R 1EFF : 401-499, 1 21-51-00Page 513 1 1 Aug 01/05 1 1 1CES 1
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R R R R ACTION RESULT -------------------------------------------------------------------------------After approx. 20 seconds: - the left pack flow indicator moves to the NORM position (between the 11 o'clock and the 1 o'clock position).
R R R R After approx. 35 seconds: - the right pack flow indicator moves to the NORM position (between the 11 o'clock and the 1 o'clock position).
**ON A/C ALL
5. Close-up________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
Subtask 21-51-00-865-056
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1HK
**ON A/C ALL
Subtask 21-51-00-860-052
B. Aircraft Maintenance Configuration
(1) Preconditioning
(a) Do the Procedure to Stop the APU or, - (Ref. TASK 49-00-00-860-004) or, - (Ref. TASK 49-00-00-860-006) or, - (Ref. TASK 49-00-00-860-009).
(b) Stop the preconditiong through the HP connector (Ref. TASK 12-33-21-618-001).
(2) Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).
R 1EFF : ALL 1 21-51-00Page 514 1 1 Aug 01/05 1 1 1CES 1
(3)
Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
(4)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
1EFF : ALL 1 21-51-00Page 515 1 1 Aug 01/05R 1 1 1CES 1
TASK 21-51-00-710-003 Operational Test of the Flow Control Valves Closing WARNING : MAKE SURE THAT THE FWD AVIONICS ACCESS DOOR 811 IS OPEN. WITH A
_______ WARNING PLACARD ATTACHED TO IT. THE WARNING NOTICE MUST TELL PERSONS NOT TO CLOSE THE DOOR. THIS PREVENTS ACCIDENTAL PRESSURIZATION OF THE AIRCRAFT.
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-33-21-618-001 Pre-conditioning through the HP Ground Connection 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure
3. Job Set-up
__________ Subtask 21-51-00-861-053
A. Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002).
1EFF : ALL 1 21-51-00Page 516 1 1 Aug 01/05R 1 1 1CES 1
Subtask 21-51-00-865-053
B. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
R **ON A/C 401-499,
49VU AIR COND/TEMP CTL/SYS 1 CHAN B/28VDC 52HH D08
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
R 122VU AIR COND/ZONE TEMP CTL/28VDC/SYS2 122VU AIR COND/ZONE TEMP CTL/28VDC/SYS1 122VU AIR COND/ZONE TEMP CTL/115VAC/SYS2 122VU AIR COND/ZONE TEMP CTL/115VAC/SYS1 122VU AIR COND/PACK TEMP/CTL SYS1/2/115VAC 122VU AIR COND/PACK TEMP/CTL SYS1/2/28VDC 122VU AIR COND/PACK TEMP/CTL SYS1/1/115VAC 122VU AIR COND/PACK TEMP/CTL SYS1/1/28VDC 122VU AIR COND/PACK TEMP CTL SYS2/2/28VDC 122VU AIR COND/PACK TEMP CTL SYS2/2/115VAC 4HK 3HK 2HK 1HK 21HH 23HH 1HH 3HH 24HH 22HH V20V19V18V17W22W21X22X21Y21Y20
R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
R 122VU AIR COND/PACK TEMP CTL SYS2/1/28VDC 4HH Y19
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
R 122VU AIR COND/PACK TEMP CTL SYS2/1/115VAC 2HH Y18
R **ON A/C 106-149, 303-399,
R 122VU 4HH Y19
R **ON A/C 401-499,
R 122VU AIR COND/TEMP CTL SYS 2/CHAN A/115VAC 53HH W22
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R R R R R R PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------122VU AIR COND/TEMP CTL SYS 2/CHAN A/28VDC 55HH W21 122VU AIR COND/TEMP CTL SYS 1/CHAN A/115VAC 49HH X22 122VU AIR COND/TEMP CTL SYS 1/CHAN A/28VDC 51HH X21 122VU AIR COND/TEMP CTL SYS 2/CHAN B/28VDC 56HH Y21 122VU AIR COND/TEMP CTL SYS 2/CHAN B/115VAC 54HH Y20 122VU AIR COND/TEMP CTL SYS 1/CHAN B/115VAC 50HH Y18
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本文鏈接地址：A320飛機維護手冊 AMM AIR CONDITIONING 空調 3(107)
