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Projected Through • 5966.5 Hours 77 2203 Landings 19 Jan 2020 Date 4544.5 APU Hours 30 APU Cycles COMPONENT TIMES G-CGUL Current TT 3466.5 Current Lndgs 953 Current Hr Mtr 3423.6 Position Logbook Description Serial Number Total Time Total Cycles TSO CSO 1 Engine Rolls Royce 8R700.71004.11
0Hrs 1533.5 Hrs 05.2000 0 31 Dec 2003 22 Oct 2007 G550 AMM 5000 Hrs 0.0 5000.0Hrs 1533.5 Hrs 05.2000 0 31 Dec 2003 20 Oct 2007 236001 L Wing Static Wicks / Bonding - Functional * Airframe MAN Test Mfga: 2361-01 Notes: [End of Month Item) (1 MOS Window) G550 AMM 05.20.00 31 Aug 2003 48 MOS 2354.6 711 19 Apr 2012
rough: 3590 Hours TT 1956 Landings Cycles 900 Cycles 2 10 Feb 2019 Date 2834.5 APU Hours 1356 APU Cycles COMPONENT TIMES Current TT 2590.0 Current Lndgs 1056 Current Hr Mtr 2571.0 Position Logbook Description Serial Number Total Time Total Cycles TSO CSO 1 Engine Rolls Royce BR700.110C411
iDate Next Due fl Adj) Remaining Hrs/Cyc/Cal Logbook I App Serial Number Section Page Mfg Ref Number Notes Revision Date Issued 236001 L Wing Static Wicks / Bonding - Functional * Airframe MAN Test Mfg#: 23.61-01 Notes: [End of Month Item] (1 MOS Window] G550 AMM 05.20.00 1903.5 741 31 Aug 2003 48 MOS 26 Aug 2014
rough: 3590 Hours TT 1956 Landings Cycles 900 Cycles 2 10 Feb 2019 Date 2834.5 APU Hours 1356 APU Cycles COMPONENT TIMES Current TT 2590.0 Current Lndgs 1056 Current Hr Mtr 2571.0 Position Logbook Description Serial Number Total Time Total Cycles TSO CSO 1 Engine Rolls Royce BR700.110C411
iDate Next Due fl Adj) Remaining Hrs/Cyc/Cal Logbook I App Serial Number Section Page Mfg Ref Number Notes Revision Date Issued 236001 L Wing Static Wicks / Bonding - Functional * Airframe MAN Test Mfg#: 23.61-01 Notes: [End of Month Item] (1 MOS Window] G550 AMM 05.20.00 1903.5 741 31 Aug 2003 48 MOS 26 Aug 2014
Entities connected to both Current Lndgs and L Wing Static Wicks / Bonding - Functional

Samantha Power
PERSONService Life
ORGANIZATIONAir Turbine Starter Oil - Change
ORGANIZATIONFirst Aid Kit
ORGANIZATIONTrim Cables
ORGANIZATIONRudder Control
ORGANIZATIONCowl Doors
ORGANIZATIONMain Fuel Boost Pump
ORGANIZATIONMain Landing Gear Corrosion
ORGANIZATIONWing Rear Beam (Left
ORGANIZATIONWing Rear Beam
ORGANIZATIONAileron Control
ORGANIZATIONPower Transfer Unit
ORGANIZATIONCockpit Voice Recorder Operational Test
ORGANIZATIONTime Limited Supplies
ORGANIZATIONTrash Receptacle Enclosure
ORGANIZATIONLanding Gear Emergency Extension
ORGANIZATIONAileron Inter-column
ORGANIZATIONElevator Control
ORGANIZATIONUpper Surface of Center Wing
ORGANIZATION