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nual Reversion - Operational Test G550 AMM Functionat'Ops Test (0) 1500 Hrs 0.0 1500.0Hrs 460.0 Hrs 0 11 Feb 2013 03 0.5 121400 Engine 1 Air Turbine Starter Oil - Change G550 AMM Lubrication/Servicing (S) 500 Hrs 1040.0 1540.0Hrs 500.0 Hrs 334 31 May 2016 98 3.0 121400 (121401) Engine 2 Air Turbine Start
unctional / Leak Test HG1153CA04 G550 AMM FunctionalrOps Test (F) 24 MOS 726.9 242 13 May 2015 31 May 2017 10 Mos 02 4.0 341306 Airframe Air Data System No. 3 Functional / Leak Test HG1153CA04 G550 AMM Functional/Ops Test (F) 24 MOS 726.9 242 13 May 2015 31 May 2017 10 Mos 02 4.0 341307 Aidram
8-01 Rockwell Collins Mode S MAN Transponders TOR-94/TDR-940 Notes: (24 MOS Initial Req.] 14 Oct 2014 24MOS" 0.0 0 14 Oct 2016 8 Mos 121400 Air Turbine Starter Oil - Change Engine 1 MAN Mfg#: 12-14-13 Notes: (50 Hour Window] 6550 AMM 05.20.00 23 20 Jun 2013 500 Hrs 2320.2 2845.0 Ws' 255.0 Hrs 927 29 Jul 201
me MAN Test 06081754 05-20-00 1056 Mfg#: 34-13-00 Notes: (End of Month Item) 20 31 Oct 2011 24 MOS 05 Feb 2016 28 Feb 2018 24 Mos 341306 Air Data System No. 3 Functional / Leak HG1153CA02 6550 AMM 2590.0 * Airframe MAN Test 06011391 05-20-00 1056 Mfg#: 34-13-00 Notes: (End of Month Item) 20 3
8-01 Rockwell Collins Mode S MAN Transponders TOR-94/TDR-940 Notes: (24 MOS Initial Req.] 14 Oct 2014 24MOS" 0.0 0 14 Oct 2016 8 Mos 121400 Air Turbine Starter Oil - Change Engine 1 MAN Mfg#: 12-14-13 Notes: (50 Hour Window] 6550 AMM 05.20.00 23 20 Jun 2013 500 Hrs 2320.2 2845.0 Ws' 255.0 Hrs 927 29 Jul 201
me MAN Test 06081754 05-20-00 1056 Mfg#: 34-13-00 Notes: (End of Month Item) 20 31 Oct 2011 24 MOS 05 Feb 2016 28 Feb 2018 24 Mos 341306 Air Data System No. 3 Functional / Leak HG1153CA02 6550 AMM 2590.0 * Airframe MAN Test 06011391 05-20-00 1056 Mfg#: 34-13-00 Notes: (End of Month Item) 20 3
Entities connected to both Air Turbine Starter Oil - Change and Air Data System No.

Samantha Power
PERSONFirst Aid Kit
ORGANIZATIONWing Rear Beam
ORGANIZATIONService Life
ORGANIZATIONEmpennage FS
ORGANIZATIONUpper Surface of Center Wing
ORGANIZATIONMain Fuel Boost Pump
ORGANIZATIONWheel Steering Unit - Lubrication
ORGANIZATIONTrim Cables
ORGANIZATIONMain Landing Gear Corrosion
ORGANIZATIONPower Transfer Unit
ORGANIZATIONAir Data Module
ORGANIZATIONRudder Control
ORGANIZATIONCowl Doors
ORGANIZATIONAileron Control
ORGANIZATIONElevator Control
ORGANIZATIONProtective Breathing Equipment (No.
ORGANIZATIONFuel Shut
PERSONPylons External
ORGANIZATIONPylons Internal (Left
ORGANIZATION