3
Shared Docs
3
Same-Page
3 / 3
Mentions
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
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
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
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]
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
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]
Entities connected to both Aileron Inter-column and Main Landing Gear Components

Samantha Power
PERSONPower Transfer Unit
ORGANIZATIONMain Landing Gear Corrosion
ORGANIZATIONTrim Cables
ORGANIZATIONWing Rear Beam
ORGANIZATIONTrash Receptacle Enclosure
ORGANIZATIONAileron Control
ORGANIZATIONRudder Control
ORGANIZATIONMain Fuel Boost Pump
ORGANIZATIONCowl Doors
ORGANIZATIONFirst Aid Kit
ORGANIZATIONUpper Surface of Center Wing
ORGANIZATIONAileron Hardover Prevention System
ORGANIZATIONCockpit Voice Recorder Operational Test
ORGANIZATIONEmpennage FS
ORGANIZATIONElevator Control
ORGANIZATIONLongitudinal Control System Friction
ORGANIZATIONInlet Cowl Aerodynamic Surfaces (Right
ORGANIZATIONWing Rear Beam (Left
ORGANIZATIONFuel Shut
PERSON