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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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R  **ON A/C 401-499,
R  49VU AIR COND/TEMP CTL/SYS 1 CHAN B/28VDC **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399, 52HH  D08 
R  122VU AIR COND/PACK TEMP/CTL SYS1/1/115VAC 122VU AIR COND/PACK TEMP/CTL SYS1/1/28VDC  1HH 3HH  X22X21 
R  **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302, 
R R  122VU AIR COND/PACK TEMP CTL SYS2/1/28VDC **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,  4HH  Y19 
R R  122VU AIR COND/PACK TEMP CTL SYS2/1/115VAC **ON A/C 106-149, 303-399,  2HH  Y18 
R  122VU  4HH  Y19 
R  **ON A/C 401-499, 
R R  122VU AIR COND/TEMP CTL SYS 1/CHAN A/115VAC 122VU AIR COND/TEMP CTL SYS 1/CHAN A/28VDC  49HH 51HH  X22 X21

 

 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------122VU AIR COND/TEMP CTL SYS 1/CHAN B/115VAC 50HH Y18
 **ON A/C ALL
 FOR 28HH 
R  **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
 122VU AIR COND/PACK TEMP/CTL SYS1/2/115VAC 122VU AIR COND/PACK TEMP/CTL SYS1/2/28VDC 122VU AIR COND/PACK TEMP CTL SYS2/2/28VDC 122VU AIR COND/PACK TEMP CTL SYS2/2/115VAC  21HH 23HH 24HH 22HH  W22W21Y21Y20 
R  **ON A/C 401-499,
R R  122VU AIR COND/TEMP CTL SYS 2/CHAN A/115VAC 122VU AIR COND/TEMP CTL SYS 2/CHAN A/28VDC 122VU AIR COND/TEMP CTL SYS 2/CHAN B/28VDC 122VU AIR COND/TEMP CTL SYS 2/CHAN B/115VAC  53HH 55HH 56HH 54HH  W22W21 Y21Y20 
**ON A/C ALL
 Subtask 21-61-51-941-054
 C. Safety Precautions
 (1) On the panel 30VU:
 (a) Make sure that the APU BLEED and the ENG BLEED/1(2) pushbutton switches are released.
 (b) Put a warning notice in position to tell persons not to operate these pushbutton switches.
 (2) On the HP ground connector put a warning notice in position to tell persons not to supply the ground air.

 

 4. Procedure
_________ (Ref. Fig. 601/TASK 21-61-51-991-009) Subtask 21-61-51-220-050
 A. Measurement of the Air-Inlet Flap Backlash and Air-Inlet Flap Gap
 (1) At the centre line of the air inlet flap (1) and the diffuser nose (2):
 (a)
 Measure and note the dimension "A".

 (b)
 Measure and note the dimension "B". NOTE : The measurement for the dimension "B" must be made with


____ the load applied (hand pressure). Do not apply excessive hand pressure as this could result in a false measurement.
 (2)
 Subtract dimension "A" from dimension "B". This will give you the backlash which exists in the air-inlet flap system.

 (3)
 If the backlash is more than 3mm (0.118 in) you must do a check of the in-service wear limits of the air-inlet flap mechanism (Ref. TASK 21-61-51-000-003) and (Ref. TASK 21-61-51-200-003).

 (a)
 If necessary replace the affected parts (Ref. TASK 21-61-51-400-003) and (Ref. TASK 21-61-00-300-001).

 (b)
 Do a check of the air-inlet flap gap and adjust if necessary (Ref. TASK 21-61-51-820-001).

 

 (4)
 Make sure that the work area is clean and clear of tool(s) and other items.


 5. Close-up
________ Subtask 21-61-51-865-063
 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
 (1)
 FOR 8HH

 -1HH, 2HH, 3HH, 4HH, 49HH, 50HH, 51HH, 52HH.

 (2)
 FOR 28HH


 -21HH, 22HH, 23HH, 24HH, 53HH, 54HH, 55HH, 56HH.
 1EFF : ALL 1 21-61-51Page 604 1 1 Aug 01/05R 1 1 1CES 1


 Inspection Measurement Location Figure 601/TASK 21-61-51-991-009
 1EFF : 1 1R 1CES  ALL  1 11 1 21-61-51 Page 605 Aug 01/05

 

 Subtask 21-61-51-410-055
 B. Remove the warning notice(s). Subtask 21-61-51-862-054
 C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
 1EFF : ALL 1 21-61-51Page 606 1 1 Aug 01/05R 1 1 1CES 1


 TASK 21-61-51-200-002 Inspection of the Air Inlet Flap Backlash 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.
 NOTE : The procedure is the same for the left and the right air inlet flap.
____
 1. Reason for the Job
__________________
 This procedure is optional. It is to assist in early detection of possible excessive wear in the ram-air inlet flap offset mechanism system.
 
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