5
Shared Docs
5
Same-Page
5 / 5
Mentions
Hrs 334 01 Jun 2016 01 1.0 292502 Airframe Power Transfer Unit Manifold Differential Pressure Indi
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
Functional/0as Teal (0) 02 Standby Electrical Power System - Operational Tesl 3971.1 242005 1318
spection 0550 AMM Special Inspection (M) 24 MOS 3971.1 1318 09 Jun 2013 31 Jan 2015' -95 Days 02 1.0 282629 Airframe Engine Fuel Shut-off Valve (Left) Operational Check 0550 AMM Functional/0es Tint (0) 24 MOS 3971.1 1318 09 Jun 2013 31 Jan 2015' -98 Days 02 1.0 282630 Airframe Engine Fuel Shut-off v
.01 verified by PO619 26 Nov 2007 275201 Flap Power Drive Unit Removal / Installation 0.0 0.0 Hrs
282628 Fuel Ejector Pump and Check Valves (Right) • Inspection 0.0 Hrs 2.00 Airframe 28.26.07 0 CI_ 26 Nov 2007 282629 Engine Fuel Shut-off Valve (Left) Operational Check 3307.8 Hrs 1.00 Airframe 28.26.09 [End of Month Item] [1 MOS Window] 24 MOS 927 CI_ 17 Mar 2014 31 Mar 2016 282630 Engine Fuel Shut-
.21.03 ver by pq164 4.00 64824.610800 292201 Power Transfer Unit Hydraulic Pump - Removal / Install
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
L 11 Feb 2013 2.00 0.000000 291040 Airframe Power Transfer Unit Manifold Filter and Bowl Removal /
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 Samantha Power and Valve (Left) Operational
Leon Black
PERSONVALVE
ORGANIZATIONGeneral Dynamics Company
ORGANIZATIONOps Number(s
ORGANIZATIONTSNMO
ORGANIZATIONWing Rear Beam
ORGANIZATIONAvg Manhours
PERSONTrim Cables
ORGANIZATIONAileron Control
ORGANIZATIONRudder Control
ORGANIZATIONFirst Aid Kit
ORGANIZATIONFuel Shut
PERSONCowl Doors
ORGANIZATIONNDT Inspection
ORGANIZATIONPower Transfer Unit
ORGANIZATIONMain Landing Gear Corrosion
ORGANIZATIONAl Rights Reserved
ORGANIZATIONMain Fuel Boost Pump
ORGANIZATIONForward Cabin
PERSONEmpennage FS
ORGANIZATION