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

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

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