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时间:2011-03-24 08:55来源:蓝天飞行翻译 作者:admin
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 (d) Attach the foil wrap with lockwire 0.032 in. (0.80 mm) dia. (Material No. CP8004) at the two sides of the pneumatic joint. 
R  Subtask 30-21-51-860-058 
R  D. Put the aircraft back to its initial configuration. 
R R  (1) Make sure that the work area is clean and clear of tool(s) and other items. 
R  Subtask 30-21-51-861-060 
R R  E. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).

 

 Foil Wrap Installation at Pneumatic System Joints Figure 403/TASK 30-21-51-991-302
 1EFF : 1 1R 1CES  ALL  1 11 1 30-21-51 Page 411 Aug 01/05

 

 Subtask 30-21-51-865-054

R  F. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------122VU ANTI ICE/ENG/2 1DN2 W10 122VU ANTI ICE/ENG/1 1DN1 X10 
R  Subtask 30-21-51-410-064 
R  G. Close Access 
R R R R R  (1) Close the fan cowl doors (Ref. TASK 71-13-00-410-040): FOR 1000EM1 437AL, 438AR FOR 1000EM2 447AL, 448AR. 
R  Subtask 30-21-51-860-059 
R  H. Do the EIS start procedure (SD DU only) (Ref. TASK 31-60-00-860-001).
 Subtask 30-21-51-869-051 
R  J. On the ANTI ICE overhead control & indicating panel 25VU, make sure that the ENG1 (2) pushbutton switch is released.
 Subtask 30-21-51-710-050 
R  K. Test 
R R R  (1) Start the related engine with the automatic or manual start procedure (Ref. TASK 71-00-00-710-003) or (Ref. TASK 71-00-00-710-004) and keep it at idle.

 

R (2) Do this test:

 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the ANTI ICE overhead control  On the ANTI ICE overhead control &
 & indicating panel 25VU:  indicating panel 25VU: 
R  - push the ENG1 (2) pushbutton  - the ON legend of the ENG1 (2) 
R  switch  pushbutton switch comes on 
R  - the FAULT legend of the ENG1 (2) 
R  pushbutton switch comes on. 
R  - after 5 minutes, release the  - the ON and FAULT legends of the ENG1 
R  ENG1 (2) pushbutton switch  (2) pushbutton switch go off. 

R  (3) Stop the engine (Ref. TASK 71-00-00-710-028). 
R  Subtask 30-21-51-865-072 
R  L. Open, safety and tag this(these) circuit breaker(s): 
R  -------------------------------------------------------------------------------
R  PANEL  DESIGNATION  IDENT. LOCATION 
R  -------------------------------------------------------------------------------
R  122VU ANTI ICE/ENG/2  1DN2  W10 
R  122VU ANTI ICE/ENG/1  1DN1  X10 
R  Subtask 30-21-51-010-066 
R  M. Open the fan cowl doors (Ref. TASK 71-13-00-010-040): 
R  FOR 1000EM1 
R  437AL, 438AR 
R  FOR 1000EM2 
R  447AL, 448AR 
R  Subtask 30-21-51-210-060 
R  N. Visual Inspection 
R  (1) Make sure that there are no leaks at the anti-ice valve of the 
R  related engine air intake. 
R  (2) Remove the materials used to do the leak test.


 5. Close-up
________

R  Subtask 30-21-51-860-060 
R  A. Do the EIS stop procedure (Ref. TASK 31-60-00-860-002) 
R  Subtask 30-21-51-865-073 
R R  B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 
R R R R R  -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------122VU ANTI ICE/ENG/2 1DN2 W10 122VU ANTI ICE/ENG/1 1DN1 X10
 Subtask 30-21-51-410-051 
R  C. Close Access
 (1) Make sure that the work area is clean and clear of tool(s) and other items.
 (2) Close the fan cowl doors (Ref. TASK 71-13-00-410-040): FOR 1000EM1 437AL, 438AR FOR 1000EM2 447AL, 448AR
 (3) Remove the warning notice(s). 
R  Subtask 30-21-51-862-057 
R  D. De-energize Electrical Circuits 
R R  (1) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002). 
R R  (2) De-energize the ground service network (Ref. TASK 24-42-00-862-001).
 
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