F 『 EEFF : ALL E Page 40476-11-41
 E E Feb 01/98 E E ECES E

 F  『
 E  C F M  E
 E  E

 E 56-5B E
 E E
 (9) Disconnect the clamps (9).

 (10) Remove the screws (6) and the washers (5).
 (Ref. Fig. 402/TASK 76-11-41-991-915)

 (11) Remove the plates (4) and (10).

 (12) Remove the pitch trim control mechanism (Ref. TASK 27-41-41-000-001).

 4. Procedure
_________
 (Ref. Fig. 402/TASK 76-11-41-991-915, 403/TASK 76-11-41-991-916, 404/TASK
 76-11-41-991-917, 405/TASK 76-11-41-991-918, 406/TASK 76-11-41-991-919)
 Subtask 76-11-41-480-052

 A. Install the rigging pin RIGGING PIN (98DNSA20208120) (11) in the
 artificial feel unit.

 Subtask 76-11-41-020-051
 B. Removal of the Throttle Control Lever Assembly
 (1) Remove and discard the 2 cotter pins (30).

 (2) Remove the 2 nuts (31), 2 washers (32) and 2 bolts (34). Make sure that the 2 bushes (33) stay bonded.

 (3) Remove the links.

 (4) Remove the 2 screws (23) and the index (22).

 (5) Remove the 2 screws (14) and the index (16).

 (6) Remove the screw (28) and the hollow pin (24).

 (7) Drive out the pin (26). Remove the link (25) and the trigger (27).

 (8) Remove the 2 screws (15) and the 2 hollow pins (13).

 (9) Remove the lever (29): pull the lever to disconnect the connector located inside, at the lever-to-bellcrank junction.

 (10) Remove the lever (12): do the same procedure as for the lever (29).

 (11) Remove the 5 screws (85).

 F 『 EEFF : ALL E Page 40576-11-41
 E E Feb 01/98 E E ECES E

 Ventilation Plates and Clamps
 Figure 402/TASK 76-11-41-991-915

 F 『 EEFF : ALL E Page 40676-11-41
 E E Feb 01/98 E E ECES E

 Rigging Pin Location
 Figure 403/TASK 76-11-41-991-916

 F 『 EEFF : ALL E Page 40776-11-41
 E E Feb 01/98 E E ECES E

 Throttle Control
 Figure 404/TASK 76-11-41-991-917

 F 『 EEFF : ALL E Page 40876-11-41
 E E Feb 01/98 E E ECES E

 Lever Assembly
 Figure 405/TASK 76-11-41-991-918

 F 『 EEFF : ALL E Page 40976-11-41
 E E Feb 01/98 E E ECES E

 Clamps and Connectors of the Throttle Control
 Figure 406/TASK 76-11-41-991-919
 F EEFF :  ALL  『E 76-11-41 Page 410 
E  E  Feb 01/98
 E  E
 ECES  E

 F  『
 E  C F M  E
 E  E
 E  56-5B  E
 E  E

 (12) Lift the lighted label (86) and disconnect the connector 21LFA (19).

 (13) Remove the lighted label (86).

 (14) Remove the 3 screws (17) and the 3 screws (20).

 (15) Remove the housing (18).

 (16) Remove and discard the 8 cotter pins (43).

 (17) Remove the 8 nuts (44), the 8 washers (45) and the 8 screws (46).

 (18) Remove 2 forward covers (63) and the 2 aft covers (42).

 (19) Remove and discard the cotter pin (72).

 (20) Remove the washer (73), the nut (74), the roller (60) the bushing (61), the screw (64), the bushing (66), the roller (65) and the link (25).

 (21) Drive out the pin (59) and remove the rocker (57).

 (22) Remove the screw (76), the washers (78) and (79) and the 2 clamps (77).

 (23) Remove the screws (80), the washers (81) and (83) and the clamps (82).

 (24) Disconnect the connectors 2145VC and 2146VC.

 (25) Put blanking caps on the disconnected electrical connectors.

 (26) Cut and remove the lockwire.

 (27) Remove the nut (37) and the washer (38).

 (28) Pull smoothly the shaft (54) to remove:

 (a) the bushing (39),

 (b) the bellcrank (41),

 (c) the adjustment bushing (49),

 (d) the bellcrank (55),

 (e) the bushing (53),

 F 『 EEFF : ALL E Page 41176-11-41
 E E Feb 01/98 E E ECES E F 『 E C F M E E E E 56-5B E E E (29) Remove the shaft (54).

 (30) On the bellcrank (41), remove the ball bearing (40), the spacer (47) and the bearing (48).

 (31) On the bellcrank (55) remove the bearing (50), the spacer (51) and the bearing (52).

 F 『 EEFF : ALL E Page 41276-11-41
 E E Feb 01/98 E E ECES E

 F 『
 E C F M E
 E E
 E 56-5B E
　
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 ENGINE CONTROLS 發(fā)動(dòng)機(jī)控制(16)