmember: Tests and checks, --- Operatorgrace provisions, training toResponsibilityaccepted standards* SUBPART H – TRAINING *FSB FindingOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibility135.321 135-63 Applicability and terms used Noted -------135.323 Training program: General --- OperatorResponsibilityOperatorResponsibility135.324 135-67 Training program: Special rules --- OperatorResponsibilityOperatorResponsibility135.325 Training program and revision:Initial and final approval ---OperatorResponsibilityOperatorResponsibility135.327 Training program: Curriculum --- OperatorResponsibilityOperatorResponsibility135.329 Crewmember training requirements --- OperatorResponsibilityOperatorResponsibility135.331 Crewmember emergency training --- OperatorResponsibilityOperatorResponsibility135.333 Training requirements: Handlingand carriage of hazardousmaterials--- OperatorResponsibilityOperatorResponsibility135.335 135-1 Approval of aircraft simulators andother training devices135.337 Qualifications: Check airmen(aircraft) and check airmen(simulator)135.338 135-64 Qualifications: Flight instructors(aircraft) and flight instructors(simulator)--- OperatorResponsibility--- OperatorResponsibility--- OperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibility135.339 135-64 Initial and transition training andchecking: Check airmen (aircraft),check airmen (simulator)135.340 135-64 Initial and transition training andchecking: Flight instructors(aircraft), flight instructors(simulator)135.341 135-18 Pilot and flight attendantcrewmember training programs135.343 135-18 Crewmember initial and recurrenttraining requirements135.345 135-46 Pilots: Initial, transition, andupgrade ground training135.347 Pilots: Initial, transition, upgrade,and differences flight training135.349 Flight attendants: Initial andtransition ground training--- OperatorResponsibility--- OperatorResponsibility--- OperatorResponsibility--- OperatorResponsibility--- OperatorResponsibility--- OperatorResponsibility--- OperatorResponsibility135.351 135-46 Recurrent training --- OperatorResponsibility135.353 Prohibited drugs --- OperatorResponsibility* SUBPART I – AIRPLANE PERFORMANCE OPERATING LIMITATIONS *135.361 Applicability Noted135.363 135-21 General --- OperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark(b)Each certificate holder operating a Aircraft performance data isturbine engine powered large provided in the FAA approvedtransport category airplaneAirplane Flight ManualFSB FindingOperatorResponsibility(f)Performance data in the AirplaneFlight Manual135.365 Large transport category airplanes:Reciprocating engine powered:Weight limitations135.367 Large transport category airplanes:Reciprocating engine powered:Takeoff limitations135.369 Large transport category airplanes:Reciprocating engine powered:En route limitations:All engines operating135.371 Large transport category airplanes:Reciprocating engine powered:En route limitations:One engine inoperative135.373 Large transport category airplanes:Reciprocating engine powered:En route limitations:Two engines inoperative135.375 Large transport category airplanes:Reciprocating engine powered:Landing limitations:Destination airports135.377 Large transport category airplanes:Reciprocating engine powered:Landing limitations:Alternate airports135.379 135-71 Large transport category airplanes:Turbine engine powered:Takeoff limitationsAircraft performance data isprovided in the FAA approvedAirplane Flight ManualNot applicableNot applicableNot applicableNot applicableNot applicableNot applicableNot applicable---OperatorResponsibilityOperatorResponsibilityNot applicableNot applicableNot applicableNot applicableNot applicableNot applicableNot applicable(a)Takeoff weights exceeding AirplaneFlight Manual limitations---OperatorResponsibilityOperatorResponsibility135.379(b)(c)(d)(2)(e)Minimum distance required fortakeoffMaximum takeoff weight calculationvariablesMaximum takeoff weight net takeoffflight pathMaximum takeoff weightThe FAA-approved Airplane FlightManual contains all data necessaryto enable the operator to complywith this requirement to includeclearway computation data.The FAA-approved Airplane FlightManual contains all data necessaryto enable the operator to complywith this requirement.The FAA-approved Airplane FlightManual contains all data necessaryto enable the operator to complywith this requirement to include nettakeoff flight path data.The FAA-approved Airplane FlightManual contains all data necessaryNot applicableOperatorResponsibilityOperatorResponsibilityOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12(f)(g)FAR Amdt. Requirement Gulfstream Position GulfstreamRemarkenvironmental conditionsto enable the operator to complywith this requirement to includeenvironmental variables.Aircraft bank angles on takeoffPerformance terms135.381 Large transport category airplanes:Turbine engine powered:En route limitations: One engineinoperativeThe FAA-approved Airplane FlightManual complies with thisparagraph.The performance terms are thesame as certified under 14 CFRpart 25The FAA-approved Airplane FlightManual and the Operating Manualcontains all data necessary toenable the operator to comply withthis requirement.OperatorResponsibilityFSB FindingOperatorResponsibilityOperatorResponsibilityOperatorResponsibility135.383 Large transport category airplanes:Turbine engine powered:En route limitations:Two engines inoperative135.385Large transport category airplanes:Turbine engine powered:Landing limitations:Destination airportsNot applicableOperatorResponsibilityNot applicable(a)(b)Landing weight limitationsDestination landing requirementsThe airplane FAA-approved FlightManual contains all data necessaryto enable the operator to complywith this requirement. TheOperating Manual contains flightplanning data to enablecomputation of fuel and oil burnedfrom departure to destination oralternate airport to compute landingweight.See note for (a)OperatorResponsibilityOperatorResponsibility(c)Turbopropeller landingrequirements---OperatorResponsibility(d)Wet runway landing requirements---OperatorResponsibility(e)Alternate requirements to complywith paragraph (b)135.387 Large transport category airplanes:Turbine engine powered:Landing limitations:Alternate airportsSee note for (a)The FAA-approved Airplane FlightManual contains all data necessaryto enable the operator to complywith this requirement. TheOperating Manual contains flightplanning data to enableOperatorResponsibilityOperatorResponsibilityOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position Gulfstream FSB FindingRemarkcomputation of fuel and oil burnedfrom departure to destination oralternate airport to compute landingweight. On board flight planningcomputer available to assist crew inmission calculations.135.389 Large nontransport category Not applicableNot applicableairplanes:Takeoff limitations135.391 Large nontransport category Not applicableNot applicableairplanes: En route limitations:One engine inoperative135.393 Large nontransport category Not applicableNot applicableairplanes: Landing limitations:Destination airports135.395 Large nontransport category Not applicableNot applicableairplanes:Landing limitations:Alternate airports135.397 Small transport category airplane Not applicableNot applicableperformance operating limitations135.398 Commuter category airplanes Not applicableNot applicableperformance operating limitations135.399 Small non transport category Not applicableNot applicableairplane performance operatinglimitationsSubpart J – Maintenance, Preventive Maintenance, and Alterations*135.411 135-78 Applicability Noted -------135.413 135-81 Responsibility for airworthiness(a)Airworthiness conditions;Maintenance---OperatorResponsibilityOperatorResponsibility(b)Required procedures formaintenance135.415 135-81 Service difficulty reports(operational)An approved maintenanceschedule derived from the MSG-3process and the AircraftMaintenance Manual complyingwith FAR 25.1529 and Appendix His provided to each operator.OperatorResponsibility--- OperatorResponsibilityOperatorResponsibilityOperatorResponsibility135.416 135-81 Service difficulty reports (structural) --- OperatorResponsibility135.417 135-81 Mechanical interruption summary --- OperatorreportResponsibility135.419 Approved aircraft inspection An approved maintenanceOperatorprogramschedule derived from the MSG-3 Responsibilityprocess and the AircraftMaintenance Manual complyingwith FAR 25.1529 and Appendix His provided to each operator.OperatorResponsibilityOperatorResponsibilityOperatorResponsibility135.421(a)135-70 Additional maintenancerequirementsCompliance with manufacturer’srecommended maintenanceAn approved maintenanceschedule derived from the MSG-3process and the AircraftOperatorResponsibilityOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemarkprogramsMaintenance Manual complyingwith 14 CFR Part 25.1529 andAppendix H is provided to eachoperator.(b)See note for (a)Manufacturer’s maintenance(c)program definitionNot applicableSingle engine aircraft engine(d)monitoring requirementsNot applicableSingle engine aircraft methods,(e)techniques, and practicesNot applicableSingle engine aircraft enginemaintenance records135.423 Maintenance, preventive--- Operatormaintenance, and alterationResponsibilityorganization135.425 Maintenance, preventivemaintenance, and alterationprograms--- OperatorResponsibility135.427 135-66 Manual requirements An approved maintenanceschedule derived from the MSG-3process and the AircraftMaintenance Manual complyingwith 14 CFR part 25.1529 andAppendix H is provided to eachoperator.OperatorResponsibility135.429 135-20 Required inspection personnel --- OperatorResponsibility135.431 135-60 Continuing analysis and--- OperatorsurveillanceResponsibility135.433 Maintenance and preventive ---- Operatormaintenance training programResponsibility135.435 135-82 Certificate requirements --- OperatorResponsibility135.437 Authority to perform and approve --- Operatormaintenance, preventiveResponsibilitymaintenance, and alterations135.439 Maintenance recordingrequirementsAn approved maintenanceschedule derived from the MSG-3process and the AircraftMaintenance Manual complyingwith 14 CFR part 25.1529 andAppendix H is provided to eachoperator.OperatorResponsibility135.441 Transfer of maintenance records --- OperatorResponsibility135.443 135-82 Airworthiness release or aircraft --- Operatormaintenance log entryResponsibilityFSB FindingOperatorResponsibilityNot ApplicableNot ApplicableNot ApplicableOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12Appendix 6 - HEAD-UP DISPLAY (HUD) SYSTEMSFlight crewmember training must be accomplished using a level 'C' simulator, with a daylightvisual display, or a level 'D' simulator. The FSB has determined that each pilot in commandof an aircraft equipped with a HUD system should receive a minimum of 3 hours of groundschool training followed by a minimum of 4 hours of simulator training in the left seat of alevel 'C', with a daylight visual display, or level 'D' simulator. A HUD equipped aircraft mayalso be used for in-flight training. In-flight training should consist of a minimum of 4 hours offlying in the left seat of the HUD equipped aircraft.The 3 hours of ground school training listed above is intended for pilots receiving“stand alone” training on the HUD system. A pilot who is progressing successfullythrough an initial training program that has HUD training (including all 3 elementslisted below) integrated into the curriculum, is recommended by an instructor, andsuccessfully completes the appropriate HUD proficiency check by a personauthorized by the Administrator, need not complete the 3 “stand alone” hours ofground school training.The 4 hours of simulator or aircraft in-flight training listed above is intended forpilots receiving “stand alone” training on the HUD system. A pilot who isprogressing successfully through an initial training program that has HUD training(including all 10 elements listed below) integrated into the curriculum, isrecommended by an instructor, and successfully completes the appropriate HUDproficiency check by a person authorized by the Administrator, need not complete the4 “stand alone” hours of simulator/aircraft in-flight training.The FSB recommends special training emphasis in the following areas:Ground Training:1) Crew coordination2) Crew briefings and callouts3) Duties of flying and non-flying pilotsFlight Training:1) Use of caged, uncaged and clear modes (especially in crosswind conditions)2) Use of the pitch limit indicator (PLI) during windshear escape3) Approaches to 'black hole' airports using the FPA4) Use of the acceleration cue as a potential flight path angle (FPA)5) Relationship of the glide path angle to the symbolic runway6) Use of the flare symbol as a cue in the Honeywell Head Up Guidance Display Model 2020and as guidance in the Rockwell-Collins Head Up Guidance System (HGS Model 6250)7) Approaches into the top of an undercast during daylight and night conditions.8) Recovery from unusual attitudes

