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

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