(2) Connect the support bracket (19) to the structure as follows:
(a) Hold the support bracket (19) in position at the structure.
(b) Install the bolts (24), the washers (25) and the nuts (26) at the top connection points to the structure.
(c) Install the bolts (28),(29), the washers (25) and the nuts (26) at the bottom connection points to the structure.
(d) TORQUE the nuts (26) to 0.7 m.daN (61.94 lbf.in) and then loosen the nuts (26), if necessary, to the next cotter pin hole.
(e) Safety the nuts (26) with the cotter pins (27).
(f) Put the bonding strap (18) in position at the structure and attach it with the screw (30) and the nut (31) (Ref. TASK 20-28-00-912-004).
R R R (g) Apply the STRUCTURE PAINTS (Material No. 16-021) to the connections of the bonding strap (18) to the support bracket (19) and the structure.
R R (h) Remove the SEALANTS (Material No. 09-018) that has come out at the connection of the support bracket (19) to the structure.
R R (i) Apply a bead of the STRUCTURE PAINTS (Material No. 16-021) at the connection of the support bracket (19) to the structure.
(3) Connect the centering rod (3) and the control rod (23) to the bellcrank assembly (4) as follows:
R R (a) Make sure that the bushes (8) and (9) are tight in the arms of the bellcrank assembly (4).
R R R R (b) Apply the BONDING AND ADHESIVE COMPOUNDS (Material No. 08-029) and safety them in the arms of the bellcrank assembly (4) if necessary.
R (c) Put the bushes (10) into the bushes (9) in the arms of the bellcrank assembly (4).
R (d) Put the centering rod (3) and the control rod (23) in position in the arms of the bellcrank assembly (4).
R (e) Install the bolts (7), the washers (11) and the nuts (12).
R (f) Make sure that the bushes (8), (9) and (10) are correctly
R installed in the arms of the bellcrank assembly (4).
R
R (g) TORQUE the nuts (12) to 0.7 m.daN (61.94 lbf.in) and then loosen
the nuts (12), if necessary, to the next cotter pin hole.
R (h) Safety the nuts (12) with the cotter pins (13).
R (4) 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).
R (f) Make sure that the bushes (8), (9) and (10) are correctly
R installed in the levers (6) and (16).
R
R (g) TORQUE the nuts (12) to 0.7 m.daN (61.94 lbf.in) and then loosen
the nuts (12), if necessary, to the next cotter pin hole.
R (h) Safety the nuts (12) with the cotter pins (13).
R (5) Make sure that the electrical connectors are clean and in the correct
R condition.
R (6) Remove the blanking caps and connect the electrical connectors (17).
R Do this on the bottom of the rudder travel limitation unit (5).
R (7) Install the bonding leads (36) with the bolt (35) and the nut (34) if
R removed (Ref. TASK 20-28-00-912-004). Do this on the electrical
R connectors (17).
R R (8) Safety the electrical connectors (17) to the bonding leads (36) with the lockwire MISCELLANEOUS (Material No. 19-018).
R R (9) Apply the STRUCTURE PAINTS (Material No. 16-021) to the connections of the bonding leads (36) and the electrical connectors (17).
R R (10) If you have removed the cover foil from the opening behind the rudder travel- limitation unit (5), do the subsequent steps:
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱2(115)
