(5)
Remove the sense lines assembly from the aircraft.
(6)
Put blanking plugs on the disconnected line ends.
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 21-61-41Page 430 1201-299, 301-399, 1Aug 01/05 1 1 1CES 1R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
TASK 21-61-41-400-002
Installation of the Anti-Ice Valve Sense-Lines Assembly
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
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No specific Torque Wrench : range 0.00 to 1.20 m.daN
(0.00 to 9.00 lbf.ft)
B. Consumable Materials
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REFERENCE DESIGNATION
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Material No. 04-014A USA MIL-PRF-907
HIGH TEMPERATURECOMPOUND (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
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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
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
53-35-13-400-002 Installation of the Quick-Release Access Panels on the Belly Fairing Structure
**ON A/C 001-049, 051-099, 101-105, 151-158, 201-210,
21-61-41-991-002 Fig. 402
R **ON A/C 106-149, 159-199, 211-299,
21-61-41-991-002-A Fig. 402A
R **ON A/C 301-399,
21-61-41-991-002-B Fig. 402B
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
3. Job Set-up__________
Subtask 21-61-41-860-052-A
A. Aircraft Maintenance Configuration
(1) Make sure that the aircraft electrical circuits are energized (Ref. TASK 24-41-00-861-002).
(2) Make sure that the access panel(s) are removed (Ref. TASK 53-35-13-000-002).
R (a) FOR 10HM - 191KB and - 191BB.
R (b) FOR 11HM - 192KB and - 192FB.
Subtask 21-61-41-865-055
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
R -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------FOR 10HM 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 11HM 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
4. Procedure_________
**ON A/C 001-049, 051-099, 101-105, 151-158, 201-210,
(Ref. Fig. 402/TASK 21-61-41-991-002)
R **ON A/C 106-149, 159-199, 211-299,
(Ref. Fig. 402A/TASK 21-61-41-991-002-A) R **ON A/C 301-399,
(Ref. Fig. 402B/TASK 21-61-41-991-002-B)
**ON A/C 001-049, 051-099, 101-105, 151-158, 201-210,
Subtask 21-61-41-420-051
A. Installation of the Sense Lines Assembly
(1)
Remove the blanking plugs from the disconnected line ends.
(2) 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址:A320飞机维护手册 AMM AIR CONDITIONING 空调 5(48)