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时间:2011-03-26 09:15来源:蓝天飞行翻译 作者:admin
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1. On the AIR COND overhead control panel 30VU:
 -make sure that the X-BLEED selector switch is in the AUTO position.
 2.
 On the circuit breaker panel 122VU: - open the AIR BLEED/X FEED

 VALVE/NORM circuit breaker 1HV.

 3.
 On the AIR COND overhead control panel 30VU:


-push the APU BLEED pushbutton switch.
On the AIR COND overhead control panel30VU:
-the blue ON legend of the APU BLEEDpushbutton switch comes on.
 The APU supplies bleed air after 5 s.
 A single chime is heard after approximately 20 s.
 On the LH (131VU) and RH (130VU) glareshield:
 -the MASTER CAUT lights come on after approximately 20 s.
 On the upper ECAM display unit:
 -AIR X BLEED FAULT (amber).
 -X BLEED ..... MAN CTL (cyan).
 -AVOID ICING CONDITIONS (cyan). comes into view.
 1EFF : ALL 1 36-12-00Page 504 1 1 May 01/05R 1 1 1CES 1


 -------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
On the BLEED page of the lower ECAM display unit: - the APU bleed valve symbol is in line (green). - the crossbleed valve symbol is in crossline (amber).
 4. On the circuit breaker panel 122VU: - close the AIR BLEED/X FEED VALVE/NORM circuit breaker 1HV.  On the LH (131VU) and RH (130VU)glareshield:- the MASTER CAUT lights go off afterapproximately 20 s.
 The crossbleed valve opens after approximately 5 s.
 On the upper ECAM display unit: - AIR X BLEED FAULT (amber). - X BLEED ..... MAN CTL (cyan). - AVOID ICING CONDITIONS (cyan). goes off.
 On the lower ECAM display unit: - the BLEED page goes off.
 5. On the ECAM control panel (ECP) 11VU: On the ECAM control panel (ECP) 11VU:
 - push the BLEED pushbutton switch.  - the light in the BLEED pushbuttonswitch comes on (white).
 On the BLEED page the lower ECAM display unit: - the APU bleed valve symbol in line (green). - the crossbleed valve symbol in line (green).
 6. On the AIR COND overhead control panel 30VU:  On the AIR COND overhead control panel30VU:
 - push the APU BLEED pushbutton switch.  - the blue ON legend of the APU BLEEDpushbutton switch goes off.

 1EFF : ALL 1 36-12-00Page 505 1 1 May 01/05R 1 1 1CES 1


 -------------------------------------------------------------------------------
ACTION  RESULT
 -------------------------------------------------------------------------------The APU bleed valve and the crossbleed valve close.
 On the BLEED page of the lower ECAM display unit:
 -
the APU bleed valve symbol in crossline (green).

 -
the crossbleed valve symbol turns from line to crossline (amber).


 -after approximately 5 s the crossbleed valve symbol in crossline (green).
 7. On the ECAM control panel (ECP)  On the ECAM control panel (ECP) 11VU: 11VU:
 -push the BLEED pushbutton  - the light in the BLEED pushbutton switch. switch goes off.
 On the lower ECAM display unit:
 -the BLEED page goes off.
 (1) Reset of the Message on the Status Page
 NOTE : During the test the message X-BLEED MAN CTL comes into view on
____ the STS page. Reset the FWC 1 and FWC 2 or do the subsequent procedure.
 (a)
 Pull the circuit breaker AIR/BLEED/X FEED/VALVE/BAT (2HV).

 (b)
 Put the X-BLEED selector switch in the OPEN position (with the crossbleed valve in closed postion) and keep it there until the message X-BLEED MAN CTL goes out of view.

 (c)
 Close the circuit breaker AIR/BLEED/X FEED/VALVE BAT/(2HV).


 1EFF : ALL 1 36-12-00Page 506 1 1 May 01/05R 1 1 1CES 1


 5. Close-up
________
 **ON A/C 001-049, 101-105, 151-199, 201-210,

 Subtask 36-12-00-860-050-A
 A. Put the aircraft back to the serviceable condition.
 (1)
 Shut down the APU (Ref. TASK 49-00-00-860-009).

 (2)
 Do the EIS stop procedure
 (Ref. TASK 31-60-00-860-002).


 (3)
 De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).


 **ON A/C 051-099,
 Subtask 36-12-00-860-050
 A. Put the aircraft back to the serviceable condition.
 (1)
 Shut down the APU (Ref. TASK 49-00-00-860-004).

 (2)
 Do the EIS stop procedure
 (Ref. TASK 31-60-00-860-002).


 (3)
 De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).

 

R **ON A/C 106-149, 211-299, 301-399, 401-499,
 
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