A320飞机维护手册 AMM AIR CONDITIONING 空调 5(36)

 (5)
 Remove the packing (5) from the pack-outlet pneumatic sensor (4).

 (6)
 Put blanking plugs on the disconnected line ends.

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 Pack Outlet Pneumatic-Sensor
 Figure 401/TASK 21-61-19-991-001

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 TASK 21-61-19-400-002 Installation of the Pack-Outlet Pneumatic Sensor 10HM10 (11HM10) WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______ YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
 NOTE : The procedure is the same for the pack-outlet pneumatic sensors 10HM10
____ and 11HB10.
 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
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. 04-012  USA VV-P-236 PURE MINERALVASELINE OR PETRO- LATUM (Ref. 20-31-00)
 Material No. 19-009  USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.5MM DIA (Ref. 20-31-00)
 C. Expendable Parts
 -------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
5 packing 21-52-03 26 -100 5 packing 21-52-03 26 -100A 5 packing 21-52-03 26A-100
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 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-33-21-618-001 Pre-conditioning through the HP Ground Connection 12-33-21-618-001 Pre-conditioning with the APU 21-61-00-710-001 Operational Test of the Pack Temperature-Control
 System 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 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 21-61-19-991-001 Fig. 401
 3. Job Set-up
__________
 Subtask 21-61-19-860-050-A
 A. Aircraft Maintenance Configuration
 (1)
 Make sure that the aircraft electrical ciruits are energized (Ref. TASK 24-41-00-861-002).

 (2)
 Make sure that the access panel is removed (Ref. TASK 53-35-13-000-002).

R (a) FOR 10HM10 191BB.
R (b) FOR 11HM10 192FB.
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 Subtask 21-61-19-865-051
 B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
R  -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------FOR 10HM10 49VU AIR COND/FLOW/CTL &/IND1 1HB D07 122VU AIR COND/PACK TEMP/CTL SYS1/1/115VAC 1HH X22 122VU AIR COND/PACK TEMP/CTL SYS1/1/28VDC 3HH X21 
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 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
 FOR 11HM10 122VU AIR COND/FLOW/CTL AND IND/2 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  2HB 21HH 23HH 24HH 22HH  V21W22W21Y21Y20 

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