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/129) TCAS resolution advisory10) Takeoff using the FPA to meet a required climb gradient.Checking requires a proficiency check conducted in a level 'C' simulator, with a daylight visualdisplay, in a level 'D' simulator, or on a HUD equipped aircraft. The proficiency check will includeat least one takeoff and departure procedure and one instrument approach and landing utilizing theHUD. The proficiency check will also include a minimum of one takeoff or missed approach and oneinstrument approach without utilizing the HUD. This is to ensure proficiency without the use of theHUD.The GV-SP, and GIV-X Head-Up Displays have been found to be functionally equivalent tothe G-V HUD. All requirements listed above apply to the GV-SP and GIV-X HUDs.HUD II“HUD II”, Rockwell-Collins Head Up Guidance System (HGS) Model 6250, utilizesa Liquid Crystal Display (LCD) which is different from the raster image on “HUD”,Honeywell Head Up Guidance Display (Model 2020). HUD II also has a largercombiner than HUD. Some of the HUD II symbology differs from HUD such as thecaged flight path vector, the non-conformal lateral deviation indicator, and theunusual attitudes. The FSB found HUD II, as well as the associated AFM change, tobe operationally suitable. Pilots transitioning from HUD to HUD II or from HUD IIto HUD should be trained on the differences using a level “A” handout. HUD IIchecking requirements are the same as those described above for HUD.

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12APPENDIX 7 – KOLLSMAN ENHANCED VISION SYSTEM (EVS)EVS meets the requirements of EFVS (Enhanced Flight Vision System) as defined in FAR 91.175.Flight crewmembers may use EVS to meet the visibility requirements of Title 14 CFR Section91.175 provided that vertical guidance with reference to an obstacle-free path is used.Flight crewmember training must include a review of Title 14 CFR Section 91.175 and areview of the associated EVS AFM system description, limitations, and procedures.Flight crewmember training must be accomplished using a level 'C' simulator, with a daylightvisual display, or a level 'D' simulator that has been qualified by the National SimulatorProgram for EVS, or the aircraft. The FSB has determined that each pilot in command of anaircraft equipped with EVS should receive a minimum of 4 hours of ground school trainingfollowed by a minimum of 2 hours of simulator training in the left seat of a level 'C', with adaylight visual display, or level 'D' simulator. An EVS equipped aircraft may also be used inlieu of a simulator for training. In-flight training should consist of a minimum of 2 hours offlying in the left seat of the EVS equipped aircraft. The flight portion of the training shouldconsist of a minimum of two (2) day and two (2) night approaches each with verticalguidance.The 4 hours of ground school training listed above is intended for pilots receiving“stand alone” training on the EVS system. A pilot who is progressing successfullythrough an initial training program that has EVS training (including all 9 elementslisted below) integrated into the curriculum, is recommended by an instructor, andsuccessfully completes the appropriate EVS proficiency check by a person authorizedby the Administrator, need not complete the 4 “stand alone” hours of ground schooltraining.The 2 hours of simulator or aircraft in-flight training listed above is intended forpilots receiving “stand alone” training on the EVS system. A pilot who is progressingsuccessfully through an initial training program that has EVS training (including all 7elements listed below) integrated into the curriculum, is recommended by aninstructor, and successfully completes the appropriate EVS proficiency check by aperson authorized by the Administrator, need not complete the 2 “stand alone” hoursof simulator/aircraft in-flight trainingThe FSB recommends special training emphasis in the following areas:Ground Training:1) Transition from EVS imagery to non-EVS, visual conditions. Maximum use should bemade of videotapes of actual EVS approaches as seen through the combiner.

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/122) Crew briefings and callouts including annunciation of published minima and operationbelow the DA(H) or MDA(H) with EVS3) Duties of flying and non-flying pilots4) Crew coordination5) Visual anomalies such as “noise” parallax, and “blooming”6) Importance of cross checking the HUD instrumentation presentations against the EVSvisual scene presentation to enable the pilot to recognize malfunctions of the groundbased ILS equipment and improper presentation of elements in the visual scene duringthe approach7) Use of barometric altitude and/or radio altitude at low heights, including temperaturecorrection if applicable.8) Importance of vertical guidance to enhance situational awareness with respect to theobstacle environment.9) Importance of ensuring descent on an obstacle-free glide path when operating belowthe MDA during non-precision approaches.Flight/Simulator Training:1) Transition from EVS imagery to non-EVS, visual conditions and runway acquisition2) Crew briefings and callouts including annunciation of published minima and operationbelow the DA(H) or MDA(H) with EVS3) Importance of the “design eye position” in acquiring the proper EVS image4) Use of on/off switch “clear” mode5) Precision and non-precision instrument approaches in both day and night conditions6) Use of caged and uncaged modes in crosswind conditions7) EVS repeater (if installed) – Imagery quality and crew coordination.Checking requires a proficiency check conducted in a level 'C' simulator, with a daylight visualdisplay, in a level 'D' simulator, that has been qualified by the National Simulator Program for EVS,or on an EVS equipped aircraft. The proficiency check will include at least one instrument approachto published minimums and landing utilizing the EVS. This check can be accomplished concurrentlywith a proficiency or competency check under 61.57, 61.58, 121.441, 135.293, or 135.297.Currency: If 61.57 (c) is being used for currency, at least one of the 6 required instrumentapproaches must be accomplished using EVS to published minimums.As a prerequisite for EVS training, pilots should have successfully completed HUD or HUD IItraining in the Gulfstream G-V Level C or D simulator, or G-V aircraft in accordance with therequirements of Appendices 3 and 6 of this report. These EVS requirements assume that a pilotentering an EVS training program is trained and proficient in the use of the HUD or HUD II.NOTE 1: This does not preclude the display of the EVS during initial HUD or HUD II training forpurposes of EVS familiarization. However, such familiarization is not creditable toward EVStraiming as specified in this Appendix.NOTE 2: The EVS is also certified for use as an aid during all phases of flight: taxi, takeoff,climb, cruise, descent and landing.

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12The GV-SP and GIV-X EVS were evaluated by the FSB and have been found to befunctionally equivalent to the G-V EVS. All requirements listed above apply to the GV-SPand GIV-X EVS.EVS II was evaluated by the FSB and has been found to be functionally equivalent to EVS.All requirements listed above apply to EVS II.

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12Appendix 8 – GIV-X OPERATING RULES COMPLIANCE CHECKLISTSerial number 4003, was utilized by the FSB to conduct its evaluation on May 3-4, 2004. 4003 was aGIV-X flight test aircraft. It enabled the FSB to determine compliance with the appropriate 14 CFRpart 91 and 135 operating requirements. The attached checklist provides the FSB’s findings on thoseoperating requirements. A FAR 125 compliance checklist was not developed for this aircraft sinceGulfstream has designed this aircraft to operate with less than 6,000 pounds payload. Since theaircraft are delivered “green” from the factory, the completion center will determine final payloadcapacity of the airplane. It may be possible that individual aircraft may be outfitted to operate inexcess of 6,000 pound payload. That operator would then have to show compliance with FAR 125requirements, unless a deviation is obtained.Any U.S. operator wishing to operate the GIV-X aircraft will have to demonstrate to the FAA that theaircraft fully complies with all applicable 14 CFR parts prior to that aircraft entering service. Thischecklist may be used by the operator to show compliance with those items listed in it.

