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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
Aug 2003 24 MOS 3307.8 927 18 Mar 2014 31 Mar 2016' 14 Mos 273100 * Airframe MAN Elevator Control and Trim Cables in Main Wheel Well and Tail Compartment - Detailed Inspection G550 AMM 05.20.00 3307.8 927 Mfga: 2730-00 Notes: [End of Month Item) [1 MOS Window) 31 Aug 2003 24 MOS 18 Mar 2014 31 M
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
5.6 621 31 Aug 2003 24 MOS 14 Feb 2014 29 Feb 2016' 18 Days 273100 * Airframe MAN Elevator Control and Trim Cables in Main Wheel Well and Tail Compartment - Detailed Inspection Mfg#: 27-30-00 Notes: (End of Month Item( [1 MOS Window] G550 AMM 05-20-00 31 Aug 2003 1605.6 621 24 MOS 22 Feb 2014 29
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
5.6 621 31 Aug 2003 24 MOS 14 Feb 2014 29 Feb 2016' 18 Days 273100 * Airframe MAN Elevator Control and Trim Cables in Main Wheel Well and Tail Compartment - Detailed Inspection Mfg#: 27-30-00 Notes: (End of Month Item( [1 MOS Window] G550 AMM 05-20-00 31 Aug 2003 1605.6 621 24 MOS 22 Feb 2014 29
Entities connected to both Current Lndgs and Tail Compartment -

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