3
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3
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EFTA01734227
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.
EFTA00620177_sub_002 - EFTA00620177_200
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
EFTA00612604_sub_002 - EFTA00612604_200
(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.
Forward Cabin
PersonPerson referenced in documents
Lateral Control System
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Samantha Power
PersonIrish-American academic, author and diplomat
Wing Rear Beam
OrganizationOrganization referenced in documents
Valves
PersonSurname reference in documents
Left Engine
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FILTER
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Aileron Control
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Trim Cables
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Rudder Control
OrganizationOrganization referenced in documents
Valve - Operational
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Fuel Shut
PersonPerson referenced in documents
General Dynamics Company
OrganizationOrganization referenced in documents
TSNMO
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Main Fuel Boost Pump
OrganizationOrganization referenced in documents
Spare Squib
PersonPerson referenced in documents
Horizontal Stabilizer Actuator
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Upper Gearbox
OrganizationOrganization referenced in documents
Tail Compartment - Detailed Inspection
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Baggage Compartment
OrganizationOrganization referenced in documents