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

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