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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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R R R R  -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------2000VU CAB COM SYSTEM - PRAM 2RX 07 F 
R  **ON A/C 052-055, 057-057, 401-499,
 Subtask 35-23-00-861-053 
R  C. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002). 

R EFF : 052-055, 057-057, 401-499, 35-23-00Page 402 Aug 01/05
 CES


R  **ON A/C 052-055, 057-057,
 Subtask 35-23-00-010-058 
R  D. Get Access
 (1) On all the emergency oxygen containers push the left hand side of the
 test lever on the door, until the over-center spring keeps the lever
 at 90 degrees to the door surface.
 NOTE : The test lever should stay in this position until manually____
 set. 
R  **ON A/C 401-499, 
R  Subtask 35-23-00-010-058-A 
R  D. Get Access 
R  (1) On all the emergency oxygen containers pull out the door stops with 
R  your fingers and turn them 90 degrees to the TEST position. 
R  Subtask 35-23-00-860-056 
R  E. Aircraft Maintenance Configuration 
R  (Ref. Fig. 401/TASK 35-23-00-991-006) 
R  (1) Remove the altitude pressure switch 16WR (Ref. TASK 35-23-15-000-
R  001), to do this do the steps that follow: 
R  (a) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position below 
R  the access door 824 and open it. 
R  (b) Remove the screws (4), the washers (5) and remove the altitude 
R  switch (2) from its support (3). 
R  NOTE : Do not disconnect the electrical connector (1) from the____ 
R  altitude switch (2). 

R EFF : 052-055, 057-057, 401-499, 35-23-00Page 403 Aug 01/05
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 Altitude Pressure Switch 16WR Figure 401/TASK 35-23-00-991-006 
R  EFF :  052-055, 057-057, 401-499,  35-23-00 Page 404 Aug 01/05
 CES 

 

R  **ON A/C 052-055, 057-057, 401-499,
 Subtask 35-23-00-480-053 
R R  F. Connect the altitude pressure switch 16WR to a vacuum source with the HOSE - ADAPTER, ALTITUDE SWITCH (98A35207599000). **ON A/C 401-499, 
R  Subtask 35-23-00-860-053 
R R R R  G. Preparation for the test (1) Make sure that the AHS ON pushbutton switch 899WR on the overhead panel 21VU is in the normal position. **ON A/C 052-055, 057-057, 401-499,
 4. Procedure_________
 Subtask 35-23-00-040-050
 A. Do the functional test of the automatic mask release.
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------

1. At the vacuum source:
-slowly increase the pressure to 14800 ft. (4500 m).
2. At the vacuum source:
 -slowly decrease the pressure to 0 ft. (0 m).
On the panel 21VU:
-
the SYS ON indicator light comes onat 14000 +0 -500 ft. (4260 +0 -150 m).

 On all the emergency oxygen containers:

 -
the doors open to the maximum permitted by the door stops.


R EFF : 052-055, 057-057, 401-499, 35-23-00Page 405 Aug 01/05
 CES


 -------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
3. On the panel 50VU:
-push and hold the TMR RESET pushbutton switch.
-release the TMR RESET
pushbutton switch.

4. In the cabin at the first and second seatrow:
 -close the doors of all related emergency oxygen containers.
 5. On the overhead panel 21VU:
-push the AHS ON pushbutton switch.
6. At the vacuum source:
-slowly increase the pressure to 16800 ft. (5120 m).
7. At the vacuum source:
 -slowly decrease the pressure to 0 ft. (0 m).
 8. On the panel 50VU: On the panel 50VU:
-
the ON indicator light on the TMRRESET pushbutton switch comes on.

 On the panel 21VU:

 -
the SYS ON indicator light goes off. On the panel 50VU:

-
the ON indicator light on the TMRRESET pushbutton switch goes off.


On the overhead panel 21VU:
-
the On legend in the AHS ONpushbutton switch comes on.

On the panel 21VU:

-
the SYS ON indicator light comes onat 16000 +0 -500 ft. (4870 +0 -150 m).

 On all the emergency oxygen containers at the first and second seatrow:

 -
 
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