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ate Next Due Nadi) Remaining HrsiCyciCal Logbook I App Serial Number Section I Page Mfg Ref Number Notes Revision I Date issued 321003 Main Landing Gear Components (Left) - * Airframe MAN Detailed Corrosion Inspection MIga: 32-10-00 Notes: [End of Month Item] {1 MOS Window) G550 AMM 05-20.00 31 Aug 2003
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
30.13.03 Notes: (End of Month Item] (1 MOS Window] 6550 AMM 1300.4 05.20-00 486 31 Aug 2003 72 MOS 25 Sep 2012 30 Sep 2018' 31 Mos 321003 Main Landing Gear Components (Left) - 6550 AMM 1903.5 * Airframe MAN Detailed Corrosion Inspection 05.20-00 741 Mfg#: 32-10-00 Notes: [End of Month Item] (1 MOS Window]
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
30.13.03 Notes: (End of Month Item] (1 MOS Window] 6550 AMM 1300.4 05.20-00 486 31 Aug 2003 72 MOS 25 Sep 2012 30 Sep 2018' 31 Mos 321003 Main Landing Gear Components (Left) - 6550 AMM 1903.5 * Airframe MAN Detailed Corrosion Inspection 05.20-00 741 Mfg#: 32-10-00 Notes: [End of Month Item] (1 MOS Window]
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 Main Landing Gear Components and Fuel Filter Bypass Indicator - Detailed
Main Landing Gear Corrosion
ORGANIZATIONPower Transfer Unit
ORGANIZATION
Samantha Power
PERSONWing Rear Beam
ORGANIZATIONAileron Control
ORGANIZATIONTrim Cables
ORGANIZATIONRudder Control
ORGANIZATIONCowl Doors
ORGANIZATIONMain Fuel Boost Pump
ORGANIZATIONInlet Cowl Aerodynamic Surfaces (Right
ORGANIZATIONFirst Aid Kit
ORGANIZATIONWing Rear Beam (Left
ORGANIZATIONAir Turbine Starter Oil - Change
ORGANIZATIONCockpit Voice Recorder Operational Test
ORGANIZATIONTime Limited Supplies
ORGANIZATIONTrash Receptacle Enclosure
ORGANIZATIONLanding Gear Emergency Extension
ORGANIZATIONService Life
ORGANIZATIONAileron Inter-column
ORGANIZATIONElevator Control
ORGANIZATION