____ inspection holes, the eye-ends are in safety.

 (g)
 Tighten the lock-nuts (7) of the tie-rod (8).

 (h)
 Safety the lock-nuts (7) with MISCELLANEOUS (Material No. 19-010) (Ref. TASK 20-11-11-911-001).

 (9) Adjust the release lever (16): (Ref. Fig. 409A/TASK 25-62-43-991-008-A)
 (a)
 If necessary loosen the bolt (18).

 (b)
 Move the lever (19) to adjust the distance between POINT "X" and POINT "Y" on the release lever (16) to 73.0 +0.5 -0.5 mm (2.8740 +0.0196 -0.0196 in.).

 NOTE : Measure the distance with a slide gage.
____
 (c)
 Tighten the bolt (18).

 (d)
 Safety the bolts (17) and (18) with MISCELLANEOUS (Material No. 19-010) (Ref. TASK 20-11-11-911-001).

 (10) Adjust the clearence between the release lever and the release pin of the emergency hatch:
 (Ref. Fig. 409A/TASK 25-62-43-991-008-A)
 (a)
 Put the emergency-exit hatch in the installed position
 (Ref. TASK 52-21-11-400-001).

 (b)
 Cut, remove and discard the lock-wire from the lock-nut (10) of the setscrew (9).

 (c)
 Loosen the lock-nut (10) of the setscrew (9).

 (d)
 Make sure that the release pin (20) of the emergency hatch is in the "ARMED" Position (see DETAIL "F").

 (e)
 Make sure that the double lever touches the setscrew (9) at POINT "C" (see DETAIL "A").

 (f)
 Move the emergency hatch until you can measure the distance between the release lever (14) and the release pin (20) (see DETAIL "G").

 (g)
 Turn the setscrew (9) and adjust the distance between the release lever (14) and the release pin (20) to 1.0 +0.5 -0.5 mm (0.0393 +0.0196 -0.0196 in.).

 NOTE : Measure the distance with a feeler gage.
____
 (h)
 Tighten the lock-nut (10) of the setscrew (9).

 (i)
 Safety the lock-nut (10) with MISCELLANEOUS (Material No. 19-010) (Ref. TASK 20-11-11-911-001).

 (j)
 Remove the emergency-exit hatch.

 (11)
 Connect the flexible control-cable: (Ref. Fig. 404A/TASK 25-62-43-991-003-A)

 (a)
 Apply COMMON GREASE (Material No. 04-004) on the clevis-pin (9).

 (b)
 Put the flexible control-cable (11) together with the washers

 (10) in position and install the clevis-pin (9).

 (c)
 Put the washer (8) in position and install the new cotter pin (7).

 (12)
 Adjust the flexible control-cable: (Ref. Fig. 409A/TASK 25-62-43-991-008-A)

 (a)
 Cut, remove and discard the lock-wire from the lock-nuts (11) and the sleeve adjust-nuts (12) of the flexible control-cable (13).

 (b)
 Loosen the lock-nuts (11) of the flexible control-cable (13).

 (c)
 Turn the sleeve adjust-nut (12) and adjust the distance at the end of the flexible control-cable (13) to 11.5 +1.7 -1.7 mm (0.4527 +0.0669 -0.0669 in.).

 NOTE : Measure the distance at the outer end of the flexible
____ control-cable (13) (see DETAIL "J") with a slide gage.
 (d)
 Do a check of the adjusted distance at the end of the flexible control-cable (13):

 (e)
 Tighten the lock-nuts (11) of the flexible control-cable (13).

 (f)
 Safety the lock-nuts (11) and the sleeve adjust-nut (12) with MISCELLANEOUS (Material No. 19-010) (Ref. TASK 20-11-11-911-001).

 1_ Pull the end of the flexible control-cable (13) three times.
 2_ Measure the distance at the end of the flexible control-cable
 (13) with a slide gage.
 3_ If the distance is not in the limits of 11.5 +1.7 -1.7 mm
 (0.4527 +0.0669 -0.0669 in.), do the steps (c) and (d) again.

 (13) Adjust the cable-travel of the flexible control-cable: (Ref. Fig. 409A/TASK 25-62-43-991-008-A)
 (a)
 Put the emergency-exit hatches in the installed position (Ref. TASK 52-21-11-400-001).

 (b)
 Install the TEST TOOL - RELEASE CABLE , ESCAPE SLIDE (TLW101) on the flexible control assembly (see DETAIL "K"):

 1 Remove the protective plug and the two collets from the test
_ tool.

 2_ Carefully engage the test tool into the related slot of the
 flexible control-cable (13).
 3_ Put the two collets in position, on the connection of the test
 tool and the flexible control-assembly.
 4_ Move the knurled sleeve-nut up and install it to the flexible
　
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 EQUIPMENT/FURNISHINGS 設備4(108)