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark* SUBPART A - GENERAL *91. 1 91-257 Applicability Noted91. 3 Responsibility and Authority of the Pilot Not applicableOperatorin CommandResponsibility91. 5 Pilot in Command Requiring More than Not applicableOperatorOne Required PilotResponsibility91. 7Civil Aircraft AirworthinessOperatorResponsibility(a)Airworthy ConditionsNotedFSB FindingOperatorResponsibilityOperatorResponsibilityOperatorResponsibility(b)Determination---91. 9Civil Aircraft Flight Manual, Marking,and Placard Requirements(a)Operating LimitationsAn FAA-approved Airplane FlightManual complying with 14 CFR Part25.1581 is provided with each aircraft.Additional compliance withoperational requirements recordedherein.OperatorResponsibilityOperatorResponsibility(b) (1)Availability of current Airplane Flight inaircraftAn FAA-approved Airplane FlightManual complying with 14 CFR Part25.1581 is provided with each aircraft.OperatorResponsibilityOperatorResponsibility(b)(2)(c)Airplane Flight Manual not requiredIdentification of aircraft in accordancewith 14 CFR Part 45Not applicableA fireproof identification platecomplying with 14 CFR Part 45 isincluded in the production airplane.Aircraft are delivered “green” byGulfstream and meet RegistrationNumber requirements whendelivered.Operatorresponsibilityat outfittingafter paint.NotApplicableNotApplicable(d)Compliance with Part 29Not applicable91. 11 Prohibition on Interference withCrewmembers--- OperatorResponsibility91. 13 Careless or Reckless Operation --- OperatorResponsibility91. 15 Dropping Objects --- OperatorResponsibility91. 17 Alcohol or Drugs --- OperatorResponsibility91. 19 Carriage of Narcotic Drugs,--- OperatorMarihuana, and Depressant orResponsibilityStimulant Drugs or Substances91. 21 Portable Electronic Devices --- OperatorResponsibilityNotApplicableOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark91. 23 91-267 Truth-in-Leasing Clause RequirementOperatorin Leases and Conditional SalesResponsibilityContractsFSB FindingOperatorResponsibility(a)(b)(c)(d)(e)Contract ContentExclusionRequirements for ContractPublic inspectionLease descriptionNotedNoted---------OperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibility91. 25 Aviation Safety Reporting Program:Prohibition Against Use of Reports forEnforcement Purposes91. 27 -91. 99* SUBPART B - FLIGHT RULES *(a)OperatorResponsibility[ Reserved ] -------91.101 Applicability Noted -------91.103Preflight ActionOperatorResponsibilityFlight under IFR---OperatorResponsibilityOperatorResponsibility(b)Take-off and landing distances An FAA-approved Airplane FlightManual complying with 14 CFR Part25.1581 is provided with each aircraft91.105 91-231 Flight Crewmembers at Stations --- Operator91.107 91-250 Use of Safety Belts, ShoulderHarnesses, and Child RestraintSystems91.109 Flight Instruction; SimulatedInstrument Flight and Certain FlightTestsNo change to the shoulder harnessinstallation from GV. Certified as a16 ‘g’ installation.ResponsibilityProper use ofthe equipmentis operatorResponsibility--- OperatorResponsibility91.111 Operating near Other Aircraft --- OperatorResponsibility91.113 Right-of-Way Rules: Except Water --- OperatorOperationsResponsibility91.115 Right-of-Way: Water Operations --- OperatorResponsibility91.117 91-233 Aircraft Speed The information on minimum safe Operatorspeed is provided in FAA-approved ResponsibilityAirplane Flight Manual91.119 Minimum Safe Altitudes: General --- OperatorResponsibility91.121 Altimeter Settings --- OperatorResponsibility91.123 91-244 Compliance with ATC Clearances and --- OperatorInstructionsResponsibility91.125 ATC Light Signals --- OperatorResponsibility91.126 91-239 Operating On or In the Vicinity of an --- OperatorAirport in Class G AirspaceResponsibility91.127 91-239 Operating On or In Vicinity of an --- OperatorAirport in Class E AirspaceResponsibilityCompliesOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark91.129 91-234 Operation in Class D Airspace --- OperatorResponsibility91.130 91-239 Operations in Class C AirspaceOperatorResponsibility(a), (b),General; Deviations---(c), (e)FSB FindingOperatorResponsibilityOperatorResponsibilityOperatorResponsibility(d)Equipment requirementsCompliance with 91.215 is outlinedbelow91.131 Operations in Class B Airspace --- OperatorResponsibility91.133 Restricted and Prohibited Areas --- OperatorResponsibility91.135 Operations in Class A Airspace --- OperatorResponsibility91.137 Temporary Flight Restrictions --- OperatorResponsibility91.138 91-270 Temporary Flight Restrictions in --- OperatorNational Disaster Areas in the State ofResponsibilityHawaii91.139 Emergency Air Traffic Rules --- OperatorResponsibility91.141 Flight Restrictions in the Proximity of --- Operatorthe Presidential and Other PartiesResponsibility91.143 Flight Limitation in the Proximity of --- OperatorSpace Flight Operations91.144 91-240 Temporary Restriction on FlightOperations During Abnormally HighBarometric Pressure Conditions91.145 Management of aircraft operations inthe vicinity of aerial demonstrationsand major sporting eventsResponsibility--- OperatorResponsibility--- OperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibility91.146-[Reserved] --- --- ----91.14991.151 Fuel Requirements or Flight in VFRConditions--- OperatorResponsibilityOperatorResponsibility91.153 VFR Flight Plan: Information Required --- OperatorResponsibilityOperatorResponsibility91.155 91-235 Basic VFR Weather Minimums --- OperatorResponsibilityOperatorResponsibility91.157 91-262 Special VFR Weather Minimums --- OperatorResponsibilityOperatorResponsibility91.159 VFR Cruising altitude or Flight Level --- OperatorResponsibilityOperatorResponsibility91.161 -[ Reserved ] -------91.16591.167 Fuel Requirements for Flight in IFRConditions--- OperatorResponsibilityOperatorResponsibility91.169 91.259 IFR Flight Plan: Information Required --- OperatorResponsibilityOperatorResponsibility91.171 VOR Equipment Check For IFROperationsDual VOR installation meets therequirement when deliveredOperatorResponsibilityOperatorResponsibility91.173 ATC Clearance and Flight PlanRequired--- OperatorResponsibilityOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark91.175 91.267 Take-off and Landing Under IFR --- OperatorResponsibility91.177 Minimum Altitudes for IFR Operations --- OperatorResponsibility91.179 IFR Cruising Altitude or Flight Level --- OperatorResponsibility91.181 Course to be Flown --- OperatorResponsibility91.183 IFR Radio Communications --- OperatorResponsibility91.185 91-211 IFR Operations: Two-way Radio --- OperatorCommunication FailureResponsibility91.187 Operations under IFR In Controlled --- OperatorAirspace: Malfunction reportsResponsibility91.189Category II and III OperationsThe aircraft is not certified forCategory II operations. This willoccur in a follow-on certification. TheFAA-approved Airplane Flight Manualwill be updated at that time.FSB FindingOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityNotDemonstrated(a)(1).(a)(2)Appropriate authorization & adequateknowledge of crewmembers---OperatorResponsibilityOperatorResponsibility(a)(3)Instrument panel and equipmentinstalledInstrument panel meets therequirements of the section.This will bedemonstratedduring theCategory IIcertificationeffort.NotDemonstrated(b)(c)-(g)Airborne equipmentApproaches, Landing, ExceptionsNoted.---OperatorResponsibilityOperatorResponsibilityOperatorResponsibility91.191 Category II Manual Gulfstream will provide a Category IIFAA-approved Airplane Flight ManualSupplement as a template forCategory II Manual91.193 Certificate of Authorization for Certain91.195 -91.199OperatorResponsibilityNotDemonstrated--- Operator NotCategory II OperationsResponsibility Applicable[ Reserved ] --- -------

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position Gulfstream FSB FindingRemark* SUBPART C - EQUIPMENT, INSTRUMENT, and CERTIFICATE REQUIREMENTS*91.201 [ Reserved ] -------91.203 91-218 Civil Aircraft: Certifications Required(a)Valid C of A, Registration Certificate.C of A is issued for each aircraftdelivered from production.---Registration isOperatorResponsibilityOperatorResponsibility(b)(c)C of A displayedFuel Tanks in the passengercompartmentNot applicableOperatorResponsibilityOperatorResponsibilityNotApplicable(d)91.205Compliance with Part 3491-251 Instrument and EquipmentRequirementsCompliance with 14 CFR Part 34 hasbeen demonstrated during TypeCertificationNotDemonstrated(a)GeneralSee BelowOperatorResponsibility(b)(c)(d)Day VFRNight VFRIFRAll equipment specified forDay VFR, as applicable to aturbine engine aircraft isincluded in the productionairplane, except for Item (12)– Pyrotechnic signal devicesare not provided.Item (13) – Crew seats only.Passenger seats to be complied withduring outfittingItem (16) - Not applicableItem (17) - Not applicableAll equipment specified for NightVFR, Items (2) thru (6) are included inthe production airplane, except for:Item (6) - Spare fuses are notprovided since all re-settable circuitsare protected by circuit breakers.All equipment specified for IFR flight,Items (2) thru (9) are included perGIV-X Product Specification.SEE:Compliancewith 91.513(B)NOTE: Thisrequires fusesfor any fusedcircuitsComplies(e)(f)Flight at and above FL240Category II OperationsDME equipment is included per theGIV-X Product Specification.All equipment as prescribed inParagraph (d) and Appendix A areprovided per the GIV-X ProductSpecification.Category II is afollow-oncertificationactivity.CompliesNotDemonstrated

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark91.207 91-265 Emergency Locator TransmittersFSB Finding(a)GeneralAn emergency locator transmitterConforming to TSO-C91A is providedas part of the production airplane.Operatingcondition,para. (a)(1) isan operatorresponsibilityOperatorResponsibility(b)LocationThe ELT is mounted on primarystructure in the aft compartment ofthe fuselage in order to minimize theprobability of damage in the event ofcrash impact.Complies(c)Battery condition---OperatorResponsibilityOperatorResponsibility(d)Periodic inspections---OperatorResponsibilityOperatorResponsibility(e)Ferrying with inoperative ELT---OperatorResponsibilityOperatorResponsibility(f)91.209Exceptions to para. 91.207(a)Aircraft LightsELT is installed in production andflight test airplanes prior to first flightOperatorResponsibilityOperatorResponsibility(a), (b),(c)91.211Position and anti-collision lightsAnchor LightsSupplemental OxygenPosition lights and anti-collision lightscomplying with 14 CFR Part 25.1381through 25.1397 and 25.1401respectively are included in theproduction airplane.Not applicableUse of theselights is anoperatorresponsibility.OperatorResponsibilityNotApplicable(a),(b)(1)GeneralA flight crew supplemental oxygensystem is included in the productionairplane. Crew oxygen masks areprovided for both pilots and observer.Passenger oxygen system to beinstalled during outfitting.OperatorResponsibilityto useequipment asrequired.OperatorResponsibility(b)(2)Pilot at Controls91.213 Inoperative Instruments andEquipment---Gulfstream has an approved MMELfor the baseline airplane. GIV-Xspecific items have been submittedfor the next FOEB meeting.OperatorResponsibilityMEL LOA isOperatorResponsibilityOperatorResponsibilityOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark91.215 91-267 ATC Transponder and AltitudeReporting Equipment and UseFSB Finding(a)Transponder performance andenvironmental requirementsTwo Honeywell Mode STransponders with ATC Modes A andC conforming to TSO-C112 areprovided in the production airplaneComplies(b), (c),(d)91.217Transponder operationsData Correspondence betweenAutomatically - Reported PressureAltitude Data and Pilot’s Reference--- Transponderoperation isan operatorresponsibilityOperatorResponsibility(a)Deactivation directed---OperatorResponsibilityOperatorResponsibility(b)(c)91.219Encoded altitude accuracyAltimeter-encoding equipmentspecificationsAltitude alerting system or device:Turbo-Jet Powered Civil AirplanesMode C altitude – production airplaneis delivered with a recent (within last30 days) air data calibration IAW 14CFR Part 91.411 and 14 CFR Part 43Conform to TSO-C10 and C88Periodictesting andcalibration isan operatorresponsibilityCompliesComplies(a)Operational Requirement for system---OperatorResponsibilityOperatorResponsibility(b)Altitude Alerting System RequirementsThe production airplane is deliveredwith an approved altitude alertingsystem meeting the requirements of(b)Complies(c),(d)91.221Operational ProceduresTraffic Alert and Collision AvoidanceSystem Equipment and Use---OperatorResponsibilityOperatorResponsibility(a)Requirement for an approved TCASA Traffic Alert and CollisionAvoidance System (TCAS II/ACAS II)is provided in the production airplane.Complies(b)TCAS: operation required--- OperatorResponsibilityOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark91.223Terrain Awareness and WarningSystemFSB Finding(a)(b)A/C manufactured after March 29,2002A/C manufactured on or before March29, 2002A Class A TAWS (compliant withTSO C151) is provided in theproduction airplane.Not applicableCompliesNotApplicable(c)AFMAll applicable information isprovided in the FAA-approvedAirplane Flight ManualNotDemonstrated(d)ExceptionsNot applicableNotApplicable91.224 -[ Reserved ] --- -------91.299* SUBPART D - SPECIAL FLIGHT OPERATIONS*91.301 [ Reserved ] --- -------91.303 91-227 Aerobatics Flight --- Operator OperatorResponsibility Responsibility91.305 Flight Test Areas --- Operator OperatorResponsibility Responsibility91.307 91-268 Parachutes and Parachuting Not applicable NotApplicable91.309 91-227 Towing: Gliders --- Operator OperatorResponsibility Responsibility91.311 Towing: Other than under § 91.309 --- Operator OperatorResponsibility Responsibility91.313Restricted Category Civil Aircraft:Operating Limitations(a); (b);(c); (d);(e); (f)General---OperatorResponsibilityOperatorResponsibility(g)Shoulder harness approvalNot applicable. Part 23 airplanes onlyNotApplicable91.315 Limited Category Civil Aircraft:--- Operator OperatorOperating LimitationsResponsibility Responsibility91.317 91-212 Provisionally Certificated Civil Aircraft: Not applicable.Operator OperatorOperating LimitationsResponsibility Responsibility91.319 Aircraft Having Experimental--- Operator OperatorCertificates: Operating LimitationsResponsibility Responsibility91.321 Carriage of Candidates in Federal --- Operator OperatorElectionsResponsibility Responsibility91.323 91-253 Increased Maximum Certificated Not applicable -------Weights for Certain AirplanesOperated in Alaska91.325 Primary Category Aircraft: Operating Not applicable -------Limitations91.326-[ Reserved ] --- -------91.399* SUBPART E - MAINTENANCE, PREVENTIVE MAINTENANCE, and ALTERATIONS *

