Component Location
Figure 003
F 『R EEFF : 001-049, 051-099, 101-105, 151-199, E Page 574-00-00
E E201-299, 301-302, May 01/05 E E ECES E F 『 E C F M E E E E 56-5B E
Component Location
Figure 003A
F 『R EEFF : 106-149, 303-399, 401-499, E Page 674-00-00
E E Aug 01/05 E E ECES E F 『 E C F M E E E E 56-5B E
Ignition Starting - ECAM Display
Figure 004
F 『 EEFF : 001-049, 051-099, 101-105, 151-199, E Page 774-00-00
E E201-299, 301-302, May 01/05 E E ECES E F 『 E C F M E E E E 56-5B E
Ignition Starting - ECAM Display
Figure 004A
F 『R EEFF : 106-149, 303-399, 401-499, E Page 874-00-00
E E Aug 01/05 E E ECES E
F 『
E C F M E
E E
E 56-5B E
E E
IGNITION - GENERAL - ADJUSTMENT/TEST
____________________________________
TASK 74-00-00-710-043
Operational Test of the Ignition System
1. Reason for the Job
__________________
To do an aural check of the igniter plug operation.
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
74-00-00-991-300 Fig. 501
74-00-00-991-301-A Fig. 502
3. Job Set-up
__________
Subtask 74-00-00-861-050
A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
Subtask 74-00-00-865-050
B. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
49VU ENGINE/1 AND 2/IGN/SYS A 1JH A03 FOR 1000EM1
49VU ENGINE/1/FADEC A/AND EIU 1 2KS1 A04 121VU ENGINE/IGN/ENG1/SYS B 3JH1 P41 121VU ENGINE/IGN/ENG1/SYS A BAT 2JH1 P39 121VU ENGINE/ENG1/FADEC B/AND EIU 1 4KS1 R41
FOR 1000EM2 49VU ENGINE/2/FADEC A/AND EIU 2 2KS2 A05 121VU ENGINE/IGN/ENG2/SYS B 3JH2 P42
F 『 EEFF : ALL E Page 50174-00-00
E E Aug 01/01 E
RE ECES E
F 『
E C F M E
E E
E 56-5B E
E E
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU ENGINE/IGN/ENG2/SYS A BAT 2JH2 P40 121VU ENGINE/ENG2/FADEC B 4KS2 Q40
Subtask 74-00-00-860-050
C. Aircraft Maintenance Configuration
(1) On the MAINTENANCE PNL 50VU :
(a) Release the ENG/FADEC GND PWR/1 (2) pushbutton switch. The ON legend of this pushbutton switch is on.
(2) On the left or right MCDU, get the SYSTEM REPORT/TEST ENG menu page (Ref. Fig. 501/TASK 74-00-00-991-300)
4. Procedure
_________ R **ON A/C 001-049, 051-099, 101-149, 155-199, 201-299, 301-399, 401-499,
Subtask 74-00-00-710-050
A. Do this test : WARNING : MAKE SURE THERE IS NO AIR PRESSURE SUPPLIED AT THE STARTER
_______
VALVE INLET.
NOTE : This test is for the system 1. For the other system(s), use the
____
indications between the parentheses.
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the MCDU:
- Push the line key adjacent to - The ENGINE 1(2) MAIN MENU page comes
the FADEC 1A (2A) indication. into view. (Ref. Fig. 502/TASK 74-00-00-991-301-A)
2. Push the line key adjacent to the - The IGNITION TEST menu comes into IGN TEST indication. view.
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 IGNITION 点火(4)
