Trailing-Edge Probe Filter - Component Location Figure 301/TASK 21-51-51-991-005 
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 (3) Filter Installation
 CAUTION : MAKE SURE THAT THE PROBE AND THE FILTER ARE CORRECTLY
_______ INSTALLED. INCORRECT INSTALLATION CAN CAUSE THE FILTER TO BECOME CLOGGED QUICKLY. A CLOGGED FILTER CAN CAUSE A PACK-OVERHEAT CONDITION. THIS CAN CAUSE DAMAGE TO THE AIR-CONDITIONING PACK.
 (a) Put the filter (3) together with the seal (2) in position in the flow control valve.
 NOTE : Make sure that the seal (2) is in the correct position and
____ is 'centered' under the filter (3).
 (b)
 TORQUE the filter (3) to between 0.90 and 1.10 m.daN (79.64 and
97.34 lbf.in).
 (c)
 Safety the filter (3) to the set-screw (1) with MISCELLANEOUS (Material No. 19-009).
 Subtask 21-51-51-865-059
 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 11HB 1HH, 2HH, 3HH, 4HH, 1HB. FOR 8HB 21HH, 22HH, 23HH, 24HH, 2HB.
 Subtask 21-51-51-710-051
 D. Test and Check
 (1)
 Do the operational test of the flow control and indicating system (Ref. TASK 21-51-00-710-002).
 (2)
 Leak Check
 WARNING : PUT ON PROTECTIVE GOGGLES AND THERMAL GLOVES WHEN YOU GO
_______ NEAR AN AIR-CONDITIONING PACK WHEN IT OPERATES. THERE CAN BE LEAKAGE OF HOT AIR, WHICH CAN CAUSE INJURIES.
 (a) During the operational test you must do a check for leaks at the filter installation. Leaks are not permitted.
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 5. Close-up
________ Subtask 21-51-51-410-056
 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.
 (2)
 Install the access panels (Ref. TASK 53-35-13-400-002):
 (a)
 FOR 11HB
 191KB and 191BB.
 (b)
 FOR 8HB
 192KB and 191BB.
 Subtask 21-51-51-942-052
 B. Remove the warning notice(s). Subtask 21-51-51-862-051
 C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
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 VALVE - PACK FLOW CONTROL (8HB,11HB,23HB,24HB) - REMOVAL/INSTALLATION
_____________________________________________________________________
R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
 TASK 21-51-51-000-001
 Removal of the Pack Flow-Control Valve
 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.
 NOTE : The procedure is the same for the pack flow-control valves 8HB and 11HB.
____
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific blanking caps
 No specific blanking plugs
 No specific circuit breaker(s) safety clip(s)
 B. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
21-51-41-000-001 Removal of the Ozone Filter (Converter) 100HM (101HM) 21-51-51-000-002 Removal of the Air Duct upstream of the Flow Control Valve 21-51-51-200-001 Attachment Components (In-Service Wear Limits) - Flow Control Valve (Unit) 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 53-35-13-000-002 Removal of the Quick-Release Access Panels from the Belly Fairing Structure
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REFERENCE DESIGNATION ------------------------------------------------------------------------------- 
 
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