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position Gulfstream FSB FindingRemark91.401 Applicability Noted -------91.403 91-267 General(a) (b)Airworthy conditions; Maintenance---OperatorResponsibilityOperatorResponsibility(c)91.405Required proceduresMaintenance RequiredAn approved maintenance schedulederived from the MSG-3 process andan Aircraft Maintenance Manualcomplying with 14 CFR Part 25.1529and Appendix H is provided to eachoperator upon delivery of the airplane.OperatorResponsibility(a); (b);(d)Discrepancies; RecordsOperatorResponsibilityOperatorResponsibility(c)Inoperative instruments91.407 Operation after Maintenance,Preventive Maintenance, rebuilding, oralterationThe aircraft will have an approvedMMEL. Approval of applicable MEL isthe operator’s responsibility.--- OperatorResponsibility91.409 91-267 Inspections An approved maintenance schedulederived from the MSG-3 process andan Aircraft Maintenance Manualcomplying with 14 CFR Part 25.1529and Appendix H is provided to eachoperator.91.410 91.266 Special maintenance programrequirements91.411 Altimeter System and AltitudeReporting Equipment Tests andInspectionsNot applicableThe Airplane Maintenance Manualincludes the tests and inspectionsrequired by 14 CFR Part 43 andappendices. The 14 CFR Part 43tests and inspections are conductedfor each aircraft prior to C of A.Operatorresponsible foraccomplishingrequiredmaintenanceOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityNotApplicableOperatorResponsibility91.413 91-267 ATC Transponder Tests andInspectionsThe Airplane Maintenance Manualincludes the tests and inspectionsrequired by 14 CFR Part 43 andappendices. The 14 CFR Part 43tests and inspections are conductedfor each aircraft prior to C of A.Operatorresponsibilityafter airplaneis in service.91.415 Changes to aircraft inspection program --- OperatorResponsibilityOperatorResponsibilityOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark91.417Maintenance recordsFSB Finding(a), (b),(c)Documents requirementsAn approved maintenance schedulederived from the MSG-3 process andthe Airplane MaintenanceManual complying with 14 CFR Part25.1529 and Appendix H is providedto each operator.OperatorResponsibilityOperatorResponsibility(d)Fuel tank installationNot applicable, since the fuel tank isnot installed within the passengercompartment/baggage compartment91.419 Transfer of maintenance records --- OperatorResponsibilityNotApplicable91.421 Rebuilt engine maintenance records Not applicable -------91.423 -[ Reserved ] --- -------91.499* SUBPART F - LARGE AND TURBINE-POWERED MULTIENGINE AIRPLANES*91.501 Applicability Noted. Operator91.503Flying Equipment and OperatingInformationResponsibilityOperatorResponsibilityOperatorResponsibility(a)(1)FlashlightsTwo rechargeable Maglite flashlightsare provided as basic aircraftequipment, one for each pilot’sstation.Workingcondition isresponsibilityof operator.OperatorResponsibility(a)(2)Cockpit checklistChecklists are provided in theFAA-approved Airplane Flight Manual/ Operating Manual / QRHOperatorResponsibilityNotDemonstrated(a)(3) &(a)(4)Aeronautical charts---OperatorResponsibilityOperatorResponsibility(a)(5)(b), (c)(d)One engine inoperative climbperformance dataCockpit checklist contentsUse of data by crew91.505 Familiarity with operating limitationsand emergency equipment91.507 Equipment requirements: Over-the-topor night VFR operationsThe FAA-approved Airplane FlightManual and Operating Manualinclude the required data.The FAA-approved Airplane FlightManual contains all requiredchecklists.---An FAA-approved Airplane FlightManual complying with 14 CFR Part25.1581 is provided with the airplaneat delivery.All equipment specified for IFR flightand Night VFR is included in theproduction airplane.Operatorresponsibilityto use the dataOperatorresponsibilityOperatorResponsibilityOperatorResponsibilityOperatorresponsible foroperableequipmentNotDemonstratedNotDemonstratedOperatorResponsibilityOperatorResponsibilityOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark91.509 Survival equipment for overwater The aircraft is equipped forOperatoroperationsExtended Over Water Operations for Responsibilitythe crew only as a productionairplane. The airplane is equipped91.51191-249 Radio equipment for overwateroperationsfor passengers during outfitting.---NotedFSB Finding.509 (b)(3) maybe contrary toG/as stated in.205(a)(b)Equipment requirementsThe production airplane meets theequipment requirements.NotDemonstrated(c)(d)Equipment exclusions---OperatorResponsibilityOperatorResponsibility(e)Definition of “shore”---Noted(f)91.513Equipment requirements in specificremote oceanic areasEmergency Equipment---OperatorResponsibilityOperatorResponsibility(a)(b)GeneralEquipment requirementsNotedThe production airplane is equippedwith a fire extinguisher in the cockpit,smoke goggles and life jackets forthe 2 pilots and observers, and aportable oxygen bottle with full facemask. The equipment meets thisparagraph.OperatorResponsibilityNotDemonstratedNote: If HalonF/E is used forclass “A” fires, itmust bedemonstrated(c)(1)(2)Fire extinguishersA HALON fire extinguisher isinstalled in the cockpit as Part of theproduction airplane.NotDemonstrated(c)(3)(4)Fire extinguishersCabin fire extinguishers are installedduring outfitting.OperatorResponsibilityNotDemonstrated(d)First Aid kitFirst Aid Kits are installed during theoutfitting processTheemergencymedical kit isoperatorresponsibilityNotDemonstrated(e)Crash axeNot applicableOperatoroptionNot Applicable(f)MegaphonesNot applicableOperatoroption91.515 Flight altitude rules --- OperatorResponsibilityNot ApplicableOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark91.517Passenger InformationFSB Finding(a)Smoking and seat-belt signsSmoking and seat-belt signs areinstalled during the outfitting processOperatorResponsibilityOperatorResponsibility(b)Oral notification if no signs provided---OperatorresponsibilityOperatorResponsibility(c)No smoking allowed while “NoSmoking” signs lighted---OperatorresponsibilityOperatorResponsibility(d)(e)Passenger compliance with signs and ---instructions91.519 91-231 Passenger briefing The applicable placards and lightedpassenger information signs areinstalled during outfitting. A videoand printed cards are also providedto the operator at delivery.91.521Shoulder HarnessOperatorResponsibilityOral briefingis OperatorResponsibilityOperatorResponsibilityOperatorResponsibility(a)(1)(2)(b)(1)(2)Shoulder Harness – Flight DeckShoulder Harness – Flight AttendantSeat in CabinThe 2 pilot seats and observer seatinstalled in the production airplanemeet these requirements.If an operator chooses to install sucha seat(s), it will be installed duringoutfitting and comply.OperatorOption andResponsibility91.523 Carry-on baggage Not applicable -------91.525Carriage of CargoCompliesNotDemonstrated(a)Carriage of cargo - RequirementsThe baggage compartment is aClass B compartment and meets therequirements of (a)(i) thru (v)OperatorResponsibility(b)91.527Accessibility of compartments for fireextinguishingOperating in Icing ConditionsThe aft baggage compartment isclassified as a Class B cargocompartmentAFMEmergencyproceduresmeet thisrequirementNotDemonstrated(a)Take-off with contaminated surfaces---OperatorResponsibilityOperatorResponsibility(b), (c)IFR/VFR flight into known orforecasted icing conditionsThe GIV-X is a transport airplaneand is certified for FIKIOperatorresponsibilityOperatorResponsibility(d)Forecast icing conditions relief---OperatorResponsibility91.529 Flight Engineer requirements --- OperatorResponsibility91.531 Second in command requirements --- OperatorResponsibility91.533 Flight attendant requirements Not applicable. OperatorResponsibilityOperatorResponsibilityNot ApplicableOperatorResponsibilityOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position Gulfstream FSB FindingRemark91.535 Stowage of food, beverage, andpassenger service equipment during--- OperatorResponsibilityOperatorResponsibilityaircraft movement on the surface,takeoff, and landing91.536 -[ Reserved ] --- -------91.599*SUBPART G - ADDITIONAL EQUIPMENT and OPERATING REQUIREMENTS FOR LARGE and TRANSPORTCATEGORY AIRCRAFT *91.601 Applicability Noted -------91.603 Aural Speed Warning Device The production airplane complies. Operator91.60591-256 Transport Category Civil AirplaneWeight LimitationsResponsibility(a)Conditions for aircraft certificatedbefore October 1, 1958Not applicableNot Applicable(b)Maximum take-off and landingweights for airfield elevation, ambienttemperature, wind and runwaygradient.91.607 Emergency exits for airplanescarrying passengers for hire.91.609 91-228 Flight Recorders and Cockpit VoiceRecordersThe FAA-approved Airplane FlightManual and Weight and BalanceManual contains all data necessary toenable the operator to comply with thisrequirement. The Operating Manualcontains flight-planning data to enablecomputation of fuel burned fromdeparture to destination or alternateairport. Additionally, the productionairplane is equipped with an on-boardflight-planning computer for takeoff, enroute, and landing computations toassist the crew in performing thesecalculations.The aircraft is equipped with four TypeIV over wing exits (two on each side).OperatorResponsibilityOperatorResponsibilityComplies(a)-(b)(c)GeneralRequirement for flight recorder---The airplane is equipped with a digitalflight data recorder meeting therequirements of Part 91 in production.The 14 CFR Part 135 eighty-eight (88)parameter DFDR will be certified as afollow-on certification effort.OperatorResponsibilityOperatorResponsibilityComplies-Part91/135NotDemonstrated(d)(e), (f)Flight recorder operationRequirement for cockpit voicerecorderThe flight recorder installed in theproduction airplane meets thisrequirement.The cockpit voice recorder installed inthe production airplane meets theserequirements.Complies Part91/135NotDemonstratedNotDemonstrated(g)Action required following accident orincident – NTSB report and records---OperatorResponsibilityOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark91.611 Authorization for ferry flight with one Not applicableengine inoperativeFSB FindingNot Applicable91.613 Materials For Compartment Interiors To be addressed during the outfittingby STCOperatorResponsibility91.615 -[ Reserved ] -------91.699*SUBPART H - FOREIGN AIRCRAFT OPERATIONS AND OPERATIONS OF US REGISTERED CIVIL AIRCRAFT OUTSIDE OFTHE UNITED STATES; AND RULES GOVERNING PERSONS ON BOARD SUCH AIRCRAFT*91.701 Applicability Noted OperatorResponsibilityOperatorResponsibility91.702 Persons on board --- OperatorResponsibilityOperatorResponsibility91.703 Operations of civil aircraft of U.S.registry outside of the United States--- OperatorResponsibilityOperatorResponsibility91.705 Operations within airspace designatedas Minimum Navigation PerformanceSpecification Airspace--- OperatorResponsibilityOperatorResponsibility91.706 Operations within airspace designatedas Reduced Vertical SeparationMinimum Airspace--- OperatorResponsibilityOperatorResponsibility91.707 Flights between Mexico or Canada andthe United States--- OperatorResponsibilityOperatorResponsibility91.709 Operations to Cuba --- OperatorResponsibilityOperatorResponsibility91.711 Special rules for foreign civil aircraft --- OperatorResponsibilityOperatorResponsibility91.713 Operation of civil aircraft of Cubanregistry--- OperatorResponsibilityOperatorResponsibility91.715 Special flight authorizations for foreigncivil aircraft--- OperatorResponsibilityOperatorResponsibility91.717 -[ Reserved ] --- -------91.799* SUBPART I - OPERATING NOISE LIMITS*91.801 Applicability: Relation to Part 36 Noted -------91.803 Part 125 operations: Designation ofapplicable regulationsNotedNotApplicable91.805 Final compliance The production airplane is certified to14 CFR Part 36 Stage 3 requirementsas noted in the FAA-approvedAirplane Flight Manual.91.807Phased compliance under Parts 121,125, and 135: Subsonic airplanesComplies(a)GeneralNoted(b)Compliance schedulesThe production airplane is certified to14 CFR Part 36 Stage 3 requirementsas noted in the FAA-approvedAirplane Flight Manual.Complies(c)Apportionment of airplanes--- OperatorResponsibilityOperatorResponsibility91.809 Replacement airplanes --- OperatorResponsibilityNotApplicable

