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

GIV-X / G-V / GV-SP FSB Report Part I, Rev. 8 8/1/12DIFFERENCE AIRCRAFT: GVBASE AIRCRAFT: GIV-XAPPROVED BY(POI)____________________________SYSTEMREMARKSFLTCHARPROCCHNGLVLACOMPLIANCE METHODTRAININGLVL LVLB CLVLDCHK / CURR22 Autoflight TOGA Flight DirectorCommand Bars initiate at12 degrees vs. 8 degreesNo No X A Aon GIV-X.23 Communications New Audio System No No X A A23 Communications Radio Tuning ThroughRFMUNo Yes X A A27 Flight Controls Spoiler Control switchadded. Lateral 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 SystemsStandby EngineInstrument on RFMUDAU (Data AcquisitionUnit) and FWC (FaultWarning Computer)replaces MAU (ModularAvionics Unit)Display ControllerElectronic Checklist AutoPop-up Feature enabled No MinorCHKCURRNo Minor X A ANo Minor X A ANo Minor X A A34 Navigation IRS ON/OFF switchesdeleted and replaced with No Minor X A AMSU switches34 Navigation EICAS FMS JoystickPanelNo None X A A34 Navigation 6 Display Units vs. 4Display UnitsNo Minor X B A34 Navigation No CCDs Used inConjunction with DisplaysNo Minor X B A34 Navigation HSI on RFMU No Minor X A A34 Navigation LaserTrack No Minor X B A34 Navigation Standby Flight instrumentshave different design and No Minor X A Alocation49 APU Different APU installedwith capability for APUassisted main engine No Minor X A Aairstart and differentelectrical load capabilities.70 Powerplant Thrust increased by900 lb to 14,750 lbNo No X A AST,TCBIorVTAA