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时间:2011-03-27 08:52来源:蓝天飞行翻译 作者:admin
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 Subtask 54-57-17-010-050
 B. Get Access
 (1) Open the fan cowl doors (Ref. TASK 71-13-00-010-040) FOR 1000EM1 437AL, 438AR FOR 1000EM2 447AL, 448AR.
 (2) Open the thrust reverser doors (Ref. TASK 78-36-00-010-040) FOR 1000EM1 451AL, 452AR FOR 1000EM2 461AL, 462AR. 
R  (3) Put an access platform: 
R  (a) In zone 410 for the left pylon. 
R  (b) In zone 420 for the right pylon.
 Subtask 54-57-17-040-050
 C. Aircraft Maintenance Configuration
 (1) Make the thrust reverser unserviceable (Ref. TASK 78-30-00-481-041).
 4. Procedure_________
 Subtask 54-57-17-020-050
 A. Removal of the Fittings (Ref. Fig. 401/TASK 54-57-17-991-001)
 (1) Remove the fitting (6).
 (a) Remove the nut (7) and the bolt (9) to disconnect the tube end (8) from the fitting (6).

 

R  Fitting at RIB1 Figure 401/TASK 54-57-17-991-001
 1EFF : 1 1 1CES  ALL  1 111 54-57-17 Page 403 Aug 01/05

 

 (b) Remove the nut (1), the bolt (4), the washer (3), the stirrup (2) and disconnect the cowl stop assembly (5). 
R R  (c) Remove the nuts (21), the washers (20) and the bolts (22) that attach the fitting (6) to the bracket (23).
 CAUTION : DO NOT REMOVE THE BOLTS WHICH ATTACH THE FITTING TO THE_______ FWD PYLON-TO-ENGINE ATTACH FITTING. REMOVE THE NUTS ONLY. - IF YOU REMOVE THE BOLTS, YOU CAN CAUSE DAMAGE TO THE BORES. 
R  (d) Remove the nuts (10) and the fitting (6).
 (2) Remove the fitting (12).
 (a) Remove the nut (15) and the bolt (13) to disconnect the tube end (14) from the fitting (12).
 (b) Remove the nut (16), the bolt (19), the washer (18), the stirrup (17) and disconnect the cowl stop assembly (5). 
R R  (c) Remove the nuts (26), the washers (25) and the bolts (24) that attach the fitting (12) to the bracket (23).
 CAUTION : DO NOT REMOVE THE BOLTS WHICH ATTACH THE FITTING TO THE_______ FWD PYLON-TO-ENGINE ATTACH FITTING. REMOVE THE NUTS ONLY. - IF YOU REMOVE THE BOLTS, YOU CAN CAUSE DAMAGE TO THE BORES. 
R  (d) Remove the nuts (11) and the fitting (12).


 TASK 54-57-17-400-001


 Installation of the Fittings at RIB1
 1.
 Reason for the Job

__________________
 Self Explanatory


 2.
 Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE  QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific  Torque Wrench : range 2.00 to 20.00 m.daN
 (15.00 to 150.00 lbf.ft)
 B. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
71-13-00-410-040  Closing of the Fan Cowl Doors
 78-30-00-081-041  Make the Thrust Reverser Serviceable after
 Maintenance

 78-30-00-481-041  Make the Thrust Reverser Unserviceable for
 Maintenance
 78-36-00-410-040 Closing of the Thrust Reverser Doors
 54-57-17-991-001 Fig. 401

 3. Job Set-up
__________
 Subtask 54-57-17-860-050

 A. Aircraft Maintenance Configuration
 (1) Make sure that the access platform is in position. R (2) Make sure that the warning notice(s) is(are) in position.
 (3) Make sure that the thrust reversers are unserviceable (Ref. TASK 78-30-00-481-041).

 4.
 Procedure

_________

 5.
 Close-up

 

 Subtask 54-57-17-420-050
 A. Installation of the Fittings (Ref. Fig. 401/TASK 54-57-17-991-001)
 (1) Install the fitting (6).
 (a) Put the fitting (6) in position and install the nuts (10). 
R R  (b) Install the bolts (22), the washers (20) and the nuts (21) to attach the fitting (6) to the bracket (23). 
R  (c) Put the cowl stop assembly (5) in position. 
R  (d) Install the stirrup (2), the bolt (4), the washer (3) and the nut (1). 
R  (e) Install the bolt (9) and the nut (7) to connect the tube end (8) to the fitting (6). 
R  (f) Tighten the nuts (1) and (7). 
R  (g) TORQUE the nuts (10) to between 14 and 16 m.daN (103.24 and 117.99 lbf.ft).
 (2) Install the fitting (12).
 (a) Put the fitting (12) in position and install the nuts (11). 
 
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