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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
0Hrs 1533.5 Hrs 05.2000 0 31 Dec 2003 22 Oct 2007 G550 AMM 5000 Hrs 0.0 5000.0Hrs 1533.5 Hrs 05.2000 0 31 Dec 2003 20 Oct 2007 236001 L Wing Static Wicks / Bonding - Functional * Airframe MAN Test Mfga: 2361-01 Notes: [End of Month Item) (1 MOS Window) G550 AMM 05.20.00 31 Aug 2003 48 MOS 2354.6 711 19 Apr 2012
[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
iDate Next Due fl Adj) Remaining Hrs/Cyc/Cal Logbook I App Serial Number Section Page Mfg Ref Number Notes Revision Date Issued 236001 L Wing Static Wicks / Bonding - Functional * Airframe MAN Test Mfg#: 23.61-01 Notes: [End of Month Item] (1 MOS Window] G550 AMM 05.20.00 1903.5 741 31 Aug 2003 48 MOS 26 Aug 2014
[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
iDate Next Due fl Adj) Remaining Hrs/Cyc/Cal Logbook I App Serial Number Section Page Mfg Ref Number Notes Revision Date Issued 236001 L Wing Static Wicks / Bonding - Functional * Airframe MAN Test Mfg#: 23.61-01 Notes: [End of Month Item] (1 MOS Window] G550 AMM 05.20.00 1903.5 741 31 Aug 2003 48 MOS 26 Aug 2014
Entities connected to both Power Transfer Unit and L Wing Static Wicks / Bonding - Functional

Samantha Power
PERSONMain Landing Gear Corrosion
ORGANIZATIONFirst Aid Kit
ORGANIZATIONWing Rear Beam
ORGANIZATIONAileron Control
ORGANIZATIONTrim Cables
ORGANIZATIONRudder Control
ORGANIZATIONCowl Doors
ORGANIZATIONMain Fuel Boost Pump
ORGANIZATIONMain Landing Gear Components
ORGANIZATIONElevator Control
ORGANIZATIONUpper Surface of Center Wing
ORGANIZATIONAir Turbine Starter Oil - Change
ORGANIZATIONCockpit Voice Recorder Operational Test
ORGANIZATIONTrash Receptacle Enclosure
ORGANIZATIONEmpennage FS
ORGANIZATIONAileron Inter-column
ORGANIZATIONLanding Gear Emergency Extension
ORGANIZATIONService Life
ORGANIZATIONPylons Internal (Left
ORGANIZATION