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark91.811 Service to small communities--- Operatorexemption: Two engine, subsonicResponsibilityairplanes91.813 Compliance plans and status: USoperations of subsonic airplanesThe production airplane is certified to14 CFR Part 36 Stage 3 requirementsas noted in the FAA-approvedAirplane Flight Manual.FSB FindingNotApplicableComplies91.815 Agricultural and fire fighting airplanes: Not applicable -------Noise operating limitations91.817 Civil aircraft sonic boom Not applicable -------91.819 Civil supersonic airplanes that do not Not applicable -------comply with Part 3691.821 Civil supersonic airplanes: noise limits Not applicable -------91.823 -[ Reserved ] --- -------91.84991.851 Definitions Noted -------91.853 Final compliance: civil subsonicairplanesCompliesThe production airplane is certified to14 CFR Part 36 Stage 3 requirementsas noted in the FAA-approvedAirplane Flight Manual.91.855 Entry and non-additional rule The production airplane is certified to14 CFR Part 36 Stage 3 requirementsas noted in the FAA-approvedAirplane Flight Manual.91.857 Stage 2 operations outside of the 48contiguous United States andauthorization for maintenance91.859 Modification to meet Stage 3 noiselevelsThe production airplane is certified to14 CFR Part 36 Stage 3 requirementsas noted in the FAA-approvedAirplane Flight Manual.The production airplane is certified to14 CFR Part 36 Stage 3 requirementsas noted in the FAA-approvedAirplane Flight Manual.CompliesNotApplicableNotApplicable91.861 Base level --- OperatorResponsibilityNotApplicable91.863 Transfers of Stage 2 airplanes withbase level--- OperatorResponsibilityNotApplicable91.865 Phased compliance for operators withbase level--- OperatorResponsibilityNotApplicable91.867 91-252 Phased compliance for new entrants --- OperatorResponsibilityNotApplicable91.869 Carry-forward compliance --- OperatorResponsibilityNotApplicable91.871 Waivers from interim compliancerequirements--- OperatorResponsibilityNotApplicable91.873 Waivers from final compliance --- OperatorResponsibilityNotApplicable91.875 Annual progress reports --- OperatorNotApplicableResponsibility91.877 Annual reporting of Hawaiianoperations--- OperatorResponsibilityNotApplicable91.879 -[ Reserved ] --- -------91.899* SUBPART J - WAIVERS *91.901 [ Reserved ] --- -------91.903 Policy and procedures Noted OperatorResponsibilityOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position Gulfstream FSB FindingRemark91.905 91-227 List of rules subject to waivers Noted OperatorResponsibilityOperatorResponsibility91.907 -[ Reserved ] --- -------91.999* SUBPART A - GENERAL *135. 1 135-58 ApplicabilityNotedOperatorResponsibilityOperatorResponsibility(a)General---(b)(c)[Reserved]Sightseeing operator defined------(d)Unscheduled repair requirements ---135. 2 135-66 Compliance schedule for operators --- Operatorthat transition to part 121 of thisResponsibilitychapter; certain new entrant operators135. 3 135-65 Rules applicable to operations subject --- Operatorto this partResponsibility135. 7 135-58 Applicability of rules to unauthorized --- OperatoroperatorsResponsibility135. 12 Previously trained crewmembers --- OperatorResponsibility135. 19 Emergency operations --- OperatorResponsibility135. 21 135-66 Manual requirements --- OperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityNotApplicableOperatorResponsibilityOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark135. 23 135-58 Manual contentsOperatorResponsibility(a)Personnel roster---FSB FindingOperatorResponsibility(b)Weight and balanceA FAA-approved weight and balancemanual is provided with each aircraftOperatorResponsibility(c)(d)(e)(f)(g)Operations specificationsAccident notification proceduresAircraft airworthiness notification topilot in commandProcedures for reporting inflightmaintenance irregularitiesNotification of corrective actions tomaintenance irregularities---------------OperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibility(h)Pilot in command procedures to obtainunscheduled maintenance---OperatorResponsibility(i)(j)(k)(l)(m)Minimum Equipment ListRefueling proceduresPassenger briefing proceduresFlight locating proceduresCompliance with emergencyproceduresA GIV-X Master Minimum EquipmentList has been submitted to the FAA------------OperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibility(n)(o)(p)(q)Pilot enroute qualification proceduresApproved aircraft inspection programProcedures for hazardous materialhandlingEvacuation procedures for assistinganother person to an exit during anemergency---An MSG 3 Maintenance Programhas been developed by Gulfstreamand approved by the FAA------OperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibility(r)Other procedure and policyinstructions---OperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark135. 25 135-66 Aircraft requirementsOperatorResponsibility(a)(b)(c)Registration and airworthinesscertificateAircraft usageAircraft usage durationAircraft is delivered with appropriatedocumentation------FSB FindingOperatorResponsibilityOperatorResponsibilityOperatorResponsibility(d)Operation in common carriage---OperatorResponsibility135. 41 Carriage of narcotic drugs, marihuana,and depressant or stimulant drugs orsubstances135. 43 Crewmember certificates: Internationaloperations* SUBPART B – FLIGHT OPERATIONS *--- OperatorResponsibility--- OperatorResponsibilityOperatorResponsibilityOperatorResponsibility135. 61 General Noted -------135. 63 135-52 Record keeping requirements --- OperatorResponsibilityOperatorResponsibility135.64 135-66 Retention of contracts andamendments: Commercial operatorswho conduct intrastate operations forcompensation or hire--- OperatorResponsibilityOperatorResponsibility135.65 Reporting mechanical irregularities --- OperatorResponsibility135.67 135-1 Reporting potentially hazardous --- Operatormeteorological conditions andResponsibilityirregularities of communications ornavigation facilities135.69 Restriction or suspension ofoperations: Continuation of flight in anemergency--- OperatorResponsibility135.71 135-32 Airworthiness check --- OperatorResponsibility135.73 Inspections and tests --- OperatorResponsibility135.75 Inspectors credentials: admission to --- Operatorpilots’ compartment: ForwardResponsibilityobserver’s seat135.77 Responsibility for operational control --- OperatorResponsibility135.79 Flight locating requirements --- OperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark135.81Informing personnel of operationalOperatorinformation and appropriate changesResponsibilityFSB FindingOperatorResponsibility(a)(b)(c)(d)Certificate holder must make available:Airman’s Information Manual orequivalent14 CFR Parts 135 and 91Aircraft equipment manuals andAircraft Flight ManualFor foreign operations, theInternational Flight Information Manualor equivalent------Installed-equipment manuals andFAA-approved Airplane Flight Manualprovided with aircraft---OperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibility135.83(a)Operating information requiredPublications accessible in cockpitA normal, abnormal, and emergencyprocedures checklists and theinformation on one-engine-inoperativeclimb performance is provided inFAA-approved Airplane Flight ManualOperatorResponsibilityOperatorResponsibilityOperatorResponsibility(b)(c)Cockpit checklist requirementsEmergency procedures checklist135.85 Carriage of persons withoutcompliance with the passengercarryingprovisions of this part135.87Carriage of cargo including carry-onbaggage(a)(b)(c)(d)(e)Approved cargo rack or binSecured by approved meansSpecificationsUnder-seat stowageCargo compartment fire extinguishingrequirements--- OperatorResponsibilityA Class B baggage compartment islocated at the aft portion of thepressure vessel and additionalstorage compartments are providedduring outfitting using customer’sspecificationsOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibility135.89 Pilot requirements: Use of oxygen The normally pressurized aircraft is Operator Operator

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemarkequipped with two 115 cubic feet Responsibility(a)Unpressurized aircraftoxygen cylinders plumbed into thesupplemental oxygen system(b)Pressurized aircraft135.91 135-60 Oxygen for medical use by passengers A medical oxygen system may be Operatorinstalled in the aircraft duringResponsibility(a)Installation and maintenanceoutfitting at customer’s requestrequirements(b)(c)(d)(e)135.93(a)(b)(c)(d)(e)(f)Smoking restrictionsPersonnel qualificationsExceptionException reporting135-68 Autopilot: Minimum altitudes for useMinimum enroute altitudeDuring ILS approachILS in degraded weatherUse to touchdownUse during takeoff and initial climbNot applicable to rotorcraftMinimum altitude for autopilot usageis defined in limitations section ofFAA-approved Airplane Flight ManualOperatorResponsibility135.95 Airmen: Limitations on use of services --- OperatorResponsibility135.97 Aircraft and facilities for recent flight --- OperatorexperienceResponsibility135.99Composition of flight crewFAA-approved Airplane Flight Manual Operatorspecifies a minimum of two flight Responsibilitycrewmembers: pilot and copilot(a)Minimum flight crew per Aircraft FlightManual and 14 CFR Part 135FSB FindingResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityNotApplicableOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibility(b)Second in command requirementOperatorResponsibility135.100 Flight crewmember duties --- Operator OperatorResponsibility Responsibility135.101 Second in command required under --- Operator OperatorIFRResponsibility Responsibility135.103 [Reserved] -------135.105 135-58 Exception to second in command FAA-approved Airplane Flight Manual Operator Operatorrequirement: Approval for use of specifies a minimum of two flight Responsibility Responsibilityautopilot systemcrewmembers: pilot and copilot(a)(b)(c)Operations during VFRRequest for amendmentSpecifications for amendment135.107 Flight attendant crewmemberrequirement--- OperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark135.109 Pilot in command or second in--- Operatorcommand: Designation requiredResponsibility135.111 Second in command required in --- OperatorCategory II operationsResponsibility135.113 Passenger occupancy of pilot seat FAA-approved Airplane Flight Manual Operatorspecifies a minimum of two flight Responsibilitycrewmembers: pilot and copilot135.115 Manipulation of controls --- OperatorResponsibility135.117 135-44 Briefing of passengers before flight --- OperatorResponsibility135.119 Prohibition against carriage of--- OperatorweaponsResponsibility135.120 135-73 Prohibition on interference with --- OperatorcrewmembersResponsibility135.121 Alcoholic beverages --- Operator135.122 Stowage of food, beverage, andpassenger service equipment duringaircraft movement on the surface,takeoff, and landing135.123 Emergency and emergency evacuationdutiesResponsibility--- OperatorResponsibilityFSB FindingOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibility--- OperatorResponsibility135.125 Airplane security --- OperatorResponsibility135.127 135-76 Passenger information requirements --- Operatorand smoking prohibitionsResponsibility135.128 135-62 Use of safety belts and child--- Operatorrestraining systemsResponsibility135.129 135-60 Exit seating --- OperatorResponsibility* SUBPART C – AIRCRAFT AND EQUIPMENT *135.141 Applicability Noted Operator135.143(a)(b)135-22 General requirementsGeneralRequired instruments and equipmentin operable conditionNotedAll instruments and equipmentincluded as part of the productionairplaneOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityResponsibilityOperatorResponsibilityOperatorResponsibility(c)ATC transponder equipmentTwo ATC transponders included aspart of the production airplane andmeet applicable TSO conditions135.144 135-73 Portable electronic devices --- OperatorResponsibility135.145 Aircraft proving tests --- Operator135.47 Dual controls required Airplane is produced with dual flightcontrols under 14 CFR Part 25ResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityComplies

