(5)
On the cable(s) to be removed, continue to loosen the turnbuckle(s)
(41) until the cable(s) is/are disconnected.
(6)
Temporarily attach the cable(s) (37) and/or (38) to the structure.
(7)
Release the cable(s) (39) and/or (40) from the pulley (83) and remove it/them from the aircraft.
1EFF : ALL 1 32-33-16Page 431 1 1 Feb 01/03R 1 1 1CES 1
TASK 32-33-16-400-002
Installation of the MLG Free-Fall Extension Cables
WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______
NOTICES ARE IN POSITION.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
1. Reason for the Job
__________________
R R Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers
No specific warning notice
No specific wedge
98A27801001000 1 RIGGING PIN
98DNSA20208060 1 RIGGING PIN
98DNSA20208150 1 RIGGING PIN
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-002 USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00)
Material No. 09-019 USA AMS 3267/3
LOW ADHESION CORROSION INHIBITING SEALANT
(Ref. 20-31-00)
Material No. 11-026 GB DEF-STAN 68-148/1
SOLVENT GENERAL PURPOSE (Ref. 20-31-00)
Material No. 16-003 F ASNB70720
COATING (OBSOLETE USE 16-021) (Ref. 20-31-00)
Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
1EFF : ALL 1 32-33-16Page 432 1 1 May 01/04 1 1 1CES 1
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
Material No. 19-010 USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
4 8 11 14 54 55 55 77 77 80 cotter-pin cotter-pins cotter pin cotter pin cotter-pin cotter-pin cotter-pin cotter-pin cotter-pin cotter-pin 32-33-01 10A-05032-33-03 30 -03032-33-03 30 -03032-33-01 02B-10032-33-03 38 -03032-33-03 03 -17032-33-03 03B-17032-33-03 03 -17032-33-03 03B-17032-33-03 36 -060
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R R R R R 21-31-00-710-002 24-41-00-862-002 32-00-00-481-001 32-00-00-481-002 32-00-00-860-001 32-00-00-860-002 32-12-00-010-001 32-12-00-410-001 32-33-00-200-001 32-33-00-720-001 Operational Test of the Pressure Control and MonitoringDe-energize the Aircraft Electrical Circuits Supplied from the External PowerInstallation of the Safety Devices on the Landing GearsInstallation of the Safety Devices on the Landing Gear Doors Flight Configuration Precautions with Electrical Power Ground Configuration after Flight Configuration with Electrical PowerOpen the Main Gear Doors for AccessClose the Main Gear Doors after Access Check Tension of Free-Fall Mechanism CableFunctional Check of Free-Fall Extension
1EFF : ALL 1 32-33-16Page 433 1 1 May 01/05 1 1 1CES 1 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
32-33-00-820-003 52-30-00-860-001 52-30-00-860-002 52-41-00-410-002 53-12-11-000-001 Adjustment of the MLG Free-Fall Extension Cable SystemOpen the FWD or AFT Cargo-Compartment Door with the Yellow Electric PumpClose the FWD or AFT Cargo-Compartment Door with the Yellow Electric PumpClose the Avionics Compartment Doors after AccessRemoval of the Cockpit Floor Panels from FR1 Thru FR12
53-12-11-400-001 Installation of the Cockpit Floor Panels from FR1 thru FR12
53-12-12-000-001 Removal of the Cabin Floor Panels from FR12 thru FR24
53-12-12-400-001 Installation of the Cabin Floor Panels from FR12 thru
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