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Differential Pressure Indicator - Detailed 05.20-00 927 Inspection Mfg#: 29.25-01 Notes: [50 Hour Window) 23 20 Jun 2013 17 Mar 2014 292502 Power Transfer Unit Manifold Differential G550 AMM 500 Hrs 3307.8 3854.6 Hrs' 388.1 Hrs Airframe MAN Pressure Indicator Detailed Inspection 052000 927 MfgA 292
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
[50 Hour Window] 6550 AMM 05-20-00 23 20 Jun 2013 500 Hrs 2588.6 3105.6 Hrs' 515.6 Hrs 1054 01 Feb 2016 292502 Airframe Mfg#. 29-25-13 Power Transfer Unit Manifold Differential MAN Pressure Indicator - Detailed Inspection Notes: (50 Hour Window] 6550 AMM 05.20-00 23 20 Jun 2013 500 Hrs 2588.6 3
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]
[50 Hour Window] 6550 AMM 05-20-00 23 20 Jun 2013 500 Hrs 2588.6 3105.6 Hrs' 515.6 Hrs 1054 01 Feb 2016 292502 Airframe Mfg#. 29-25-13 Power Transfer Unit Manifold Differential MAN Pressure Indicator - Detailed Inspection Notes: (50 Hour Window] 6550 AMM 05.20-00 23 20 Jun 2013 500 Hrs 2588.6 3
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]
oval / Installation 1159SCH511-3 mx707782 No Airframe 29.22.01 ver by pq164 0.0 0.0 Hrs 0 0 CrL 0 26 Nov 2007 8.00 292202 Transducer. Power Transfer Unit (PTU) (STA 780) 0.0 0.0 Hrs 1159SCAV600.l ha13634 0 0 CI_ No 0 26 Nov 2007 Airframe ver by pq164 2.00 2924.952000 292203 TRANSDUCER. L
stallation 0.0 0.0 Hrs 60.00 1 I 59L50001-20 MA0512 0 0 OL 592826.040000 Airframe No 0 32.10.00 16000 LDG FOR EASA 26 Nov 2007 321003 Main Landing Gear Components (Left) - Detailed Corrosion Inspection 2354.6 Hrs 25.00 Airframe 32.1000 (End of Month Item) (1 MOS Window) 48 MOS 711 OL 19 Apr 2012 30 Ap
on 0.0 0.0 Hrs 8.00 1159SCH511-4 MX763777 0 0 CiL 107293.351200 No 0 I t Feb 2013 Airframe 29.22.01 VER BY O312506 292202 Transducer. Power Transfer Unit (PTU) {STA 780) 0.0 0.0 Hrs 2.00 1159SCAV600.1 HAL6429 0 0 CiL 2924.952000 No 0 11 Feb 2013 Airframe VER BY O312506 292203 TRANSDUCER.
n Landing Gear (Right) - Removal / Installation 0.0 1159L50001.26 MA0994 0 No 0 32.10.00 0.0 Hrs 0 C& 11 Feb 2013 60.00 0.000000 321003 Main Landing Gear Components (Left) - Detailed Corrosion Inspection 0.0 Hrs 25.00 Airframe 32.10.00 48 (End of Month Item) (1 MOS Window) 48 MOS 0 CI_ 27 Jun 2013 30 J
Entities connected to both Power Transfer Unit and Main Landing Gear Components

Samantha Power
PERSONMain Landing Gear Corrosion
ORGANIZATIONGeneral Dynamics Company
ORGANIZATIONFirst Aid Kit
ORGANIZATIONMain Fuel Boost Pump
ORGANIZATIONAir Turbine Starter Oil - Change
ORGANIZATIONCockpit Voice Recorder Operational Test
ORGANIZATIONTrash Receptacle Enclosure
ORGANIZATIONElevator Control
ORGANIZATIONTrim Cables
ORGANIZATIONUpper Surface of Center Wing
ORGANIZATIONRudder Control
ORGANIZATIONCowl Doors
ORGANIZATIONWing Rear Beam
ORGANIZATIONMain Landing
LOCATIONEmpennage FS
ORGANIZATIONAileron Control
ORGANIZATIONPylons External
ORGANIZATIONWheel Steering Unit - Lubrication
ORGANIZATIONLanding Gear Emergency Extension
ORGANIZATION