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

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