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark135.149 135-38 Equipment requirements: GeneralOperatorResponsibility(a)Sensitive altimeterSensitive altimeter is included aspart of the production airplaneFSB FindingOperatorResponsibility(b)(c)Carburetor heating or deicingequipmentA third gyroscopic bank-and-pitchindicatorNot applicableThird gyroscopic bank-and-pitchindicator is included as part of theproduction airplaneNot ApplicableComplies(d)[Reserved]---(e)Any other equipment FAA requires135.150 Public address and crewmemberinterphone systems135.151135-60 Cockpit voice recordersNotedFAA-approved Airplane FlightManual limits passenger load to 19peopleOperatorResponsibilityOperatorResponsibilityNot ApplicableCompliesPart 91/135(a)ApplicabilityA FAA-approved cockpit voicerecorder is included as part of theproduction airplaneNotDemonstrated(b)Multi-engine, turbine-powered airplanehaving 20 to 30 passenger seatsFAA-approved Airplane FlightManual limits passenger load to 19peopleNot Applicable(c)Procedures following accident orincident---OperatorResponsibility(d)Requirements for recording from boomor mask microphoneInstalled CVR records theuninterrupted audio signal from aboom or mask microphone inaccordance with 14 CFR Part25.1457(c)(5)Complies(e)Recording duration requirementsInstalled CVR retains at least 30minutes of audio recordingComplies

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark135.152 135-69 Flight recorders(a)ApplicabilityA FAA-approved Flight DataRecorder meeting the eighty-eightparameter requirement of 14 CFR135.152 will be a follow-oncertification effort.FSB FindingCompliesPart 91/135NotDemonstrated(b)(c)(d)(e)(f)(g)(h)Multi-engine, turbine-powered airplanehaving 20 to 30 passenger seatsContinuous operation requirementsRecorded data retention requirementsProcedures following accidentRequirements with respect to aircraftmanufacture dateDevice to assist in underwater locatingOperational parametersFAA-approved Airplane Flight Manuallimits passenger load to 19 peopleSee note for (a)See note for (a)See note for (a)See note for (a)See note for (a)See note for (a)NotDemonstratedNotDemonstratedNotDemonstratedNotDemonstratedNotDemonstratedNotDemonstratedNotDemonstrated(i)(j)Parameters for turbine-poweredairplanes having 20 to 30 passengerseats and manufactured after August18, 2000Parameters for turbine-poweredairplanes having 20 to 30 passengerseats and manufactured after August19, 2000FAA-approved Airplane Flight Manuallimits passenger load to 19 peopleFAA-approved Airplane Flight Manuallimits passenger load to 19 peopleNot applicableNot ApplicableNot Applicable(k)Exception to requirements fordeHavilland DHC-6Not Applicable

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark135.153 135-75 Ground proximity warning systemOperatorResponsibility(a)ApplicabilityA FAA-approved enhanced groundproximity warning system is includedas part of the production airplaneFSB FindingComplies(b)[Reserved]---(c)Airplane Flight Manual requirementsFAA-approved Airplane Flight Manualincludes operational procedures forenhanced ground proximity warningsystemComplies(d)Operation requirements---(e)Deactivation requirements---(f)135.154Expiration of requirementTerrain awareness and warningsystemNotedOperatorResponsibility(a)Airplanes manufactured after March29, 2002A FAA-approve terrain awarenesswarning system meeting therequirements for Class A equipmentin TSO-C151 is included as part ofthe production airplaneComplies(b)Airplanes manufactured on or beforeMarch 29, 2002---(c)135.155(a)(b)Airplane Flight ManualFire extinguishers: Passenger-carryingaircraftType and quantity of hand fireextinguisher extinguishing agentOne hand fire extinguisher convenientand located on flight deckFAA-approved Airplane Flight Manualincludes operational procedures forenhanced ground proximity warningsystemExtinguishing agent (halon) in flightdeck hand fire extinguisher is suitablefor all fires likely to occurA flight deck hand fire extinguisher isincluded as part of the productionairplane.OperatorResponsibilityCompliesNote: IfHALON F/E isused for class“A” fires, itmust bedemonstratedNotDemonstrated(c)One hand fire extinguisher convenientand located in passenger compartmentAt least one hand fire extinguisher ismounted in the passengercompartment at a convenient locationduring outfittingNotDemonstrated

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark135.157Oxygen equipment requirementsOperatorResponsibilityFSB Finding(a)(b)(c)135.158(a)Unpressurized aircraftPressurized aircraftSystem operation135-33 Pitot heat indication systemsApplicabilityThe normally pressurized aircraft isequipped with two 115 cubic feetoxygen cylinders plumbed into thesupplemental oxygen system,providing oxygen to crew and, uponaircraft outfitting, passengersSee note for (a)Oxygen system quantity monitoring isthrough gauges on flight deck, threeflight deck oxygen regulating systemsreadily allow monitoring andadjustmentsA pitot heat system with indicationscertified in accordance with FAR 25 isincluded as part of the productionairplaneOperatorResponsibilityOperatorsResponsibilityNotDemonstratedCompliesComplies(b)135.159(a)Extension135-38 Equipment requirements: Carryingpassengers under VFR at night orunder VFR over-the-top conditionsGyroscopic rate-of-turn indicator---All equipment required by this sectionare included as part of the aircraftproduced under GIV-X ProductSpecificationOperatorResponsibilityComplies(b)Slip skid indicatorComplies(c)Gyroscopic bank-and-pitch indicatorComplies(d)Gyroscopic direction indicatorComplies(e)GeneratorComplies(f)Night flight requirementsComplies(g)(h)Continuous in-flight electrical loaddefinedHelicopter requirementsNot applicableCompliesNotApplicable

