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时间:2011-02-24 09:55来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

_______ IS PRESSURIZED. A PRESSURE-SEALED DOOR THAT OPENS WHEN THE AIRCRAFT IS PRESSURIZED.
 -WILL CAUSE EXPLOSIVE DECOMPRESSION.
 -CAN KILL OR CAUSE INJURY TO PERSONS AND/OR CAUSE DAMAGE TO THE AIRCRAFT/EQUIPMENT.
 (1)
 Open the FWD cargo-compartment door 825 (Ref. TASK 52-30-00-860-001).

 (2)
 Put the access platform at the FWD cargo-compartment door 825.


 (3) Remove the access panel 131PW (Ref. TASK 25-54-12-000-001).
 Subtask 21-63-00-865-055

 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------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,
 122VU AIR COND/ZONE TEMP CTL/28VDC/SYS2 4HK V20 122VU AIR COND/ZONE TEMP CTL/28VDC/SYS1 3HK V19 122VU AIR COND/ZONE TEMP CTL/115VAC/SYS2 2HK V18 122VU AIR COND/ZONE TEMP CTL/115VAC/SYS1 1HK V17


R  -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------**ON A/C 401-499,
R R  122VU AIR COND/TEMP CTL SYS 2/CHAN A/115VAC 122VU AIR COND/TEMP CTL SYS 2/CHAN A/28VDC 122VU AIR COND/TEMP CTL SYS 1/CHAN A/115VAC 122VU AIR COND/TEMP CTL SYS 1/CHAN A/28VDC 122VU AIR COND/TEMP CTL SYS 2/CHAN B/28VDC 122VU AIR COND/TEMP CTL SYS 2/CHAN B/115VAC 122VU AIR COND/TEMP CTL SYS 1/CHAN B/115VAC  53HH 55HH 49HH 51HH 56HH 54HH 50HH  W22W21X22X21 Y21Y20Y18 
**ON A/C ALL
 4. Procedure_________
 Subtask 21-63-00-440-051
 A. Reactivation of the Pressure Regulating Valve
 (1) Remove the lockwire from the manual override lever (3) of the hot-air pressure-regulating valve (2).
 (2) Remove the temporary attachment from the disconnected electrical connector 14HK-C (1).
 (3) Make sure that the electrical connectors are clean and in the correct condition.
 (4) Connect the electrical connector 14HK-C (1) to the hot-air pressure-regulating valve (2). 
R  **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
 Subtask 21-63-00-865-068
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1HK, 2HK, 3HK, 4HK.

 


R **ON A/C 401-499,
 Subtask 21-63-00-865-068-A
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 49HH, 50HH, 51HH, 52HH, 53HH, 54HH, 55HH, 56HH.
 **ON A/C ALL
 Subtask 21-63-00-810-051
 C. Do the trouble shooting of the hot-air pressure-regulating valve 14HK (Ref. TSM ATA 21) and do the applicable corrective maintenance procedure(s).
 5. Close-up
________
 Subtask 21-63-00-410-055

 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Install the access panel 131PW (Ref. TASK 25-54-12-400-001).

 (3)
 Remove the access platform(s).

 (4)
 Close the FWD cargo-compartment door 825 (Ref. TASK 52-30-00-860-002).


 Subtask 21-63-00-862-058
 B. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).

 

R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
 TASK 21-63-00-040-004
 Deactivation of the Zone Controller - Hot-Air Pressure-Regulating Valve Check
 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. Reason for the Job
__________________
 Refer to the MMEL TASK: 21-63-01 c)
 Cockpit and Cabin Temperature Control
 Zone Controller

 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific blanking caps
 No specific access platform 2 m (6 ft. 7 in.)
 B. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
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
 
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