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4307.8Hrs 841.3 Hrs Engine 2 MAN Detailed Inspection 052000 927 Mfg#: 7238-01 Notes: [50 Hour Window] 10 15 Oct 2007 20 Mar 2014 801011 Air Turbine Starter Magnetic Chip G550 AMM 1000 Hrs 3307.1 4307.1Hrs 840.6 Hrs * Engine 1 MAN Collector Detailed Inspection 05.20.00 927 Mfg#: 8000-00 Notes: [End of Month
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
ad (Warranty Managed 0.0 Airframe OPT Program) 0 Notes: (25 Jan 2018 Initial Date Req.] 25 Jan 2013 29 Apr 2006 25 Jan 2018' 23 Mos 801011 Air Turbine Starter Magnetic Chip 6550 AMM 1000 Hrs 2320.2 3320.2Hrs 730.2 Hrs * Engine 1 MAN Collector - Detailed Inspection 05-20-00 927 Mfg#: 80.00.00 Notes: (End of Mo
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
ad (Warranty Managed 0.0 Airframe OPT Program) 0 Notes: (25 Jan 2018 Initial Date Req.] 25 Jan 2013 29 Apr 2006 25 Jan 2018' 23 Mos 801011 Air Turbine Starter Magnetic Chip 6550 AMM 1000 Hrs 2320.2 3320.2Hrs 730.2 Hrs * Engine 1 MAN Collector - Detailed Inspection 05-20-00 927 Mfg#: 80.00.00 Notes: (End of Mo
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 Air Turbine Starter Magnetic Chip and L Wing Static Wicks / Bonding - Functional
Main Landing Gear Corrosion
ORGANIZATIONFirst Aid Kit
ORGANIZATIONWing Rear Beam (Left
ORGANIZATIONWing Rear Beam
ORGANIZATIONAileron Control
ORGANIZATIONTrim Cables
ORGANIZATIONRudder Control
ORGANIZATIONCowl Doors
ORGANIZATIONMain Fuel Boost Pump
ORGANIZATIONPower Transfer Unit
ORGANIZATIONAir Turbine Starter Oil - Change
ORGANIZATIONCockpit Voice Recorder Operational Test
ORGANIZATIONTime Limited Supplies
ORGANIZATIONTrash Receptacle Enclosure
ORGANIZATIONLanding Gear Emergency Extension
ORGANIZATIONService Life
ORGANIZATIONAileron Inter-column
ORGANIZATIONElevator Control
ORGANIZATION
Samantha Power
PERSONUpper Surface of Center Wing
ORGANIZATION