A320飞机维护手册 AMM AIR CONDITIONING 空调 1(71)

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 36-11-49-000-042  Removal of the Pylon Interface Duct
 36-11-49-400-042  Installation of the Pylon Interface Duct
 49-00-00-860-003  APU Start by External Power (GTCP 36-300)
 49-00-00-860-004  APU Shutdown by External Power (GTCP 36-300)
 49-00-00-860-005  APU Start by External Power (APS 3200)
 49-00-00-860-006  APU Shutdown by External Power (APS 3200)
 49-00-00-860-008  APU Start by External Power (131-9(A))
 49-00-00-860-009  APU Shutdown by External Power (131-9(A))
 49-11-11-000-001  Removal of the Auxiliary Power Unit (APU) - 4005KM
 (GTCP 36-300)
 49-11-11-000-003  Removal of the Power Plant (APU) (APS 3200)
 49-11-11-000-004  Removal of the Power Plant (APU) (131-9(A))
 49-11-11-400-001  Installation of the Auxiliary Power Unit (APU) -
4005KM (GTCP 36-300)
 49-11-11-400-003  Installation of the Power Plant (APU) (APS 3200)
 49-11-11-400-004  Installation of the Power Plant (APU) (131-9(A))
 53-35-13-000-002  Removal of the Quick-Release Access Panels from the
 Belly Fairing Structure
 53-35-13-400-002  Installation of the Quick-Release Access Panels on
 the Belly Fairing Structure
 ACMM 211104
 CMM 214302
 CMM 214352
 CMM 215102

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 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
CMM 215110
 CMM 215202
 CMM 215204
 CMM 215234
 21-00-00-991-004 Fig. 201

 **ON A/C 001-049, 101-105, 151-199,
 21-00-00-991-001-A Fig. 202

R **ON A/C 051-099, 106-149, 201-299, 301-399,
 21-00-00-991-001 Fig. 202A

R **ON A/C 401-499,
 21-00-00-991-001-B Fig. 202B
 **ON A/C ALL
 21-00-00-991-002 Fig. 203
 3. Job Set-up
__________
 Subtask 21-00-00-941-051
 A. Necessary Special Tools
 (1)
 Special blanking caps - locally manufactured - see Job Set-up 2 off. These are to be locally manufactured, refer to (Ref. Fig. 201/TASK 21-00-00-991-004) and to SIL 21-029.

 (2)
 Temperature simulating devices - locally manufactured - see Job Set-up 3 off. These are to be locally manufactured, refer to schematic in (Ref. Fig. 203/TASK 21-00-00-991-002) and to SIL 21-029.

 

 Temperature Simulating Device - Schematic Figure 203/TASK 21-00-00-991-002
 1EFF : 1 1R 1CES  ALL  1 11 1 21-00-00 Page 238 Aug 01/05

 

 Subtask 21-00-00-861-051
 B. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002). Subtask 21-00-00-860-058
 C. Aircraft Maintenance Configuration
 (1)
 Do the EIS start procedure (Ref. TASK 31-60-00-860-001).

 (2)
 On the ECAM control panel push the COND pushbutton switch.

 (3)
 Make sure that at least one of the CKPT, the FWD cabin or the AFT cabin temperatures shown on the ECAM lower display unit (DU) is more than 24 deg. C.

 (4)
 If none of the temperatures is more than 24 deg. C you must do the alternative ECS decontamination procedure (Ref. TASK 21-00-00-615-001).

 Subtask 21-00-00-865-060
 D. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AIR BLEED/ENG 1/MONG 2HA1 D11 121VU APU/APU/CTL 2KD L42 121VU APU/ECB/SPLY 1KD L41 122VU AIR BLEED/ENG 2/MONG 2HA2 Z22
 Subtask 21-00-00-010-051
 E. Remove the access panels 191BB, 192FB, 191KB and 192KB (Ref. TASK 53-35-13-000-002).
 4. Procedure
_________ **ON A/C 001-049, 101-105, 151-199,
 (Ref. Fig. 202/TASK 21-00-00-991-001-A)
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R **ON A/C 051-099, 106-149, 201-299, 301-399,
 (Ref. Fig. 202A/TASK 21-00-00-991-001)

R **ON A/C 401-499,
 (Ref. Fig. 202B/TASK 21-00-00-991-001-B)
 **ON A/C ALL
 Subtask 21-00-00-869-061
 A. Cleaning of the APU Bleed Air Duct forward of the Load Control Valve
 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)
 Put a warning notice in position in the cockpit to tell persons not to start the APU or the engines.
　
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