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uator Linkage General Visual Inspection GV AMM Special Inspection (M) 96 MOS 2997.3 805 03 Dec 2007 03 Dec 2015 10 Mos 8.0 271010 Airframe Aileron Control and Trim Cables in Pressurized Areas of Fuselage and Overwing to Aft Wing Links Detailed Inspection GV AMM Special Inspection (M) 96 MOS 2997.3
(Right) General Visual Inspection GV AMM Special Inspection (R) 500 Hrs 7182.5 7726.7 Hrs 474.1 Hrs 1776 28 Dec 2014 0.0 321221 Airframe Main Landing Gear Corrosion Inhibiting Compound Reapplication (Left) GV AMM Lubrication/Servicing (S) 7028.6 1741 24 MOS 09 Oct 2014 31 Oct 2016' 20 Mos 20.0 321222 Ai
ft Lavatory) • Inspection C354TS G550 AMM Special Inspection (R) 12 MOS 1040.0 334 01 Jun 2016 30 Jun 2oir 11 Mos 01 1.0 271011 Airframe Aileron Control and Trim Cables in Main Wheel Wells / Wing Trailing Edge Detailed Inspection G550 AMM Special Inspection (R) 24 MOS 726.9 242 12 May 2015 30 Ju
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
egrity Test 05.2000 927 Mfg#: 26.21-00 Notes: [End of Month Item] [1 MOS Window] 31 Aug 2003 24 MOS 17 Mar 2014 31 Mar 2016' 14 Mos 271011 Aileron Control and Trim Cables in Main G550 AMM 3307.8 * Airframe MAN Wheel Wells I Wing Trailing Edge - 05.20.00 927 Detailed Inspection Mfga: 27.10-00 N
949 Notes: EXP DATE APR 2015 CONFIRMED BY OPERATOR & CAMO 24 MOS 28 Oct 2014 01 Nov 2016 22 Mos [End of Month Item] [CUSTOM FREQUENCY] 321221 Main Landing Gear Corrosion Inhibiting G550 AMM 3444.5 * Airframe MAN Compound Reapplication (Left) 05.20.00 949 Mfg#: 32-10-00 Notes: [End of Month Item] (1 MOS Window
N Functional Test 54498D1 05.10-00 0 Mfg#: 26.21-03 Notes: (End of Month Item] 31 Aug 2003 120 MOS 29 Apr 2006 29 Feb 2016 18 Days 271011 Aileron Control and Trim Cables in Main G550 AMM 1605.6 * Airframe MAN Wheel Wells / Wing Trailing Edge - 05.20-00 621 Detailed Inspection Mfg#: 27,10-00 No
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
N Functional Test 54498D1 05.10-00 0 Mfg#: 26.21-03 Notes: (End of Month Item] 31 Aug 2003 120 MOS 29 Apr 2006 29 Feb 2016 18 Days 271011 Aileron Control and Trim Cables in Main G550 AMM 1605.6 * Airframe MAN Wheel Wells / Wing Trailing Edge - 05.20-00 621 Detailed Inspection Mfg#: 27,10-00 No
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
Entities connected to both Aileron Control and Main Landing Gear Corrosion

Samantha Power
PERSONTrim Cables
ORGANIZATIONRudder Control
ORGANIZATIONWing Rear Beam
ORGANIZATIONFuel Shut
PERSONCowl Doors
ORGANIZATIONPower Transfer Unit
ORGANIZATIONMain Fuel Boost Pump
ORGANIZATIONFirst Aid Kit
ORGANIZATIONEmpennage FS
ORGANIZATIONGeneral Dynamics Company
ORGANIZATIONElevator Control
ORGANIZATIONUpper Surface of Center Wing
ORGANIZATIONTrash Receptacle Enclosure
ORGANIZATIONService Life
ORGANIZATIONWheel Steering Unit - Lubrication
ORGANIZATIONAileron Inter-column
ORGANIZATIONLongitudinal Control System Friction
ORGANIZATIONPylons Internal (Left
ORGANIZATIONPylons External
ORGANIZATION