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时间:2011-03-26 09:06来源:蓝天飞行翻译 作者:admin
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24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 24-42-00-861-001 Energize the Ground Service Network from the External Power 24-42-00-862-001 De-energize the Ground Service Network Supplied from the External Power 35-12-41-400-002 Installation of the Full-Face/Quick-donning Oxygen-Mask 35-12-41-991-001 Fig. 401
 3. Job Set-up
__________
 Subtask 35-12-41-860-055
 A. Aircraft Maintenance Configuration
R (1) Make sure that the ACCESS PLATFORM 2M (6 FT) is in position at the access door 812.
 (2)
 Open the access door 812.

 (3)
 Make sure that the ground service network is energized (Ref. TASK 24-42-00-861-001).


R (4) Make sure that the WARNING NOTICE which tells persons not to open the valve of the oxygen cylinder assembly is in position.
 (5) Make sure that the parts retained from the removed component are clean and in the correct condition.
 Subtask 35-12-41-865-053
 B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU OXYGEN/CREW/OXY/SPLY 1HT HA01
 EFF : ALL

35-12-41Page 406


 4. Procedure
_________
 (Ref. Fig. 401/TASK 35-12-41-991-001) Subtask 35-12-41-420-056
 A. Installation of the Oxygen-Mask Stowage-Box (10RN1, 10RN2, 10RN3, 5774HM) NOTE : Only use SPECIAL MATERIALS (Material No. 05-003B) on the threads
____ of the nut or on the flared part of the tube. Apply only a thin layer of the compound on the first three threads that are male.
 (1)
 Install the stowage box of the oxygen mask in its housing.

 (2)
 Lock the latches (2).

 (3)
 Remove the sealed vinyl bag from the end of the line (5).

 (4)
 Remove the blanking plugs from the line (5) and the union (3).

 (5)
 Install a new seal (4) on the union of the line (5).

 (6)
 Install the line (5) on the union (3) and tighten it. NOTE : Counter-torque the union (3) when you tighten the line (5) so

____ that you do not damage the stowage box (1).

 (7)
 Remove the blanking caps from the electrical connector (6) and the fixed connector (7). It is not necessary to do this operation for the stowage box assembly of the 4th Occupant.

 (8)
 Connect the electrical connector (6) to the fixed connector (7). It is not necessary to do this operation for the stowage box assembly of the 4th Occupant.

 (9)
 If it is necessary, install the full-face/quick-donning oxygen-mask (Ref. TASK 35-12-41-400-002)


 Subtask 35-12-41-790-050
 B. Leak test
 (1)
 Apply a layer of SPECIAL MATERIALS (Material No. 05-004) to the mechanical connection.

 (2)
 Open the valve of the oxygen cylinder very slowly.


 EFF : ALL

35-12-41Page 407


 (3)
 Let the pressure become stable for approximately 90 seconds.

 (4)
 Fully open the valve of the oxygen cylinder.

 (5)
 Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1HT

 (6)
 On the panel 21VU:

 -push the OXYGEN/CREW SUPPLY pushbutton switch. The OFF legend goes off.

 (7)
 Make sure that there are no leaks on the connection.

 (8)
 Remove the SPECIAL MATERIALS (Material No. 05-004).

 (9)
 On the panel 21VU:


 -release the OXYGEN/CREW SUPPLY pushbutton switch. The OFF legend comes on.
 (10)
 De-energize the aircraft electrical circuits. (Ref. TASK 24-41-00-862-002)

 (11)
 Install the lining panel.


 5. Close-up
________ Subtask 35-12-41-860-056
 A. Put the aircraft back to its initial configuration.
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Remove the warning notice(s).

 (3)
 De-energize the ground service network
 (Ref. TASK 24-42-00-862-001)

 

 Subtask 35-12-41-410-051
 B. Close Access
 (1)
 Close the access door 812.

 (2)
 Remove the access platform(s).


 EFF : ALL

35-12-41Page 408


 TASK 35-12-41-000-002 Removal of the Full-Face/Quick-Donning Oxygen-Mask WARNING : KEEP ALL HYDROCARBONS (FUELS, LUBRICANTS, ETC.) AWAY FROM ALL SOURCE
 
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