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Document Mentions (7 shared documents)
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e Indicator - Detailed Inspection GV AMM Special Inspection (R) 500 Hrs 7182.5 7726.7 Hrs' 1776 28 Dec 2014 474.1 Hrs 0.5 292502 Airframe Power Transfer Unit Manifold Differential Pressure Indicator GV AMM Special Inspection (R) Detailed Inspection 500 Hrs 7182.5 7726.7 Hrs' 1776 28 Dec2014 474.1
(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
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ndicator - Detailed Inspection G550 AMM Special Inspection (R) 500 Hrs 1040.0 1540.0Hrs 500.0 Hrs 334 01 Jun 2016 01 1.0 292502 Airframe Power Transfer Unit Manifold Differential Pressure Indicator • Detailed Inspection G550 AMM Special Inspection (R) 500 Hrs 1040.0 1540.0Hrs 500.0 Hrs 334 01 Jun
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
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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
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
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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
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
2 mentions1 same-page
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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
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
2 mentions1 same-page
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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
6 Hrs Installation 1159L50100.11 PLT0196 711 711 711 OL No 53 19 Apr 2012 Airframe 32.12.01 2354.6 Hrs 711 Cycilnd 12.00 121442.260800 Main Landing Gear Corrosion Inhibiting Compound 321221 Reapplication (Left) Airframe 32.10.00 [End of Month Item] [1 MOS Window] 24 MOS 3444.5 Hrs 949 CI_ 03 Nov 2014
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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.
(Right) Removal / 0.0 Installation 1159L50100-13 PLT0690 0 No 0 3212.01 0.0 Hrs 0 CI 11 Feb 2013 12.00 108223.224000 321221 Airframe Main Landing Gear Corrosion Inhibiting Compound Reapplication (Left) 32.10.00 02 (End of Month Item) [1 MOS Window) 24 MOS 726.9 Hrs 242 CI_ 19 May 2015 30 Jun 2017' 2
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Mutual Connections (189)
Entities connected to both Power Transfer Unit and Main Landing Gear Corrosion
Samantha Power
PERSON8 w/ Power·8 w/ Main
First Aid Kit
ORGANIZATION6 w/ Power·6 w/ Main
General Dynamics Company
ORGANIZATION6 w/ Power·6 w/ Main
Wing Rear Beam
ORGANIZATION5 w/ Power·6 w/ Main
Cowl Doors
ORGANIZATION5 w/ Power·5 w/ Main
Elevator Control
ORGANIZATION5 w/ Power·5 w/ Main
Main Landing Gear Components
ORGANIZATION5 w/ Power·5 w/ Main
Main Fuel Boost Pump
ORGANIZATION5 w/ Power·5 w/ Main
Empennage FS
ORGANIZATION5 w/ Power·5 w/ Main
Upper Surface of Center Wing
ORGANIZATION5 w/ Power·5 w/ Main
Rudder Control
ORGANIZATION5 w/ Power·5 w/ Main
Trim Cables
ORGANIZATION5 w/ Power·5 w/ Main
Aileron Control
ORGANIZATION5 w/ Power·5 w/ Main
Air Turbine Starter Oil - Change
ORGANIZATION5 w/ Power·4 w/ Main
Landing Gear Emergency
ORGANIZATION4 w/ Power·5 w/ Main
Trash Receptacle Enclosure
ORGANIZATION5 w/ Power·4 w/ Main
Cockpit Voice Recorder Operational Test
ORGANIZATION5 w/ Power·4 w/ Main
Pylons External
ORGANIZATION4 w/ Power·4 w/ Main
Pylons Internal (Left
ORGANIZATION4 w/ Power·4 w/ Main
Main Landing
LOCATION4 w/ Power·4 w/ Main