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Document Mentions (4 shared documents)
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ight) - Detailed Corrosion Inspection G550 AMM Special inspection (M) 48 MOS 0.0 0 27 Jun 2013 30 Jun 2017 11 Mos 48 25.0 321221 Airframe Main Landing Gear Corrosion Inhibiting Compound Reapplication (Left) G550 AMM Lubrication/Servicing (S) 24 MOS 726.9 242 19 May 2015 30 Jun 2017' 11 Mos 02 20.0 321222
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
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7-61-03 Notes: [End of Month Item] [1 MOS Window( 6550 AMM 05-20-00 1605.6 621 31 Aug 2003 24 MOS 14 Feb 2014 29 Feb 2016' 18 Days 321221 Main Landing Gear Corrosion Inhibiting * Airframe MAN Compound Reapplication (Left) Mfg#: 32-10-00 Notes: [End of Month Item] (1 MOS Window] G550 AMM 05-20-00 4 1605.6
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
2 mentions1 same-page
Page ?Same page
7-61-03 Notes: [End of Month Item] [1 MOS Window( 6550 AMM 05-20-00 1605.6 621 31 Aug 2003 24 MOS 14 Feb 2014 29 Feb 2016' 18 Days 321221 Main Landing Gear Corrosion Inhibiting * Airframe MAN Compound Reapplication (Left) Mfg#: 32-10-00 Notes: [End of Month Item] (1 MOS Window] G550 AMM 05-20-00 4 1605.6
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
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2 mentions1 same-page
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ts (Right) General Visual Inspection 500 Hrs 0.0 3026.7 Hrs* 180.1 Hrs 321046 0 0.0 14 Aug Airframe 2003 G550 AMM Special Inspection (R) Main Landing Gear Corrosion Inhibiting Compound Reapplication (Left) 2689.1 321221 1320 20.0 24 MOS 26 Jul 2014 31 Jul 5 Mos Airframe 2016' G550 AMM Lubrication/Serv
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
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Mutual Connections (116)
Entities connected to both Main Landing Gear Corrosion and Air Data System No.
Samantha Power
PERSON8 w/ Main·6 w/ Air
Wing Rear Beam
ORGANIZATION6 w/ Main·5 w/ Air
First Aid Kit
ORGANIZATION6 w/ Main·5 w/ Air
Empennage FS
ORGANIZATION5 w/ Main·5 w/ Air
Power Transfer Unit
ORGANIZATION7 w/ Main·3 w/ Air
Air Data Module
ORGANIZATION4 w/ Main·5 w/ Air
Trim Cables
ORGANIZATION5 w/ Main·4 w/ Air
Rudder Control
ORGANIZATION5 w/ Main·4 w/ Air
Cowl Doors
ORGANIZATION5 w/ Main·4 w/ Air
General Dynamics Company
ORGANIZATION6 w/ Main·3 w/ Air
Main Fuel Boost Pump
ORGANIZATION5 w/ Main·4 w/ Air
Elevator Control
ORGANIZATION5 w/ Main·4 w/ Air
Upper Surface of Center Wing
ORGANIZATION5 w/ Main·4 w/ Air
Aileron Control
ORGANIZATION5 w/ Main·4 w/ Air
Service Life
ORGANIZATION4 w/ Main·4 w/ Air
FS
Fuel Shut
PERSON4 w/ Main·4 w/ Air
Wheel Steering Unit - Lubrication
ORGANIZATION4 w/ Main·4 w/ Air
Pylons External
ORGANIZATION4 w/ Main·3 w/ Air
Air Turbine Starter Oil - Change
ORGANIZATION4 w/ Main·3 w/ Air
Pylons Internal (Left
ORGANIZATION4 w/ Main·3 w/ Air