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark135.161Radio and navigational equipment:OperatorCarrying passengers under VFR atResponsibilitynight or under VFR over-the-top(a)Two-way radio communication withground facilities 25 miles awayAll radio and navigation equipmentrequired by this section are includedas part of the aircraft produced underGIV-X Product SpecificationFSB FindingCompliesCompliesComplies(b)VFR over-the-top requires ability toreceive radio signals from groundfacilityComplies(c)VFR at night requires ability to receiveradio signals from ground facilityComplies135.163(a)(b)135-73 Equipment requirements: Aircraftcarrying passengers under IFRVertical speed indicatorFree-air temperature indicatorAll equipment and applicablerequirements of this section areincluded as part of the aircraftproduced under GIV-X ProductSpecificationOperatorResponsibilityCompliesComplies(c)Heated pitot tube for each airspeedindicatorComplies(d)e)(f)Power failure warning device forgyroscopic instrumentsAlternate source of static pressureSingle-engine aircraft requirementsCompliesComplies(g)Multi-engine aircraft requirementsComplies(h)(i)135.165(a)Two independent sources of energy,each of which is able to drive allrequired gyroscopic instrumentsContinuous inflight electrical loaddefined135-61 Radio and navigational equipment:Extended overwater or IFR operationsSpecifications, 10 passenger seats ormoreAll radio and navigation equipmentrequired by this section are includedas part of the aircraft produced underGIV-X Product Specification, with theexception of headsetsOperatorResponsibilityCompliesCompliesComplies(b)Specifications, other aircraft thanspecified in (a)Complies(c)Independent receiver definedComplies(d)FAA consideration of long-rangecommunications and navigationequipment135.167 135-49 Emergency equipment: Extendedoverwater operations--- OperatorResponsibilityCompliesOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark135.169 135-55 Additional airworthiness requirements Aircraft certified to 14 CFR Part 25 Operatorrequirements, equipment required by Responsibilitythis section are included as part ofthe aircraft produced under GIV-XProduct Specification135.170 135-56 Materials for compartment interiors Materials used in flight deck arecertified to 14 CFR Part 25.853standards, compartment materialsare per an STC and resolved duringoutfitting135.171Shoulder harness installation at flightcrewmember stationsOperatorResponsibilityOperatorResponsibilityFSB FindingOperatorResponsibilityOperatorResponsibilityComplies(a)Approved shoulder harnessFAA-approved shoulder harness foreach flight crewmember station isinstalled as part of the aircraftproduced under GIV-X ProductSpecificationOperatorResponsibility(b)135.173Use of shoulder harness135-60 Airborne thunderstorm detectionequipment requirements---OperatorResponsibilityOperatorResponsibility(a)ApplicabilityDigital airborne weather radarequipment is standard equipmentComplies(b)(c)Helicopter operationsFlight under IFR or night VFRNot applicable---NotApplicable(d)Procedures for Equipment failureenroute---OperatorResponsibility(e)(f)135.175(a)Exceptions for certain locationsAlternate electrical power supply notrequiredAirborne weather radar equipmentrequirementsApplicability---NotedDigital airborne weather radar isequipment is standard equipmentOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityComplies(b)(c)Flight under IFR or night VFRProcedures for Equipment failureenroute------OperatorResponsibilityOperatorResponsibility(d)Exceptions for certain locations---OperatorResponsibility(e)Alternate power supply not requiredNotedOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark135.177 135-80 Emergency equipment requirements FAA-approved Airplane Flight Manual Operatorfor aircraft having a passenger seating limits passenger load to 19 people Responsibilityconfiguration of more than 19passengers135.178 Additional emergency equipment FAA-approved Airplane Flight Manual Operatorlimits passenger load to 19 people Responsibility135.179 135-60 Inoperable instruments and equipment A Master Minimum Equipment List Operator135.180135-54 Traffic Alert and Collision AvoidanceSystemhas been developed by the FAAResponsibilityOperatorResponsibilityFSB FindingNotApplicableOperatorResponsibilityOperatorResponsibility(a)ApplicabilityA FAA-approved TCAS II/ACAS IIsystem is included as part of theproduction airplaneComplies(b)Airplane Flight Manual requirements135.181 135-70 Performance requirements: Aircraftoperated over-the-top or in IFRconditions135.183 Performance requirements: LandFAA-approved Airplane Flight Manualincludes operational procedures fortraffic alert and collision avoidancesystemFAA-approved Airplane Flight Manualincludes applicable performance dataOperatorResponsibilityCompliesCompliesFAA-approved Airplane Flight Manual Operator Compliesaircraft operated over waterincludes applicable performance data Responsibility135.185 Empty weight and center of gravity:Currency requirementA FAA-approved weight and balancemanual is provided with each aircraft,OperatorResponsibilityOperatorResponsibilityfinal weight and balance informationprovided upon completion of outfitting* SUBPART D – VFR/IFR OPERATING LIMITATIONS AND WEATHER REQUIREMENTS *135.201 Applicability Noted ------135.203 VFR: Minimum altitudes --- OperatorResponsibilityOperatorResponsibility135.205 135-41 VFR: Visibility requirements --- OperatorResponsibilityOperatorResponsibility135.207 VFR Helicopter surface referencerequirementsNot applicableOperatorResponsibilityOperatorResponsibility135.209 VFR: Fuel supply --- OperatorResponsibilityOperatorResponsibility135.211 135-32 VFR: Over-the-top carryingpassengers: Operating limitations--- OperatorResponsibilityOperatorResponsibility135.213 135-60 Weather reports and forecasts --- OperatorResponsibilityOperatorResponsibility135.215 IFR: Operating limitations --- OperatorResponsibilityOperatorResponsibility135.217 IFR: Takeoff limitations --- OperatorResponsibilityOperatorResponsibility135.219 IFR: Destination airport weatherminimums--- OperatorResponsibilityOperatorResponsibility135.221 IFR: Alternate airport weatherminimums--- OperatorResponsibilityOperatorResponsibility135.223 135-20 IFR: Alternate airport requirements --- OperatorResponsibilityOperatorResponsibility135.225 IFR: Takeoff, approach and landingminimums--- OperatorResponsibilityOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark135.227 135-60 Icing conditions: Operating limitations GIV-X is transport airplane certified Operatorfor FIKI. AFM has operatingResponsibilitylimitations for icing conditions.135.229 Airport requirements --- OperatorResponsibility* SUBPART E – FLIGHT CREWMEMBER REQUIREMENTS *FSB FindingOperatorResponsibilityOperatorResponsibility135.241 135-57 Applicability Noted -------135.243 135-58 Pilot in command qualifications --- OperatorResponsibilityOperatorResponsibility135.244 135-58 Operating experience --- OperatorResponsibilityOperatorResponsibility135.245 Second in command qualifications --- OperatorResponsibilityOperatorResponsibility135.247 Pilot qualifications: Recent experience --- OperatorResponsibilityOperatorResponsibility135.249 135-51 Use of prohibited drugs --- OperatorResponsibilityOperatorResponsibility135.251 Resting for prohibited drugs --- OperatorResponsibilityOperatorResponsibility135.253 135-48 Misuse of alcohol --- OperatorResponsibilityOperatorResponsibility135.255 135-48 Testing for alcohol --- OperatorResponsibilityOperatorResponsibility* SUBPART F – CREWMEMBER FLIGHT TIME AND DUTY PERIOD LIMITATIONS AND REST REQUIREMENTS *135.261 135-52 Applicability Noted -------135.263 Flight time limitations and restrequirements: All certificate holders--- OperatorResponsibilityOperatorResponsibility135.265 Flight time limitations and restrequirements: Scheduled operations--- OperatorResponsibilityOperatorResponsibility135.267 135-60 Flight time limitations and restrequirements: Unscheduled one- andtwo-pilot crews--- OperatorResponsibilityOperatorResponsibility135.269 Flight time limitations and restrequirements: Unscheduled three- andfour-pilot crews--- OperatorResponsibilityOperatorResponsibility135.271 Helicopter hospital emergency medicalevacuation service (HEMES)--- OperatorResponsibilityOperatorResponsibility135.273 135-60 Duty period limitations and rest timerequirements--- OperatorResponsibilityOperatorResponsibility* SUBPART G – CREWMEMBER TESTING REQUIREMENTS *135.291 Applicability Noted -------135.293 135-27 Initial and recurrent pilot testingrequirements--- OperatorResponsibilityOperatorResponsibility135.295 Initial and recurrent flight attendantcrewmember testing requirements--- OperatorResponsibilityOperatorResponsibility135.297 135-15 Pilot in command: Instrumentproficiency check requirements--- OperatorResponsibilityOperatorResponsibility135.299 Pilot in command: Line checks: Routesand airports--- OperatorResponsibilityOperatorResponsibility135.301 Crewmember: Tests and checks,grace provisions, training to acceptedstandards--- OperatorResponsibilityOperatorResponsibility* SUBPART H – TRAINING *135.321 135-63 Applicability and terms used Noted -------135.323 Training program: General --- OperatorResponsibilityOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark135.324 135-67 Training program: Special rules --- OperatorResponsibility135.325 Training program and revision: InitialOperatorand final approval ---Responsibility135.327 Training program: Curriculum --- OperatorResponsibility135.329 Crewmember training requirements --- OperatorResponsibility135.331 Crewmember emergency training --- OperatorResponsibility135.333 Training requirements: Handling and --- Operatorcarriage of hazardous materialsResponsibility135.335 135-1 Approval of aircraft simulators and --- Operatorother training devicesResponsibility135.337 Qualifications: Check airmen (aircraft) --- Operatorand check airmen (simulator)Responsibility135.338 135-64 Qualifications: Flight instructors --- Operator(aircraft) and flight instructorsResponsibility(simulator)135.339 135-64 Initial and transition training andchecking: Check airmen (aircraft),check airmen (simulator)135.340 135-64 Initial and transition training andchecking: Flight instructors (aircraft),flight instructors (simulator)(b)--- OperatorResponsibility--- OperatorResponsibility135.341 135-18 Pilot and flight attendant crewmembertraining programs--- OperatorResponsibility135.343 135-18 Crewmember initial and recurrent --- Operatortraining requirementsResponsibility135.345 135-46 Pilots: Initial, transition, and upgrade --- Operatorground trainingResponsibility135.347 Pilots: Initial, transition, upgrade, and --- Operatordifferences flight trainingResponsibility135.349 Flight attendants: Initial and transition --- Operatorground trainingResponsibility135.351 135-46 Recurrent training --- OperatorResponsibility135.353 Prohibited drugs --- OperatorResponsibility* SUBPART I – AIRPLANE PERFORMANCE OPERATING LIMITATIONS *135.361 Applicability Noted135.363 135-21 General---OperatorResponsibilityEach certificate holder operating aturbine engine powered large transportcategory airplaneAircraft performance data is providedin the FAA approved Airplane FlightManualFSB FindingOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibility(f)Performance data in the AirplaneFlight Manual135.365 Large transport category airplanes:Reciprocating engine powered:Weight limitations135.367 Large transport category airplanes:Reciprocating engine powered:Takeoff limitationsAircraft performance data is providedin the FAA approved Airplane FlightManualNot applicable -------Not applicable -------OperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position Gulfstream FSB FindingRemark135.369 Large transport category airplanes: Not applicable -------Reciprocating engine powered:En route limitations:All engines operating135.371 Large transport category airplanes: Not applicable -------Reciprocating engine powered:En route limitations:One engine inoperative135.373 Large transport category airplanes:Reciprocating engine powered:En route limitations:Two engines inoperativeNot applicable -------135.375 Large transport category airplanes:Reciprocating engine powered:Landing limitations:Destination airports135.377 Large transport category airplanes:Reciprocating engine powered:Landing limitations:Alternate airports135.379 135-71 Large transport category airplanes:Turbine engine powered:Takeoff limitationsNot applicable -------Not applicable ----------OperatorResponsibility(a)Takeoff weights exceeding AirplaneFlight Manual limitations---OperatorResponsibility(b)(c)Minimum distance required for takeoffMaximum takeoff weight calculationvariablesThe FAA-approved Airplane FlightManual contains all data necessary toenable the operator to comply withthis requirement to include clearwaycomputation data.The FAA-approved Airplane FlightManual contains all data necessary toenable the operator to comply withthis requirement.OperatorResponsibilityOperatorResponsibility(d)(2)Maximum takeoff weight net takeoffflight pathThe FAA-approved Airplane FlightManual contains all data necessary toenable the operator to comply withthis requirement to include net takeoffflight path data.OperatorResponsibility(e)Maximum takeoff weight environmentalconditionsThe FAA-approved Airplane FlightManual contains all data necessary toenable the operator to comply withthis requirement to includeenvironmental variables.OperatorResponsibility(f)Aircraft bank angles on takeoffThe FAA-approved Airplane FlightManual complies with this paragraph.OperatorResponsibility(g)Performance termsThe performance terms are the sameas certified under 14 CFR Part 25OperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark135.381 Large transport category airplanes: The FAA-approved Airplane Flight OperatorTurbine engine powered:Manual and the Operating Manual ResponsibilityEn route limitations: One engine contains all data necessary to enableinoperativethe operator to comply with thisrequirement.FSB FindingOperatorResponsibility135.383 Large transport category airplanes:Turbine engine powered:En route limitations:Two engines inoperative135.385Large transport category airplanes:Turbine engine powered:Landing limitations:Destination airportsNot applicable -------OperatorResponsibility(a)(b)Landing weight limitationsDestination landing requirementsThe airplane FAA-approved FlightManual contains all data necessary toenable the operator to comply withthis requirement. The OperatingManual contains flight planning datato enable computation of fuel and oilburned from departure to destinationor alternate airport to computelanding weight.See note for (a)OperatorResponsibilityOperatorResponsibility(c)(d)Turbopropeller landing requirementsWet runway landing requirements------NotApplicableOperatorResponsibility(e)Alternate requirements to comply withparagraph (b)135.387 Large transport category airplanes:Turbine engine powered:Landing limitations:Alternate airports135.389 Large nontransport category airplanes:Takeoff limitations135.391 Large nontransport category airplanes:En route limitations:One engine inoperative135.393 Large nontransport category airplanes:Landing limitations:Destination airports135.395 Large nontransport category airplanes:Landing limitations:Alternate airports135.397 Small transport category airplaneperformance operating limitationsSee note for (a)The FAA-approved Airplane FlightManual contains all data necessary toenable the operator to comply withthis requirement. The OperatingManual contains flight planning datato enable computation of fuel and oilburned from departure to destinationor alternate airport to computelanding weight. On board flightplanning computer available to assistcrew in mission calculations.OperatorResponsibilityNot applicable -------Not applicable -------Not applicable -------Not applicableNot applicable -------OperatorResponsibilityOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position Gulfstream FSB FindingRemark135.398 Commuter category airplanesNot applicable -------performance operating limitations135.399 Small non transport category airplane Not applicable -------performance operating limitationsSubpart J – Maintenance, Preventive Maintenance, and Alterations*135.411 135-78 Applicability Noted -------135.413 135-81 Responsibility for airworthiness(a)Airworthiness conditions; Maintenance---OperatorResponsibilityOperatorResponsibility(b)Required procedures for maintenanceAn approved maintenance schedulederived from the MSG-3 process andthe Aircraft Maintenance Manualcomplying with FAR 25.1529 andAppendix H is provided to eachoperator.OperatorResponsibility135.415 135-81 Service difficulty reports (operational) --- OperatorResponsibility135.416 135-81 Service difficulty reports (structural) --- OperatorResponsibility135.417 135-81 Mechanical interruption summary --- OperatorreportResponsibility135.419 Approved aircraft inspection program An approved maintenance schedule Operatorderived from the MSG-3 process and Responsibilitythe Aircraft Maintenance Manualcomplying with FAR 25.1529 andAppendix H is provided to eachoperator.OperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibility135.421135-70 Additional maintenance requirements(a)(b)Compliance with manufacturer’srecommended maintenance programsManufacturer’s maintenance programdefinitionAn approved maintenance schedulederived from the MSG-3 process andthe Aircraft Maintenance Manualcomplying with 14 CFR Part 25.1529and Appendix H is provided to eachoperator.See note for (a)OperatorResponsibilityOperatorResponsibilityOperatorResponsibility(c)Single engine aircraft enginemonitoring requirementsNot applicableNotApplicable(d)Single engine aircraft methods,techniques, and practicesNot applicableNotApplicable(e)Single engine aircraft enginemaintenance records135.423 Maintenance, preventive maintenance,and alteration organization135.425 Maintenance, preventive maintenance,and alteration programsNot applicable--- OperatorResponsibility--- OperatorResponsibilityNotApplicableOperatorResponsibilityOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12FAR Amdt. Requirement Gulfstream Position GulfstreamRemark135.427 135-66 Manual requirements An approved maintenance schedule Operatorderived from the MSG-3 process and Responsibilitythe Aircraft Maintenance Manualcomplying with 14 CFR PART25.1529 and Appendix H is providedto each operator.135.429 135-20 Required inspection personnel --- OperatorResponsibility135.431 135-60 Continuing analysis and surveillance --- OperatorResponsibility135.433 Maintenance and preventive---- Operatormaintenance training programResponsibility135.435 135-82 Certificate requirements --- Operator135.437 Authority to perform and approvemaintenance, preventive maintenance,and alterationsResponsibility--- OperatorResponsibility135.439 Maintenance recording requirements An approved maintenance schedulederived from the MSG-3 process andthe Aircraft Maintenance Manualcomplying with 14 CFR PART25.1529 and Appendix H is providedto each operator.OperatorResponsibility135.441 Transfer of maintenance records --- OperatorResponsibility135.443 135-82 Airworthiness release or aircraft --- Operatormaintenance log entryResponsibilityFSB FindingOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibilityOperatorResponsibility

