R 1EFF : 301-399, 1 27-21-44Page 417 1 1 May 01/04 1 1 1CES 1
R R (c) Adjust the length of the rod (17) until you can install the bolt (21).
R R R (d) Engage the lockwashers (14) and (15) and TORQUE the nuts (13) and (16) to 1.374 m.daN (10.13 lbf.ft). Safety them with Lockwire corrosion resistant steel dia 0.8 mm (0.03 in.).
R R (25) Install the washer (22), install and tighten the nut (23). Safety it with the new cotter pin (24).
R R (26) Remove the PIN, RIGGING - RUDDER CONTROL (98A27901002000) (35) from the yaw/brake bellcranks of the CAPT and F/O.
R **ON A/C ALL
Subtask 27-21-44-080-050
B. Remove the PIN, RIGGING - RUDDER CONTROL (98A27901002000) (36) from the tension regulator.
Subtask 27-21-44-710-050
C. Test of the CAPT Yaw/Brake Bellcrank
(1) Do the operational test of the rudder mechanical control (Ref. TASK 27-24-00-710-001).
(2) Do the operational test of the normal braking system (operational check of the pedals) (Ref. TASK 32-42-00-710-001).
(3) Do the operational test of the alternate braking system (operational check of the pedals) (Ref. TASK 32-43-00-710-001).
5. Close-up________
Subtask 27-21-44-942-050
A. Put the aircraft back to the serviceable condition.
(1) Make sure that the work area is clean and clear of tool(s) and other items.
(2) Remove the warning notice(s).
Subtask 27-21-44-410-050
B. Close Access
(1)
Close the access door 811.
(2)
Remove the access platform(s).
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TASK 27-21-44-000-002
Removal of the F/O Yaw/Brake Bellcrank
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific warning notice
No specific access platform 1.5 m (4 ft. 11 in.)
98A27901002000 1 PIN, RIGGING - RUDDER CONTROL
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
27-21-44-991-001 Fig. 401
**ON A/C 301-399,
27-21-44-991-001-A Fig. 401A
**ON A/C ALL
27-21-44-991-004 Fig. 404
27-21-44-991-005 Fig. 405
3. Job Set-up
__________
Subtask 27-21-44-941-053
A. Put the warning notice
(1) Put a warning notice to tell persons not to pressurize the Green and the Yellow hydraulic systems.
(2) Put a warning notice to tell persons not to operate the pedals. Subtask 27-21-44-010-051
B. Get Access
(1)
Put the access platform in position.
(2)
Open the access door 811.
4. Procedure
_________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 401/TASK 27-21-44-991-001)
**ON A/C 301-399,
(Ref. Fig. 401A/TASK 27-21-44-991-001-A)
**ON A/C ALL
(Ref. Fig. 404/TASK 27-21-44-991-004, 405/TASK 27-21-44-991-005)
Subtask 27-21-44-480-051
A. Install the PIN, RIGGING - RUDDER CONTROL (98A27901002000) (36) on the tension regulator.
F/O Yaw/Brake Bellcrank Figure 404/TASK 27-21-44-991-004
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F/O Yaw/Brake Bellcrank 中國航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱2(29)
