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时间:2011-03-26 14:47来源:蓝天飞行翻译 作者:admin
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No specific  Torque Wrench : range 0.00 to 1.20 m.daN
 (0.00 to 9.00 lbf.ft)
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific  lint-free cloth
 Material No. 03-002  GB DEF-STAN 91-101 LUBRICATING OIL TURBINE ENGINE SYNT BASE (Ref. 20-31-00)
 Material No. 19-010  USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
 C. 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 from the External Power 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action 29-14-00-614-002 Pressurization of the Hydraulic Reservoirs through the Ground Connector


 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
49-00-00-710-008 Operational Test of the APU (APS 3200) 49-90-00-600-004 Check Oil Level and Replenish (APS 3200) 52-41-00-010-001 Open the APU Doors for Access 52-41-00-410-001 Close the APU Doors after Access 49-91-42-991-003 Fig. 201
 3. Job Set-up
__________
 Subtask 49-91-42-860-051
 A. Aircraft Maintenance Configuration
 (1)
 Make sure that the aircraft electrical circuits are energized (Ref. TASK 24-41-00-861-002).

 (2)
 On the panel 25VU, make sure that the APU MASTER SW pushbutton switch is off.

 (3)
 Make sure that there is a warning notice in the cockpit to tell persons not to start the APU.

 (4)
 Make sure that hydraulic systems are depressurized
 (Ref. TASK 29-00-00-864-001).


 (5)
 Make sure that the access platform is in position below the APU compartment.

 (6)
 Make sure that the APU access doors are open (Ref. TASK 52-41-00-010-001).

 (7)
 Make sure that the LIGHT control switch 11LJ is set to the on position.


 Subtask 49-91-42-865-060
 B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU APU/APU/CTL 2KD L42 121VU APU/ECB/SPLY 1KD L41


 4. Procedure
_________
 (Ref. Fig. 201/TASK 49-91-42-991-003) Subtask 49-91-42-420-053
 A. Installation of the Magnetic Drain Plug
 (1)
 Apply OILS (Material No. 03-002) to the new O-ring (4).

 (2)
 Install the new O-ring (4) on the plug (1).

 (3)
 Install the plug (1) into the gearbox.

 (4)
 TORQUE the plug (1) to between 0.57 and 0.73 m.daN (50.44 and 64.60 lbf.in).

 (5)
 Safety the plug (1) with MISCELLANEOUS (Material No. 19-010).

 (6)
 Apply OILS (Material No. 03-002) to the new preformed packing (2).

 (7)
 Install the new preformed packing (2) on the magnetic element (3).

 (8)
 Install the magnetic element (3) in the gearbox and hand-tighten it.

 (9)
 Make the area dry with a lint-free cloth to remove the unwanted oil from the gearbox surface.


 (10)
 Service the oil system (Ref. TASK 49-90-00-600-004). Subtask 49-91-42-865-061

 B.
 Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1KD, 2KD


 Subtask 49-91-42-790-051
 C. Leak Test
 (1) Do the operational test of the APU (Ref. TASK 49-00-00-710-008).
 (a) Make sure that the magnetic drain plug does not leak.


 5. Close-up
________ Subtask 49-91-42-410-054
 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Set the LIGHT control switch 11LJ to the off position.

 (3)
 Close the APU access doors 315AL, 316AR (Ref. TASK 52-41-00-410-001).


 (4)
 Remove the access platform(s). Subtask 49-91-42-860-052

 B.
 Aircraft Maintenance Configuration

 (1)
 Pressurize the reservoirs of the hydraulic systems.
 
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