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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
nspection 05.2000 927 Mfga: 52-11-01 Notes: [End of Month Item) [I MOS Window) 7 30 Jun 2006 36 MOS 18 Mar 2014 31 Mar 201r 26 Mos 493402 Fuel Filter Bypass Indicator - Detailed G550 AMM 600 Hrs 1981.0 2581.0Hrs 536.5 Hrs APU I MAN Inspection (Delta P Indicator) 05.20.00 0 Mfg#: 49.34-01 Notes: [50 Hour Window) 20
[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
acement • Fuel Boost Airframe MAN Pumps, P/N 1159SCP500-5 Notes: (31 Oct 2016 Initial Date Req.] 11 Sep 2015 0.0 0 31 Oct 2016 8 Mos 493402 Fuel Filter Bypass Indicator - Detailed APU 1 MAN Inspection (Delta P Indicator) Mfgit: 49-34-01 Notes: (50 Hour Window] 6550 AMM 05.20-00 20 31 Oct 2011 600 Hrs 1558.0 2132.0 Hr
[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
acement • Fuel Boost Airframe MAN Pumps, P/N 1159SCP500-5 Notes: (31 Oct 2016 Initial Date Req.] 11 Sep 2015 0.0 0 31 Oct 2016 8 Mos 493402 Fuel Filter Bypass Indicator - Detailed APU 1 MAN Inspection (Delta P Indicator) Mfgit: 49-34-01 Notes: (50 Hour Window] 6550 AMM 05.20-00 20 31 Oct 2011 600 Hrs 1558.0 2132.0 Hr
Entities connected to both Power Transfer Unit and Fuel Filter Bypass Indicator - Detailed

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