(2)
Close the access door 314AR.
(3)
Remove the access platform(s).
1EFF : ALL 1 26-22-00Page 529 1 1 May 01/05R 1 1 1CES 1
Subtask 26-22-00-860-055
B. Put the aircraft back to its initial configuration.
(1)
Remove the 600 ohms headset from the CAPT jack panel.
(2)
De-energize the audio integrating system (Ref. TASK 23-51-00-710-001).
(3)
De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002).
Subtask 26-22-00-865-063
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1KD, 2KD.
1EFF : ALL 1 26-22-00Page 530 1 1 May 01/05R 1 1 1CES 1
TASK 26-22-00-710-004
Operational Test of APU Fire-Exting. P/BSW funct. (single chan. config) and APU LP Fuel-Valve using each indiv. motor in turn and APU Emerg. Shutdown Circuit
WARNING : THE ACCIDENTAL FIRING OF THE EXTINGUISHER BOTTLE CAN CAUSE SERIOUS
_______ INJURY TO PERSONS WHO WORK OR ARE IN THE CLOSE PROXIMITY.
WARNING : BE CAREFUL WHEN YOU PUSH THE "APU/MSTR" P/BSW TO ON. THE IGNITION BOX
_______ WILL BECOME ENERGIZED FOR APPROXIMATELY 3 SECONDS. THIS CAN CAUSE INJURY OR KILL PERSONS.
1.
Reason for the Job
__________________
Refer to the MPD TASK: 262200-06
2.
Job Set-up Information
______________________
A. 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 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure
3. Job Set-up
__________ Subtask 26-22-00-860-056
A. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002).
(2)
Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. TASK 31-60-00-860-001).
1EFF : ALL 1 26-22-00Page 531 1 1 May 01/05R 1 1 1CES 1
Subtask 26-22-00-865-064
B. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU APU/FIRE AND OVHT/DET/LOOP B 2WG L44 121VU APU/FIRE AND OVHT/DET/LOOP A 1WG L43 121VU APU/APU/CTL 2KD L42 121VU APU/ECB/SPLY 1KD L41 121VU APU/AUTO/EXTIG/GND/TEST 30WF L40 121VU APU/FIRE/EXTIG/SQUIB/B 2WF L39 121VU APU/FIRE/EXTIG/SQUIB/A 1WF L38 121VU APU/FIRE/LP VALVE/NORM 4WF M42 121VU APU/FIRE/LP VALVE/STBY 3WF M41 121VU APU/FUEL/LP VALVE/CTL 1QF M40 121VU APU/FUEL/LP VALVE/SPLY 2QF M39
4. Procedure
_________
R **ON A/C 001-049, 063-099, 101-149, 151-199, 201-299, 301-399, 401-499,
Subtask 26-22-00-710-057-B
A. Test of the Fire Emergency-Stop Relays 5WF and 6WF.
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. In the INT LT section of the In the cockpit: overhead panel 25VU: - all annunciator lights come on fully
-put the ANN LT switch in the bright.
TEST position.
2. In the INT LT section of the In the cockpit: overhead panel 25VU: - all applicable annunciator lights go
-put the ANN LT switch in the off.
BRT position.
3. On the circuit breaker panel 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址:A320飞机维护手册 AMM FIRE PROTECTION 防火2(70)