(2)
 Close the NLG doors (Ref. TASK 32-22-00-410-001).

 (3)
 Close the MLG doors (Ref. TASK 32-12-00-410-001).

 1EFF : ALL 1 32-33-00Page 561 1 1 Aug 01/05 1 1 1CES 1

 (4)
 Install the cockpit floor panels 211FF, 211JF (Ref. TASK 53-12-11-400-001).

 (5)
 Install the passenger compartment floor panels 241EF, 242FF (Ref. TASK 53-32-12-400-002).

 (6)
 Install the forward cargo-compartment ceiling-panels 131MC, 131NC.

 (7)
 Close the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-002).

 **ON A/C ALL
 Subtask 32-33-00-720-054
 Y. Test CAUTION : MAKE SURE THAT THE RIGGING PINS ARE REMOVED BEFORE OPERATION OF
_______ THE FREE FALL SYSTEM. DAMAGE WILL OCCUR IF THE RIGGING PINS ARE INSTALLED DURING SYSTEM OPERATION.
 (1) Do a functional test of the landing-gear free-fall extension system (Ref. TASK 32-33-00-720-001).
 5. Close-up
________ Subtask 32-33-00-942-057
 A. Removal of Equipment
 (1)
 Remove the safety barriers.

 (2)
 Remove the warning notice(s).

 (3)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 1EFF : ALL 1 32-33-00Page 562 1 1 Aug 01/05R 1 1 1CES 1

 TASK 32-33-00-820-004
 Adjustment of the MLG Free-Fall Extension Mechanical System
 WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
 -
THE FLIGHT CONTROLS

 -
THE FLIGHT CONTROL SURFACES

 -
THE LANDING GEAR AND THE RELATED DOORS

 -COMPONENTS THAT MOVE.
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
 1. Reason for the Job
__________________
 Self Explanatory
 NOTE : Adjustment of the free-fall system must be made with the aircraft
____
 weight on the landing gear (weight on wheels).

 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) No specific safety barriers No specific warning notice No specific wedge No specific Torque Wrench : range 0.00 to 1.20 m.daN
 (0.00 to 9.00 lbf.ft) 98A27801001000 1 RIGGING PIN 98A27901002000 1 PIN, RIGGING - RUDDER CONTROL 98A32301000000 1 RIGGING PIN 98DNSA20208040 1 RIGGING PIN 98DNSA20208060 4 RIGGING PIN
 1EFF : ALL 1 32-33-00Page 563 1 1 Aug 01/05R 1 1 1CES 1

 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific  lockwire, corrosion resistant steel, 0.8 mm (0.032 in) dia
 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
07-11-00-581-001  Lifting for Aircraft Maintenance Operations
 07-11-00-586-002  Lowering of the Aircraft for Maintenance Operations
 24-41-00-862-002  De-energize the Aircraft Electrical Circuits Supplied
 from the External Power
 32-00-00-481-001  Installation of the Safety Devices on the Landing
 Gears
 32-00-00-860-001  Flight Configuration Precautions with Electrical
 Power
 32-00-00-860-002  Ground Configuration after Flight Configuration with
 Electrical Power
 32-12-00-010-001  Open the Main Gear Doors for Access
 32-12-00-410-001  Close the Main Gear Doors after Access
 32-22-00-010-001  Nose Gear Doors - Ground Doors Opening
 32-22-00-410-001  Nose Gear Doors - Ground Doors Closing
 32-33-00-200-001  Check Tension of Free-Fall Mechanism Cable
 32-33-00-720-001  Functional Check of Free-Fall Extension
 32-33-00-820-001  Adjustment of the NLG Free-Fall Extension Cable
 System
 32-33-00-820-002  Adjustment of the NLG Free-Fall Extension Mechanical
 System
 32-33-00-820-003  Adjustment of the MLG Free-Fall Extension Cable
　
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