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[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
Inspection 05.20.00 741 Mfg#: 32-20-00 Notes: (End of Month Item) [1 MOS Window) 31 Aug 2003 48 MOS 12 Sep 2014 30 Sep 2018' 31 Mos 324133 Mechanical Brake Linkage at Rudder 6550 AMM 1300.4 * Airframe MAN Pedal - General Visual Inspection 05.20-00 486 Mfg#: 32-44-00 Notes: (End of Month Item] (1 MOS Win
[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
Inspection 05.20.00 741 Mfg#: 32-20-00 Notes: (End of Month Item) [1 MOS Window) 31 Aug 2003 48 MOS 12 Sep 2014 30 Sep 2018' 31 Mos 324133 Mechanical Brake Linkage at Rudder 6550 AMM 1300.4 * Airframe MAN Pedal - General Visual Inspection 05.20-00 486 Mfg#: 32-44-00 Notes: (End of Month Item] (1 MOS Win
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.
ttle Valve (No. 2) - Removal 0.0 Installation 0.0 its 3.00 1159H50362-3 0 0 CtL 897.202200 Airframe No 0 3248.07-RI 11 Feb 2013 324133 Mechanical Brake Linkage at Rudder Pedal - General Visual Inspection 0.0 Hrs 6.00 Airframe 32.44.00 06 (End of Month Item) [1 MOS Window) 72 MOS 0 CtL 27 Jun 2013
Entities connected to both Power Transfer Unit and Mechanical Brake Linkage

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