(2)
Close the NLG doors (Ref. TASK 32-22-00-410-001).
(3)
Close the MLG doors (Ref. TASK 32-12-00-410-001).
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(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.
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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
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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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