(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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