R 1EFF : ALL 1 27-23-51Page 419 1 1 Aug 01/05 1 1 1CES 1
(4) Make sure that the electrical connectors are clean and in the correct
condition.
(5) Make sure that the bolts (7),(21),(24),the bushes (8),(9),(10) and the nuts (12) are clean and in a good condition.
Subtask 27-23-51-560-050-A
B. Preparation of the Replacement Component
(1) Make sure that the PIN - RIGGING (98D27207545000) and the PIN -RIGGING (98D27207545000) (32) are installed in the levers (6) and (16) of the replacement travel limitation unit (5).
(2) Apply SEALANTS (Material No. 09-005) to the component interface of the rudder travel limitation unit (5), the bracket (20) and the support bracket (19).
NOTE : Make sure that the bonding area of the bracket (20) stays____ clean.
Subtask 27-23-51-420-050-A
R C. Installation of the Rudder Travel-Limitation Unit 4CC
R R R R R R R R R WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL_______ MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
R R (1) Install the rudder travel-limitation unit (5) on the bracket (20) as follows:
R R (a) Put the rudder travel-limitation unit (5) in position at the bracket (20). Attach it with the bolts (24) and the washers (23).
(b) TORQUE the bolts (24) to 0.5 m.daN (44.24 lbf.in).
R R R (c) Remove the SEALANTS (Material No. 09-005) that has come out at the connection of the travel limitation unit (5) and the bracket (20).
R 1EFF : 004-049, 055-099, 101-149, 151-199, 1 27-23-51Page 420 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1
R (2) Install the rudder travel-limitation unit (5) on the support bracket
R (19) as follows:
R (a) Put the rudder travel-limitation unit (5) with the bracket (20)
R in position at the support bracket (19). Attach it with the bolts
R (21) and the new tabwashers (22).
(b) TORQUE the bolts (21) to 0.5 m.daN (44.24 lbf.in).
R (c) Safety the bolts (21) with the tabwashers (22).
R (d) Remove the SEALANTS (Material No. 09-005) that has come out at
R the connection of the bracket (20) and the support bracket (19).
(e) Install the bonding strap (18) with the bolt (30) and the nut
(31).
R (f) Make sure that the bonding strap (18) is correctly installed
R (Ref. TASK 20-28-00-912-004).
R
R (3) Connect the control rods (14) and (15) to the travel-limitation unit
R (5) as follows:
R (a) Make sure that the bushes (8) and (9) are tight in the levers (6)
R and (16).
R (b) Apply the BONDING AND ADHESIVE COMPOUNDS (Material No. 08-029) to
R the bushes (8) and (9) and safety them in the levers (6) and (16)
R if necessary.
R
R (c) Put the bush (10) into the bush (9) at the levers (6) and (16).
R (d) Put the control rods (14) and (15) in position at the levers (6)
R and (16).
R (e) Install the bolts (7), the washers (11) and the nuts (12).
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM FLIGHT CONTROLS 飛行操縱2(116)
