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R  (Ref. CMM 212600). 
R  Subtask 21-26-43-210-080 
R  D. Do an inspection of the component interface and/or the adjacent area. 
R  NOTE : Make sure that the plate (2) is in the correct position.____ 
R  Subtask 21-26-43-420-081 
R  E. Installation of the Demister Filter 
R  (1) Engage the tabs of the cover (3) into the recesses of the filter 
R  element (1). Apply pressure to assemble the two components. 
R  (2) Engage the filter element (1) in the body. 
R  (3) Lock the handle of the cover (3) into the body. 
R  5. Close-up________ 
R  Subtask 21-26-43-410-088 
R  A. Close Access 
R  (1) Make sure that the work area is clean and clear of tool(s) and other 
R  items. 
R  (2) Close the access door 824 (Ref. TASK 52-41-00-410-002). 
R  (3) Remove the access platform(s). 
R  Subtask 21-26-43-865-118 
R  B. Remove the safety clip(s) and the tag(s) and close this(these) circuit 
R  breaker(s): 
R  1HQ, 2HQ, 3HQ, 5HQ, 6HQ

 

R Subtask 21-26-43-861-115
R C. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
R Subtask 21-26-43-862-110
R D. De-energize the ground service network (Ref. TASK 24-42-00-862-001).

 

R TASK 21-26-43-600-019 R Servicing of the Filter Cartridge (2082HM) R 1. Reason for the Job
__________________ R Self Explanatory R 2. Job Set-up Information
______________________
R A. Fixtures, Tools, Test and Support Equipment
R -------------------------------------------------------------------------------R REFERENCE QTY DESIGNATION R -------------------------------------------------------------------------------
R No specific circuit breaker(s) safety clip(s) R No specific access platform 1.6 m (5 ft. 3 in.)
R B. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R 24-41-00-861-002 R R 24-41-00-862-002 R R 24-42-00-861-001 R R 24-42-00-862-001 R R 52-41-00-410-002 R CMM 212600 R 21-26-43-991-031
R 3. Job Set-up
__________
R Subtask 21-26-43-862-111 Energize the Aircraft Electrical Circuits from the External Power De-energize the Aircraft Electrical Circuits Supplied from the External Power Energize the Ground Service Network from the External Power De-energize the Ground Service Network Supplied from the External Power Close the Avionics Compartment Doors after Access
Fig. 304
R A. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-R 002).
R Subtask 21-26-43-861-116
R B. Energize the ground service network (Ref. TASK 24-42-00-861-001).

 

R  Subtask 21-26-43-865-119 
R  C. Open, safety and tag this(these) circuit breaker(s): 
R  -------------------------------------------------------------------------------
R  PANEL  DESIGNATION  IDENT. LOCATION 
R  -------------------------------------------------------------------------------
R  49VU AIR COND/AVNCS VENT/CTL  6HQ  D06 
R  49VU AIR COND/AVNCS VENT/CTL  5HQ  D05 
R  122VU AIR COND/AVNCS/VENT/MONG  3HQ  Y17 
R  123VU AVNCS VENT/BLOWER/FAN  1HQ  AD10 
R  123VU AVNCS VENT/EXTC/FAN  2HQ  AE02 
R  Subtask 21-26-43-010-094 
R  D. Get Access 
R  (1) Put the access platform in position at the access door 824. 
R  (2) Open the access door 824. 
R  4. Procedure_________ 
R  (Ref. Fig. 304/TASK 21-26-43-991-031) 
R  Subtask 21-26-43-020-081 
R  A. Removal of the Filter Cartridge 
R  (1) Release each of the four fasteners: 
R  (a) Move the lock (14) to the door of the body (10). 
R  (b) Lift the fasteners. 
R  (2) Push the door and lift the fasteners to fully release the door of the 
R  body (10). 
R  (3) Open the door of the body (10). 
R  (4) Hold the two ends of the ring (12) with the loop bowden cable. 
R  (5) Pull the filter (13) with the straps to disengage the bearing from 
R  its housing. 
R  (6) Remove the filter (13) from the body (10).

 

R Filter Cartridge R Figure 304/TASK 21-26-43-991-031
 1EFF : 001-049, 101-105, 1 21-26-43Page 318 1 1 Config-2 Aug 01/05 1 1 1CES 1
　
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