R 1EFF : 001-004, 051-054, 1 32-21-13Page 423 1 1 May 01/05 1 1 1CES 1

 (c)
 TORQUE the valve (1) to between 1 and 1.25 m.daN (88.49 and

 110.61 lbf.in).

 (d)
 Install the stop plate (4), align it with a hole of the plate (5) and the related thread of the nut (7).

 (e)
 Install the new lockwasher (3) and the screw (2).

 (f)
 TORQUE the screw (2) to between 0.25 and 0.35 m.daN (22.12 and

 30.97 lbf.in) and safety with the lockwasher (3).
 (11)
 Remove the lifting trolley.

 (12)
 Do the replenishment of the NLG shock absorber (Ref. TASK 12-12-32-611-005).

 (13)
 Pressurize the shock absorber with nitrogen to slowly extend the shock absorber and make sure that the cams are engaged (Ref. TASK 12-14-32-614-004).

 (14)
 With the shock absorber fully extended, make sure that the wheel axle is perpendicular to the aircraft centerline.

 NOTE : In the fully extended position of the shock absorber, the NLG
____ is automatically centered (the nose wheel steering is in zero position).
 (a) Make sure that the dimension H of the extended part of the NLG sliding tube between the lower area of the NLG lower bearing and the upper surface of the towing fitting lug is between 454.6 mm (17.8976 in.) and 445.6 mm (17.5433 in.). (Ref. Fig. 404/TASK 32-21-13-991-009)
 (15)
 Try to turn the NLG shock absorber around its vertical axis to make sure that the anti-rotation lugs are engaged in the slots of the back plate:

 (a)
 the shock absorber must not turn.

 (b)
 If you can turn the shock absorber, this shows that the anti-rotation lugs are not engaged in the slots because the centering cams are not correctly installed.You must remove the shock absorber to install the cams in the correct position.

 (16)
 Install the stop (72), the bolts (74), the washers (71) and (73) and the nuts (70). Tighten the nuts (70).

R 1EFF : 001-004, 051-054, 1 32-21-13Page 424 1 1 May 01/05 1 1 1CES 1

 NLG Shock Absorber - Clearance Figure 404/TASK 32-21-13-991-009 
R 1EFF : 1 1 1CES  ALL  1 111 32-21-13 Page 425 May 01/05

 (17)
 Install the support (67) assembled with the electrical connector (68).

 (18)
 Install the screw (69), the washer (52) and the nut (51). Tighten the nut (51).

 (19)
 Install the pin (63), the washer (56) and the nut (57). Tighten the nut (57).

 NOTE : Make sure that there are no hard points when you moved the
____
 torque links through their full travel.

 (20)
 Apply a layer of COMMON GREASE (Material No. 04-022) to the washers (58), (59) and (60) and to the pin (61).

 (21)
 Align the bores of the torque links and install the washers (58),

 (60) and the washer (59).

 (22)
 Install the pin (61).

 (23)
 Make sure that the play at the torque link hinges is correct (Ref. TASK 32-21-00-200-003).

 (24)
 Do the torque procedure on the nut (53)

 (a)
 Apply a layer of SPECIAL MATERIALS (Material No. 05-047) to the washer (55) and install it on the pin (61).

 (b)
 Apply a layer of SPECIAL MATERIALS (Material No. 05-047) to the threads of the nut (53) and install it.

 (c)
 TORQUE the nut (53) to 9 m.daN (66.37 lbf.ft) and loosen the nut (53). Do this three times.

 (d)
 Loosen the nut (53) to get a clearance between 0 mm (0.0000 in.) and 0.1 mm (0.0039 in.).

 (e)
 Make sure that you can align a hole of the nut (53) with the slot of the pin (61) and keep the clearance given above. If not:

 -loosen the nut (53),
 -remove the washer (55),
 -adjust the thickness of the washer (55) to get the clearance given above with a hole of the nut (53) aligned with the slot of the pin (61).
R 1EFF : 001-004, 051-054, 1 32-21-13Page 426 1 1 May 01/05 1 1 1CES 1 NOTE : The total thickness of the washer (55) (shoulder included)

____ must not be less than 4 mm (0.1574 in.). If the thickness of the washer (55) is less than 4 mm (0.1574 in.), replace it with a new washer (55).
 -
do a passivating treatment on the reworked surface (Ref. CMM 320901),

 -
do the torque procedure on the nut (53) again.

 (f)
 Apply a layer of SPECIAL MATERIALS (Material No. 05-047) to the threads of the screw (54).

 (g)
 Install the screw (54), the washer (77), the nut (76) and tighten it.
　
中國航空網(wǎng) m.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 LANDING GEAR 起落架3(84)