(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
 -------------------------------------------------------------------------------
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. 04-014A  USA MIL-PRF-907
 HIGH TEMPERATURECOMPOUND (Ref. 20-31-00)
 C. Referenced Information
 -------------------------------------------------------------------------------
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
 -------------------------------------------------------------------------------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)