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: G-VAPPROVED BY(POI)____________________________COMPLIANCE METHODSYSTEMREMARKSFLTCHARPROCCHNG34 Navigation Display Unit Controllerhas 4 overhead switchesinstead of 3 No Major X B ALVLALVLBLVLCLVLDCHKCURR34 Navigation RNP and EstimatedPosition Uncertainty(EPU) is displayed onPFD34 Navigation MCDU on EmergencyPower49 APU Bleeds off takeoffcapability added No Minor70 Powerplant Thrust increased by635 lb to 15,385 lbNo Minor X A ANo Minor X B AST,TCBI, SUVTNo No HO AAAA
GIV-X / G-V / GV-SP FSB Report Part I, Rev.8 8/1/12DIFFERENCE AIRCRAFT: G-VBASE AIRCRAFT: GV-SPAPPROVED BY(POI)____________________________DESIGNREMARKS20 Aircraft General PerformanceMax T.O. Weight 500 lb.decrease to 90,500 lb21 ECS Outflow valve changedto butterfly style.24 Electrical Power Revised location ofPDB's and associatedcircuit breakers.25 Furnishings Redesign and relocationof cockpit observer’sseat to behind Captain’sseat27 Flight Controls Trailing Edge Contoursnot installed38 Water & Waste Non-fuselage conformalfresh water tank38 Water “& Waste Relocation of vacuumlavatory waste tank fromabove APU to baggagecompartment49 APU No Bleeds Off takeoffcapability52 Doors Main Door moved aft 24inches52 Doors Aft Lav Dump Doorrelocated53 Fuselage 27 Boundary LayerEnergizers removedfrom the canopy56 Windows Removal of 7 th cabinwindow57 Wings 7 Vortex generatorsrelocated inboard oneach wingLimitationsMax T.O. Weightdecreased by 500 lb to90,500 lbFLTCHARPROCCHNGLVLACOMPLIANCE METHODTRAININGLVL LVLB CLVLDCHKG/CURRCHKNo No X ACURRNo No X A ANo Minor X A ANo No X A ANo No X A ANo No X A ANo No X A ANo Minor 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 AA
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Flight Standardization Board (FSB) Report GIV-x, G-V ... - Code7700

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