(2)
Loosen the nut (15).
(3)
Loosen the unlocked-stop screw (14) until it moves away from the quadrant (11).
(4)
Adjust the unlocked-stop screw (14) until it touches the quadrant (11).
(5)
Tighten the nut (15) to keep the unlocked-stop screw (14) in position.
(6)
Make sure that the unlocked-stop screw (14) touches the quadrant (11).
(7)
Safety the nut (15) with the lockwire, corrosion resistant steel, 0.8 mm (0.032in) dia.
(8)
On the panel 110VU, remove the two wedges from the GRAVITY GEAR EXTN handle (1).
(9)
Release the GRAVITY GEAR EXTN handle (1) from the center console and turn it counterclockwise three turns.
1EFF : ALL 1 32-33-00Page 538 1 1 Nov 01/02R 1 1 1CES 1
Subtask 32-33-00-820-053
H. Rigging Check
(1) Do this check to make sure that the system is correctly rigged:
(a)
Operate the GRAVITY GEAR EXTN handle (1) and turn it as follows:
-clockwise three turns
-counterclockwise three turns
-this gives one complete cycle.
(b)
Operate the GRAVITY GEAR EXTN handle (1) through ten cycles. At the same time make sure that the rods do not touch the structure.
(c)
Fold the GRAVITY GEAR EXTN handle (1) into the center console with the free-fall system in the locked position.
(d)
Make sure that the PIN, RIGGING - RUDDER CONTROL can be freely and easily installed and removed at position Pin 3.
(2) Remove the PIN, RIGGING - RUDDER CONTROL at position Pin 3. Subtask 32-33-00-865-058
J. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GA, 2GA, 52GA.
Subtask 32-33-00-869-069
K. Ground Configuration
(1) If you did the flight configuration precautions, put the aircraft back to the ground configuration (Ref. TASK 32-00-00-860-002).
Subtask 32-33-00-410-054
L. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Close the NLG doors (Ref. TASK 32-22-00-410-001).
(3)
Install the cockpit floor panels 210FF, 210JF (Ref. TASK 53-12-11-400-001).
1EFF : ALL 1 32-33-00Page 539 1 1 Nov 01/02R 1 1 1CES 1
(4) Close the lateral avionics-compartment door 822. Subtask 32-33-00-720-053
M. 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 free-fall extension system (Ref. TASK 32-33-00-720-001).
5. Close-up
________ Subtask 32-33-00-942-055
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.
(4)
Remove the warning notice(s).
1EFF : ALL 1 32-33-00Page 540 1 1 Nov 01/02R 1 1 1CES 1
TASK 32-33-00-820-003
Adjustment of the MLG Free-Fall Extension Cable 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 R
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 tensiometer
No specific warning notice
No specific wedge
98A27801001000 2 RIGGING PIN
98DNSA20208060 2 RIGGING PIN
1EFF : ALL 1 32-33-00Page 541 1 1 Aug 01/05 1 1 1CES 1 B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM LANDING GEAR 起落架5(107)
