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时间:2011-02-24 09:37来源:蓝天飞行翻译 作者:admin
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 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
21-26-43-600-011 Servicing of the Filter Cartridge (2082HM) 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 52-41-00-410-002 Close the Avionics Compartment Doors after Access CMM 212600 21-26-42-991-007 Fig. 606
 3. Job Set-up
__________ Subtask 21-26-42-010-059
 A. Get Access
 (1)
 Put the access platform in position at the access door 824.

 (2)
 Open the access door 824.


R 1EFF : 002-049, 051-099, 101-105, 1 21-26-42Page 637 1 1 May 01/05 1 1 1CES 1 Subtask 21-26-42-861-057


 B. Energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-861-002).

 NOTE : The energization of the aircraft electrical circuits starts the
____ full test of the ventilation system. The test continues for 2 minutes approximately. Do not connect the manometer until this test is completed.
 Subtask 21-26-42-860-053
 C. Aircraft Maintenance Configuration
 (1)
 Remove the protective caps from the pressure ports. The pressure ports of the filter cartridge are black.

 (2)
 Connect the MANOMETER (EMA84) to the pressure ports.


 4. Procedure
_________ (Ref. Fig. 606/TASK 21-26-42-991-007) Subtask 21-26-42-210-061
 A. Check for Blockage of the Filter Cartridge
 (1) If the differential pressure is more than 16.5 mbar (0.23 psi):
 (a) Clean the filter (Ref. CMM 212600) or replace it by a new one (Ref. TASK 21-26-43-600-011).
 5. Close-up
________ Subtask 21-26-42-862-057
 A. De-energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-862-002).

 Subtask 21-26-42-860-054
 B. Put the aircraft back to its initial configuration.
 (1)
 Disconnect the MANOMETER (EMA84) from the pressure ports.

 (2)
 Install the protective caps on the pressure ports.


R 1EFF : 002-049, 051-099, 101-105, 1 21-26-42Page 638 1 1 May 01/05 1 1 1CES 1


 Check for Blockage of the Filter Cartridge with Pressure Ports
 Figure 606/TASK 21-26-42-991-007

R 1EFF : 002-049, 051-099, 101-105, 1 21-26-42Page 639 1 1 May 01/05 1 1 1CES 1 Subtask 21-26-42-410-058


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

 (2)
 Close the access door 824 (Ref. TASK 52-41-00-410-002).

 (3)
 Remove the access platform(s).


R 1EFF : 002-049, 051-099, 101-105, 1 21-26-42Page 640 1 1 May 01/05 1 1 1CES 1R **ON A/C 301-399, 401-499,

 

 TASK 21-26-42-200-006
 Check for Blockage of the Demister Filter with the Pressure Ports

 1.
 Reason for the Job

__________________
 Self Explanatory


 2.
 Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific manometer 0 to 0.3447 bar (0 to 5 psi)
 No specific access platform 1.60 m (5 ft. 3 in.)

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
21-26-43-600-016 Discard Demister Filter 21-26-43-600-017 Discard Filter Cartridge 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 52-41-00-410-002 Close the Avionics Compartment Doors after Access 21-26-42-991-012 Fig. 607
 3. Job Set-up
__________
 Subtask 21-26-42-010-062

 A. Get Access
 (1)
 Put the access platform in position at the access door 824.

 (2)
 Open the access door 824.


R 1EFF : 301-399, 401-499, 1 21-26-42Page 641 1 1 Aug 01/05 1 1 1CES 1 Subtask 21-26-42-861-059


 B. Energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-861-002).

 NOTE : The energization of the aircraft electrical circuits starts the
____ full test of the ventilation system. The test continues for 2 minutes approximately. Do not connect the manometer until this test is completed.
 
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