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.842.80 4.0 240121 Airframe Emergency Battery Power System (Left) - Operational Test 12 MOS 7109.1
Wing Trailing Edge Detailed Inspection GV AMM Special Inspection (R) 24 MOS 6385.9 1575 11 Sep 2013 24 Sep 2015' 7 Mos 2.0 271110 Airframe Aileron Inter-column Linkage Disconnect Assemblies - Operational Test GV AMM Functional/Ops Test (0) 1000 Hrs 48 MOS 6385.9 7385.9Hrs 1575 11 Sep 2013 11 Sep 2017
ur Window) 23 20 Jun 2013 17 Mar 2014 292502 Power Transfer Unit Manifold Differential G550 AMM 50
on Communication 0.0 Airframe MAN & Surveillance Systems. LLC 0 Notes: [36 MOS Initial Req.] 13 Mar 2012 36MOS" 13 Mar 2015 52 Days 271110 Aileron Inter-column Linkage Disconnect G550 AMM 1000 Hrs 2849.4 3849.4Hrs 382.9 Hrs * Airframe MAN Assemblies Operational Test 05.2000 833 Mfga: 27.11-01 Not
14 31 Jul 2016 5 Mos 240122 Emergency Battery Power System (Right) 6550 AMM 2320.2 * Airframe MA
s Airframe MAN Front Frame (Right) - Detailed Inspection 05-20-00 741 Mfg#: 78-30-30 Notes: (50 Hour Window] 31 Aug 2003 18 Sep 2014 271110 Aileron Inter-column Linkage Disconnect G550 AMM 1000 Hrs 1903.5 2910.0 Hrs* 320.0 Hrs * Airframe MAN Assemblies • Operational Test 05-20-00 741 Mfg#: 27.11.01
14 31 Jul 2016 5 Mos 240122 Emergency Battery Power System (Right) 6550 AMM 2320.2 * Airframe MA
s Airframe MAN Front Frame (Right) - Detailed Inspection 05-20-00 741 Mfg#: 78-30-30 Notes: (50 Hour Window] 31 Aug 2003 18 Sep 2014 271110 Aileron Inter-column Linkage Disconnect G550 AMM 1000 Hrs 1903.5 2910.0 Hrs* 320.0 Hrs * Airframe MAN Assemblies • Operational Test 05-20-00 741 Mfg#: 27.11.01
.01 verified by PO619 26 Nov 2007 275201 Flap Power Drive Unit Removal / Installation 0.0 0.0 Hrs
0.00 271109 Airframe AILERON LINKAGE DISCONNECT 0.0 1159SCC565-1 0 No 0 27.11.17 0.0 Hrs 0 CI_ 26 Nov 2007 4.00 7318.316400 Airframe Aileron Inter-column Linkage Disconnect Assemblies - Operational Operational Test 27.11.01 [End of Month Item] [50 Hour Window] [1 MOS Window] 1000 Hrs 48 MOS 2849.
Entities connected to both Samantha Power and Aileron Inter-column
General Dynamics Company
ORGANIZATIONWing Rear Beam
ORGANIZATIONTSNMO
ORGANIZATIONFirst Aid Kit
ORGANIZATIONRudder Control
ORGANIZATIONTrim Cables
ORGANIZATIONAileron Control
ORGANIZATIONMain Fuel Boost Pump
ORGANIZATIONCowl Doors
ORGANIZATIONFuel Shut
PERSONTrash Receptacle Enclosure
ORGANIZATIONMain Landing Gear Corrosion
ORGANIZATIONPower Transfer Unit
ORGANIZATIONEmpennage FS
ORGANIZATIONService Life
ORGANIZATIONAir Turbine Starter Oil - Change
ORGANIZATIONUpper Surface of Center Wing
ORGANIZATIONAir Data Module
ORGANIZATIONElevator Control
ORGANIZATIONForward Cabin
PERSON