(2)
Apply SEALANTS (Material No. 09-018) or SEALANTS (Material No. 09-019) to the plain shank and flange of the bearing housing (12) and to the bolts (11).
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 27-54-55-420-057
C. Installation of the Flap-Actuator Lever Assembly
(1)
Install the bearing housing (12) in the outboard bracket (14) and install the bolts (11) with the heads inboard.
(2)
Install the washer (19) and the ring nut (18) and tighten the ring nut (18) to pull the bearing housing (12) into position. Remove the ring nut (18) and the washer (19).
(3)
Install the nuts (20) and safety with new cotter-pins (21).
(4)
Apply SEALANTS (Material No. 09-018) or SEALANTS (Material No. 09-019) to the mating face of the washer (19).
(5)
Install the washer (19) on the bearing housing (12).
(6)
Apply COMMON GREASE (Material No. 04-022) to the ring nut (18).
(7)
Install the ring nut (18) on the bearing housing (12).
(8)
TORQUE the ring nut (18) with the SPANNER-FLAP LEVER TRACKS 2 AND 3 (98D27504028000) to between 1.4 and 1.5 m.daN (10.32 and 11.06 lbf.ft).
(9)
If necessary, drill a 2.5 mm (0.10 in.) hole for the cotter pin (15) in an applicable position on the bearing housing (12). Remove all unwanted material from the area.
(10)
Safety the ring nut (18) with a new cotter-pin (15).
(11)
Apply COMMON GREASE (Material No. 04-022) to the bearing surfaces of the lever (5).
(12)
Turn the lever (5) through 90 deg. and install it in the bearing housing (12).
(13)
Apply SEALANTS (Material No. 09-018) or SEALANTS (Material No. 09-019) to the mating surface of the bearing housing (3) and on the bolt (2).
(14)
Install the bearing housing (3), the bolt (2) and the nut (1).
(15)
Apply COMMON GREASE (Material No. 04-022) to the retention plate (13) and to the bolt (4).
(16)
Install the retention plate (13), the bolt (4) and the nut (16).
(17)
TORQUE the nut (16) to between 1.4 and 1.5 m.daN (10.32 and 11.06 lbf.ft)
(18)
Manually operate the lever (5) and make sure that it moves freely.
(19)
Safety the nut (16) with the new cotter pin (17).
(20)
Remove the adjustable strut.
(21)
Move the flap to align the flap link arms (9) to the levers (5) at Track 3 and Track 4.
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-54-55Page 477 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
(22)
Apply COMMON GREASE (Material No. 04-004) to the bolts (10) and the nuts (7).
(23)
At Tracks 3 and 4:
(Ref. Fig. 403/TASK 27-54-55-991-002)
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-210,
(Ref. Fig. 404/TASK 27-54-55-991-003) R **ON A/C 106-149, 211-299, 401-499,
(Ref. Fig. 404A/TASK 27-54-55-991-003-A) R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(a)
Install the bolts (10), the washers (8) and the nuts (7).
(b)
TORQUE the nuts (7) to between 7.6 and 8.5 m.daN (56.04 and 62.68 lbf.ft) and safety with new cotter-pins (6).
(24)
Do a check of the flap rigged position (Ref. TASK 27-51-00-820-003).
(25)
At Tracks 3 and 4, apply STORAGE PRESERVATION (Material No. 15-007) to the bolts (10) and the nuts (7) after assembly.
(26)
Install the Track 3 actuator 6221CM(6271CM) (Ref. TASK 27-54-49-400-003)
**ON A/C 301-399,
Subtask 27-54-55-420-057-A
C. Installation of the Flap-Actuator Lever Assembly
(1)
Install the bearing housing (12) in the outboard bracket (14) and install the bolts (11) with the heads inboard.
(2)
Install the washer (19) and the ring nut (18) and tighten the ring nut (18) to pull the bearing housing (12) into position. Remove the ring nut (18) and the washer (19).
(3)
Install the nuts (20) and safety with new cotter-pins (21).
(4)
Apply SEALANTS (Material No. 09-018) or SEALANTS (Material No. 09-019) to the mating face of the washer (19).
(5)
Install the washer (19) on the bearing housing (12).
(6)
Apply COMMON GREASE (Material No. 04-022) to the ring nut (18).
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 FLIGHT CONTROLS 飛行操縱6(8)
