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 8/1/12DIFFERENCE 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
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Flight Standardization Board (FSB) Report GIV-x, G-V ... - Code7700

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