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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
d Inspection G550 AMM Special Inspection (M) 24 MOS 726.9 242 12 May 2015 30 Jun 2017' 11 Mos 02 1.0 282629 Airframe Engine Fuel Shut-off Valve (Left) Operational Check G550 AMM Functional/Ops Test (0) 24 MOS 726.9 242 12 May 2015 30 Jun 2017' 11 Mos 02 1.0 282630 Airframe Engine Fuel Shut-off Valve
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
E. R MAIN PRESS RTN SAMPLE 0.0 0.0 Hrs 2.00 AD8942.82D29Y3 0 0 OL 3817.880400 No 0 26 Nov 2007 Airframe 291501 Hydraulic System Shut-off Valve (Left) Operational Test 3307.8 Hrs 2.00 927 OL 24 MOS 18 Mar 2014 31 Mar 2016' Airframe 29.15.00 (End of Month Item) [1 MOS Window) G-CGUL G550 5176 Current
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.
Manufacturer Labor Warranty MM Ref @=Adlustments (Used Hrs, Cye, Date) Ops Number(s) I Comments Date Type 291501 Hydraulic System Shut-off Valve (Left) Operational Test 726.9 Hrs 2.00 Airframe 29.15.00 02 [End of Month Item) [1 MOS Window) 24 MOS 242 CI_ 12 May2015 30 Jun 2017* 291502 Hydraulic Syst
Entities connected to both Power Transfer Unit and Valve (Left) Operational

Samantha Power
PERSONMain Landing Gear Corrosion
ORGANIZATIONGeneral Dynamics Company
ORGANIZATIONRudder Control
ORGANIZATIONFirst Aid Kit
ORGANIZATIONTrim Cables
ORGANIZATIONAileron Control
ORGANIZATIONWing Rear Beam
ORGANIZATIONElevator Control
ORGANIZATIONFuel Shut
PERSONMain Fuel Boost Pump
ORGANIZATIONTrash Receptacle Enclosure
ORGANIZATIONCowl Doors
ORGANIZATIONLanding Gear Emergency
ORGANIZATIONEmpennage FS
ORGANIZATIONMain Landing Gear Components
ORGANIZATIONTSNMO
ORGANIZATIONOps Number(s
ORGANIZATIONWheel Steering Unit - Lubrication
ORGANIZATIONMain Landing
LOCATION