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14 31 Jul 2016 5 Mos 240122 Emergency Battery Power System (Right) 6550 AMM 2320.2 * Airframe MA
g Hrs/Cyc/Cal Logbook I App Serial Number Section Page Mfg Ref Number Notes Revision Date Issued 552006 * Airframe MAN Mfg#: 55.23-00 Elevator Hinge (Right) - Detailed Inspection Notes: f 144 MOS Initial Req.] [End of Month Item) [1 MOS Window) G550 AMM 05.20-00 31 Aug 2003 144MOS"/96M OS 0
14 31 Jul 2016 5 Mos 240122 Emergency Battery Power System (Right) 6550 AMM 2320.2 * Airframe MA
g Hrs/Cyc/Cal Logbook I App Serial Number Section Page Mfg Ref Number Notes Revision Date Issued 552006 * Airframe MAN Mfg#: 55.23-00 Elevator Hinge (Right) - Detailed Inspection Notes: f 144 MOS Initial Req.] [End of Month Item) [1 MOS Window) G550 AMM 05.20-00 31 Aug 2003 144MOS"/96M OS 0
l 2016 5 Mos $1.842.67 4.0 Standby Electrical Power System Operational Test 2676.5 242O05 1312 1.
tor Hinge (Left) - Detailed Inspection 0.0 552005 0 26.0 144 MOS 02 Jun 30 Jun 4 Mos Airframe 2004 2016 G550 AMM Special Inspection (M) Elevator Hinge (Right) - Detailed Inspection 0.0 552006 0 26.0 144 MOS 02 Jun 30 Jun 4 Mos Airframe 2004 2016 G550 AMM Special Inspection (M) N62MS G
Entities connected to both Samantha Power and Elevator Hinge
Wing Rear Beam
ORGANIZATIONFirst Aid Kit
ORGANIZATIONAileron Control
ORGANIZATIONRudder Control
ORGANIZATIONMain Fuel Boost Pump
ORGANIZATIONTrim Cables
ORGANIZATIONCowl Doors
ORGANIZATIONFuel Shut
PERSONMain Landing Gear Corrosion
ORGANIZATIONService Life
ORGANIZATIONAir Turbine Starter Oil - Change
ORGANIZATIONPower Transfer Unit
ORGANIZATIONAir Data Module
ORGANIZATIONEmpennage FS
ORGANIZATIONUpper Surface of Center Wing
ORGANIZATIONAir Data System No.
ORGANIZATIONTrash Receptacle Enclosure
ORGANIZATIONRudder External
ORGANIZATIONWing Rear Beam (Left
ORGANIZATIONElevator Control
ORGANIZATION