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时间:2011-02-24 09:55来源:蓝天飞行翻译 作者:admin
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 Subtask 21-61-52-010-051
 C. Get Access
 (1)
 Open the access panel/s (Ref. TASK 53-35-13-000-002).

 (a)
 For the Left ram-air outlet flap,

 -191KB.

 (b)
 For the Right ram-air outlet flap,


 -192KB.

 (2)
 Remove the ram-air outlet-flap actuator (1) (Ref. TASK 21-61-52-000-001).

 (a)
 For the Left ram-air outlet flap,

 -FOR 9HH

 (b)
 For the Right ram-air outlet flap,

 


R 1EFF : 001-003, 051-054, 1 21-61-52Page 411 1 1 May 01/05 1 1 1CES 1


 4. Procedure
_________
 (Ref. Fig. 402/TASK 21-61-52-991-002) Subtask 21-61-52-020-051
 A. Removal of the Ram-Air Outlet Flap
 (1)
 For the Left ram-air outlet flap:

 (a)
 Remove the nut (20), the washer (19) and the bolt (16).

 (b)
 Remove the nut (4), the washer (3) and the lever (2).

 (c)
 Remove the nut (14) and the washer (15).

 (d)
 Remove the screws (12) and the lining plate (13).

 (e)
 Hold the ram-air outlet flap (5) in the closed position and:

 (f)
 Remove the ram-air outlet flap (5).

 

 (2)
 For the Right ram-air outlet flap:

 (a)
 Remove the nut (20), the washer (19) and the bolt (16).

 (b)
 Remove the nut (4) and the washer (3).

 (c)
 Remove the nut (14) and the washer (15).

 (d)
 Remove the screws (12) and the lining plate (13).

 (e)
 Hold the ram-air outlet flap (5) in the closed position and: 1 Remove the screws (7) and the lining plate (6).

 


 1_ Remove the screws (7) and the lining plate (6).
 2_ Remove and discard the lockwire from the bolts (11) and (10).
 3_ Remove the bolt (11), the washer (18) and disconnect the
 bonding strap (17).
 4_ Remove the bolts (10).
 5_ Remove the shafts (8) and (9).

_
R 1EFF : 001-003, 051-054, 1 21-61-52Page 412 1 1 May 01/05 1 1 1CES 1


 Ram Air-Outlet Flap
 Figure 402/TASK 21-61-52-991-002

R 1EFF : 001-003, 051-054, 1 21-61-52Page 413 1 1 May 01/05 1 1 1CES 1 (f) Remove the ram-air outlet flap (5).


 2_ Remove and discard the lockwire from the bolts (11) and (10).
 3_ Remove the bolt (11), the washer (18) and disconnect the
 bonding strap (17).
 4_ Remove the bolts (10).
 5_ Remove the shafts (8) and (9) and the lever (2).

 (3) Do the inspection of the in-service wear limits for the applicable components (Ref. TASK 21-61-52-200-002).
 5. Close-up
________
R 1EFF : 001-003, 051-054, 1 21-61-52Page 414 1 1 May 01/05 1 1 1CES 1


 TASK 21-61-52-400-002
 Installation of the Ram-Air Outlet Flap
 WARNING : MAKE SURE THAT AIR IS NOT SUPPLIED TO THE AIR CONDITIONING SYSTEM_______ FROM THE MAIN ENGINE, THE APU OR A GROUND SOURCE. HOT COMPRESSED AIR CAN CAUSE INJURY TO PERSONNEL.
 1. Reason for the Job__________________
 Self Explanatory
 2. Job Set-up Information______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R R No specific  Torque Wrench : range 0.00 to 1.20 m.daN (0.00 to 9.00 lbf.ft) 
B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 19-010  USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00) 

R 1EFF : 001-003, 051-054, 1 21-61-52Page 415 1 1 May 01/05 1 1 1CES 1 C. Referenced Information


 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
20-28-00-912-004  Electrical Bonding of Components With Conductive
 Bolts and Screws and Bonding Straps in the Fuselage
 and in the Wings (this does not include the tanks)-
21-61-00-710-001  Operational Test of the Pack Temperature-Control
 System
 21-61-52-000-001  Removal of the Air-Outlet Flap Actuator 9HH (29HH)
 21-61-52-400-001  Installation of the Air-Outlet Flap Actuator 9HH
 (29HH)
 21-61-52-820-001  Adjustment of the Air Outlet Flap
 
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