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1.00 $1,432.86 $1,432.86 Part Ref: 501.107542 POWER SUPPLY Step: 12.55.1 Completed Removed Attitud
o be within limits and no other defects noted. All work done IAW GlIB MM 27-01-00. Labor USD: No Charge N/ C Discrepancy: 12.119 CMP GIIB 270510 Elevator Control System - Operational Test Resolution: COMPLIED WITH CMP GlIB 270510 Elevator Control System - Operational Test. All Maintenence Performed In Reference To GIIB AMM 27-01.00.
.01 verified by PO619 26 Nov 2007 275201 Flap Power Drive Unit Removal / Installation 0.0 0.0 Hrs
SW TSNMO TSOMO TSRMO Manufacturer Labor Warranty MM Ref @=Adlustments (Used Hrs, Cye, Date) Ops Number(s) 1 Comments Date Type 273005 Elevator Control System - Operational Test Airframe 27.30.00 2849.4 Hrs 833 Cit 11 Apr 2013 8.00 Elevator Actuator Load Relief Bungee Assembly (Left) • 273006 0.0 Removal / Installat
0 11 Feb 2013 Airframe 27.51.01 275201 Flap Power Nye Unit - Removal / Installation 0.0 0.0 Hrs
(Right) - Removal/ Installation 0.0 0.0 its 90.00 1159CS52093.422 612 0 0 CtL 618961.948800 No 0 11 Feb 2013 Airframe 27.31.21 273005 Elevator Control System - Operational Test 726.9 Hrs 8.00 242 OL 21 May 2015 Airframe 27.30.00 273006 Elevator Actuator Load Relief Bungee Assembly (Left) - Removal / Installation 0.
Entities connected to both Samantha Power and Elevator Control System - Operational Test
VALVE
ORGANIZATIONFILTER
ORGANIZATIONGeneral Dynamics Company
ORGANIZATIONTSNMO
ORGANIZATIONWing Rear Beam
ORGANIZATIONOps Number(s
ORGANIZATIONAvg Manhours
PERSONAileron Control
ORGANIZATIONRudder Control
ORGANIZATIONTrim Cables
ORGANIZATIONMain Fuel Boost Pump
ORGANIZATIONFuel Shut
PERSONForward Cabin
PERSONSpare Squib
PERSONLongitudinal Control System Friction
ORGANIZATIONBaggage Compartment
ORGANIZATIONOutboard Flap Actuator
ORGANIZATIONLateral Control System
ORGANIZATIONValve - Operational
ORGANIZATIONTail Compartment - Detailed Inspection
PERSON