A320飞机维护手册 AMM FUEL 燃油2(46)

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 21-51-51-000-001  Removal of the Pack Flow-Control Valve
 21-51-51-000-002  Removal of the Air Duct upstream of the Flow Control
 Valve
 21-51-51-400-001  Installation of the Pack Flow-Control Valve
 21-51-51-400-002  Installation of the Air Duct upstream of the Flow
 Control Valve
 21-52-41-000-001  Removal of the Air Conditioning Pack 10HM (11HM)
 21-52-41-400-001  Installation of the Air Conditioning Pack 10HM (11HM)
 24-41-00-862-002  De-energize the Aircraft Electrical Circuits Supplied
 from the External Power
 28-13-00-700-001  Functional Check (Pressure and Free Flow) of Vapor
 Seal and Vent/Drain System
 28-13-42-000-001  Removal of the Vapor Seal
 28-13-42-300-001  Center Tank Vapor Seal Membrane Repair
 36-12-41-000-001  Removal of a Bleed-Air Duct
 36-12-41-400-001  Installation of a Bleed-Air Duct
 36-22-18-000-001  Removal of the Fuselage Overheat Sensing-Elements
 (Loop A and B)
 36-22-18-400-001  Installation of the Fuselage Overheat
 Sensing-Elements (Loop A and B)
 28-13-42-991-004  Fig. 401
 28-13-42-991-006  Fig. 402
 **ON A/C 001-002,
 28-13-42-991-001  Fig. 403 

R **ON A/C 003-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 28-13-42-991-001-A Fig. 403A
 **ON A/C 001-002,
 28-13-42-991-002 Fig. 404

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REFERENCE DESIGNATION
 -------------------------------------------------------------------------------

R **ON A/C 003-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 28-13-42-991-002-A Fig. 404A
 **ON A/C 001-002,
 28-13-42-991-003 Fig. 405 R **ON A/C 003-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 28-13-42-991-003-A Fig. 405A
 **ON A/C ALL
 3. Job Set-up
__________
 **ON A/C 001-049, 101-105, 151-199,

 Subtask 28-13-42-860-051-A
 A. Aircraft Maintenance Configuration (Ref. Fig. 401/TASK 28-13-42-991-004, 402/TASK 28-13-42-991-006)
 (1)
 Make sure that the aircraft electrical circuits are de-energized (Ref. TASK 24-41-00-862-002).

 (2)
 Make sure that the air conditioning packs 10HM (11HM) are removed (Ref. TASK 21-52-41-000-001).

 (3)
 Make sure that the pack flow-control valves 8HB (11HB) are removed (Ref. TASK 21-51-51-000-001).

 (4)
 Make sure that the ozone filter 100HM (101HM) is removed (Ref. TASK 21-51-41-000-001).

 (5)
 Make sure that the hot trim-air ducts (100) are removed.

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 (6)
 Make sure that the overheat detection loops A and B are removed from the heat shields and the APU bleed-air ducts (Ref. TASK 36-22-18-000-001).

 (7)
 Make sure that the APU bleed-air ducts (123) and (124) are removed (Ref. TASK 36-12-41-000-001).

 (8)
 Make sure that the electrical harness at the air conditioning pack compartment in Zone 191/192 are removed.

 

R **ON A/C 051-099, 106-149, 201-299, 301-399, 401-499,
 Subtask 28-13-42-860-051
 A. Aircraft Maintenance Configuration (Ref. Fig. 401/TASK 28-13-42-991-004, 402/TASK 28-13-42-991-006)
 (1)
 Make sure that the aircraft electrical circuits are de-energized (Ref. TASK 24-41-00-862-002).

 (2)
 Make sure that the air conditioning packs 10HM (11HM) are removed (Ref. TASK 21-52-41-000-001).

 (3)
 Make sure that the pack flow-control valves 8HB (11HB) are removed (Ref. TASK 21-51-51-000-001).

 (4)
 Make sure that the air ducts upstream of the flow-control valves 8HB (11HB) are removed (Ref. TASK 21-51-51-000-002).

 (5)
 Make sure that the hot trim-air ducts (100) are removed.

 (6)
 Make sure that the overheat detection loops A and B are removed from the heat shields and the APU bleed-air ducts (Ref. TASK 36-22-18-000-001).

 (7)
 Make sure that the APU bleed-air ducts (123) and (124) are removed (Ref. TASK 36-12-41-000-001).

 (8)
 Make sure that the electrical harness at the air conditioning pack compartment in Zone 191/192 are removed.

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 4. Procedure
_________
 **ON A/C 001-002,
　
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