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Hrs 334 01 Jun 2016 01 1.0 292502 Airframe Power Transfer Unit Manifold Differential Pressure Indi
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
14 31 Jul 2016 5 Mos 240122 Emergency Battery Power System (Right) 6550 AMM 2320.2 * Airframe MA
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
14 31 Jul 2016 5 Mos 240122 Emergency Battery Power System (Right) 6550 AMM 2320.2 * Airframe MA
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
l 2016 5 Mos $1.842.67 4.0 Standby Electrical Power System Operational Test 2676.5 242O05 1312 1.
No. I - Functional / Leak Test 2761.6 341304 1352 4.0 12 MOS 01 Mar 29 Feb 24 Days Airframe 2015 2016' G550 AMM FunctionatlOps Test (F) Air Data System No. 2 Functional / Leak Test 2761.6 341305 1352 4.0 12 MOS 01 Mar 29 Feb 24 Days Airframe 2015 2016* G550 AMM Functionat(Ops Test (F) Air D
Functional/0as Teal (0) 02 Standby Electrical Power System - Operational Tesl 3971.1 242005 1318
No. 1 - Functional / Leak Test G550 AMM 4650.4 1644 24 MOS 20 Jun 2014 30 Jun 2016 13 Mos Funclional/Ops Test (F) 02 4.0 341305 Airframe Air Data System No. 2 - Functional / Leak Test 6550 AMM 4550.4 1544 24 MOS 20 Jun 2014 30 Jun 2016 13 Mos FunctionaVOps Test (F) 02 40 341306 Airframe Air Da
ame 33.40.00 334025 Anticollision Strobe Light Power Supply Unit (Left) - Removal / Installation 0.0
SW TSNMO TSOMO TSRMO Manufacturer Labor Warranty MM Ref @=Adlustments (Used Hrs, Cye, Date) Ops Number(s) I Comments Date Type 341305 Air Data System No. 2 Functional / Leak Test 726.9 Hrs HG1153CA04 242 CI_ 24 MOS 13 May 2015 31 May 2017 4.00 Airframe 34.13.00 02 Post ASC 14A, but aircraft
Entities connected to both Samantha Power and Air Data System No.
General Dynamics Company
ORGANIZATIONWing Rear Beam
ORGANIZATIONFirst Aid Kit
ORGANIZATIONOps Number(s
ORGANIZATIONAileron Control
ORGANIZATIONRudder Control
ORGANIZATIONCowl Doors
ORGANIZATIONTrim Cables
ORGANIZATIONEmpennage FS
ORGANIZATIONFuel Shut
PERSONMain Fuel Boost Pump
ORGANIZATIONAir Data Module
ORGANIZATIONService Life
ORGANIZATIONMain Landing Gear Corrosion
ORGANIZATIONAl Rights Reserved
ORGANIZATIONUpper Surface of Center Wing
ORGANIZATIONAir Turbine Starter Oil - Change
ORGANIZATIONPower Transfer Unit
ORGANIZATIONTrash Receptacle Enclosure
ORGANIZATIONElevator Control
ORGANIZATION