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12Appendix 9 - PLANEVIEW AVIONICS SOFTWARE VERSION “C”PlaneView Avionics Software version “C” includes these functions: charts, graphical flightplanning, uplinked weather, video, enhanced envelope protection and vertical situation displaywith terrain. The FSB found it, as well as the associated AFM change, to be operationally suitable.Pilots transitioning from PlaneView Avionics Software version “B” to “C” in the GIV-X or GV-SP should be trained on the differences using any one of the following level “C” differencestraining devices: interactive computer based instruction, cockpit system simulators, cockpitprocedures trainers, part task trainers, or level 2-5 flight training devices. There are no checking orcurrency requirements for PlaneView Avionics Software “C”.The PlaneView Charts function is FAA certified as part of the aircraft's type design. It isfunctionally equivalent to a Class 3 Electronic Flight Bag (EFB) with Type C softwareapplications. The PlaneView Charts Function may fail if a Data Management Unit (DMU),Local Area Network (LAN) or Personal Computer Memory Card International Association(PCMCIA) card fails, so either paper charts or a Class 1 or Class 2 EFB that is accepted bythe FAA and contains Airport Diagrams, Departure, Arrival and Approach Charts must bereadily available to the flight crew.

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12Appendix 10 - PLANEVIEW AVIONICS SOFTWARE VERSION “D”PlaneView Avionics Software version “D” includes these functions: Vertical Glide Path (VGP),RNP SAAR, performance step climb, takeoff obstacle clearance computations, radio tuning andRunway Awareness Advisory System (RAAS). The FSB found it, as well as the associated AFMchange, to be operationally suitable. Pilots transitioning from PlaneView Avionics Softwareversion “B” to “D” or from version “C” to “D” in the GIV-X or GV-SP should be trained on thedifferences using any one of the following level “C” differences training devices: interactivecomputer based instruction, cockpit system simulators, cockpit procedures trainers, part tasktrainers, or level 2-5 flight training devices. There are no checking or currency requirements forPlaneView Avionics Software “D”.Pilots training RNP SAAR procedures should use the guidance found in Advisory Circular90-101.

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12Appendix 11 - PLANEVIEW AVIONICS SOFTWARE VERSION “E”PlaneView Avionics Software version “E” includes the addition of Synthetic Vision PrimaryFlight Display (SV PFD). SV PFD depicts terrain, obstacles and airports with texture andcolors on the Primary Flight Display. It obtains that data from the TAWS database. The FSBfound it, as well as the associated AFM change, to be operationally suitable. Pilotstransitioning from PlaneView Avionics Software version C” to “E” or from version “D” to“E” in the GIV-X or GV-SP should be trained on the differences using any one of thefollowing level “C” differences training devices: interactive computer based instruction,cockpit system simulators, cockpit procedures trainers, part task trainers, or level 2-5 flighttraining devices. There are no checking or currency requirements for PlaneView AvionicsSoftware version “E”.

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12Appendix 12 - PLANEVIEW AVIONICS SOFTWARE VERSION “F”The PlaneView Avionics Software version “F” “Basic Load” includes these functions:improved map identifiers declutter logic, improved map airway labeling, improvement onmap to graphically join airways, HUD-II interface capability, pilot-controlled CMF selectionswitch, and improved (table-augmented) performance within FMS. A customer option toenable automatic linking of abnormal and emergency checklists to a defined set of activatedCrew Alerting (CAS) messages is an included feature. Additionally, there are customer optionpackages associated with Cert “F” with the functions grouped into the following packages:Enhanced Navigation –Enhanced SV PFD –XM WX Weather –FANS-1 CPDLC using existing ACARS ProtocolGPS SBAS receptionLPV approach capabilityRNP 0.1 navigation capabilityElectronic Terminal Charts stored on each AGMTerrain elevation displayed on map at pilot-selected locationsAutomatic Preview of short-range navigation approachAutomatic transition from short-range navigation source tolong-range navigation source and automatic arming ofFMS/LNAV flight director mode upon selection ofTO/GA feature.Retention of FMS/LNAV flight director mode upon selection ofTO/GA feature when using long-range navigation sourceTemperature-compensated waypoint altitude constraints andVNAV performance in terminal areaCircling approach capabilityThe enhanced SV PFD includes the following improvements tothe basic version: terrain-conformal range rings, grid linesoriented north-south and east-west, terrain depicted on the HSI,a frustum depicted on the HSI representing the viewed area ofthe SV PFD; and the TAWS and TCAS automatic “pop-up” onthe HSI.The map can display the following three weather products,either individually or combined, which are automaticallyreceived at specific intervals: NEXRAD Doppler radar, Infraredcomposite images of clouds, and Winds aloft.Pilots transitioning from PlaneView Avionics Software version “D” to “F” or from version“E” to “F” in the GIV-X or GV-SP should be trained on the differences using the informationprovided in Table 1. There are no checking or currency requirements for PlaneView AvionicsSoftware version “F”.

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12Table 1 – Training DifferencesFROM TO (1) TRAININGLEVELCert “D” or “E” Cert “F” (Basic Load)ACert “F” withC (2)Enhanced NavigationCert “F” withEnhanced SV PFDACert “F” with XMAWeatherNotes: (1) Any combination of customer option packages will be trained to thehighest Training Level.(2) Acceptable Level C training devices include: interactive computer-basedinstruction, cockpit system simulators, cockpit procedures trainers, part tasktrainers, or level 2-5 flight training devices. The devices must be capable ofemulating FMS and cockpit displays performance: allowing pilot entry ofappropriate FMS selections and presenting “real-time” information on thedisplays during the conduct of the flight.The PlaneView Charts function is FAA certified as part of the aircraft's type design in Cert.“F” as a Class 3 Electronic Flight Bag (EFB) with Type C software applications. The AFMlimitation applied during PlaneView Avionics Software Version “C” which required “eitherpaper charts or a Class 1 or Class 2 EFB that is accepted by the FAA and contains AirportDiagrams, Departure, Arrival and Approach Charts must be readily available to the flightcrew” does not apply to Cert. “F” equipped aircraft.

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12Appendix 13 - PLANEVIEW AVIONICS SOFTWARE VERSION “G”PlaneView Avionics Software version “G” includes the addition of the following features:Early Missed Approach activation with the MCDU and TO/GA, LPV Approach capture fromabove, Maximum descent angle improvements, Datalink recording on the Cockpit VoiceRecorder, Path-based TCAS Guidance on the SV PFD, listing of multiple localizerapproaches to the same runway, and update to Fuel Tank Temperature CAS message andrelated Synoptics for the GIV-X only. The FSB found PlaneView Avionics Software version“G”, as well as the associated AFM change, to be operationally suitable.Pilots transitioning from PlaneView Avionics Software version “D”, “E”, or “F” to “G” inthe GIV-X or GV-SP should be trained using one of the following level “A” differencestraining methods: PlaneView Pilot Familiarization Guide or PlaneView Pilot OperatingHandbook for Cert. G. There are no checking or currency requirements for PlaneViewAvionics Software version “G”.Pilots transitioning to PlaneView Avionics Software Enhanced version “G” who have notreceived training on Cert. “F” Enhanced Navigation or Enhanced SV PFD should be trainedon the differences using the information provided in Table 2.Table 2 – Training DifferencesFROM TO (1) TRAININGLEVELCert “D”. “E” or “F” Cert “G” (Basic Load)ABasicCert “F” or “G” withC (2)Enhanced NavigationCert “F” or “G” withXM WeatherACert “F” or “G” withAEnhanced SV PFDCert. “F”Cert. “G” EnhancedAEnhancedNotes:(1) Any combination of customer option packages will be trained to thehighest Training Level.(2) Acceptable Level C training devices include: interactive computer-basedinstruction, cockpit system simulators, cockpit procedures trainers, part tasktrainers, or level 2-5 flight training devices. The devices must be capable ofemulating FMS and cockpit displays performance: allowing pilot entry ofappropriate FMS selections and presenting “real-time” information on thedisplays during the conduct of the flight.

GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12Appendix 14 - G-V DISPLAY UNIT DU-885 MODIFICATIONThe DU-885 modification changes the G-V as follows:1) Replaces six DU-880 cathode ray tubes (CRT) with six DU-885 liquid crystaldisplays (LCD).2) Adds two Cursor Control Devices, an XM Weather receiver, and a data loader.3) Adds the following functions:a) Charts – Displays approach charts, airport maps, SIDs, STARs and noiseprocedures on the Enhanced Navigation Display (ND). Airplane position isalso displayed on the charts that are geo-referenced.b) Maps – Displays the FMS moving map over geopolitical boundariesaugmented with navigational aides and XM weather on the ND.c) Video – Displays multiple video inputs on the ND.d) Database configuration – Displays database statuson the ND and permitsuploading charts and map data.e) DU maintenance – Continuously tests the DU and displays a list of thefailed tests on the ND (ground use maintenance function only).Pilots transitioning from the DU-880 to the DU-885 system should be trained on thedifferences using any one of the following level “C” differences training devices:interactive computer based instruction, cockpit system simulators, cockpitprocedures trainers, part task trainers, or level 2-5 flight training devices. There areno checking or currency requirements for this transition.