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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
nspection 05.2000 927 Mfga: 52-11-01 Notes: [End of Month Item) [I MOS Window) 7 30 Jun 2006 36 MOS 18 Mar 2014 31 Mar 201r 26 Mos 493402 Fuel Filter Bypass Indicator - Detailed G550 AMM 600 Hrs 1981.0 2581.0Hrs 536.5 Hrs APU I MAN Inspection (Delta P Indicator) 05.20.00 0 Mfg#: 49.34-01 Notes: [50 Hour Window) 20
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
acement • Fuel Boost Airframe MAN Pumps, P/N 1159SCP500-5 Notes: (31 Oct 2016 Initial Date Req.] 11 Sep 2015 0.0 0 31 Oct 2016 8 Mos 493402 Fuel Filter Bypass Indicator - Detailed APU 1 MAN Inspection (Delta P Indicator) Mfgit: 49-34-01 Notes: (50 Hour Window] 6550 AMM 05.20-00 20 31 Oct 2011 600 Hrs 1558.0 2132.0 Hr
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
acement • Fuel Boost Airframe MAN Pumps, P/N 1159SCP500-5 Notes: (31 Oct 2016 Initial Date Req.] 11 Sep 2015 0.0 0 31 Oct 2016 8 Mos 493402 Fuel Filter Bypass Indicator - Detailed APU 1 MAN Inspection (Delta P Indicator) Mfgit: 49-34-01 Notes: (50 Hour Window] 6550 AMM 05.20-00 20 31 Oct 2011 600 Hrs 1558.0 2132.0 Hr
Entities connected to both Current Lndgs and Fuel Filter Bypass Indicator - Detailed

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