E E May 01/05 E E ECES E
F 『
E C F M E
E E
E 56-5B E
E E
**ON A/C ALL
TASK 77-32-34-860-041
Change the configuration of the Accelerometer
1. Reason for the Job
__________________
Self Explanatory
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 31-32-00-860-012 Procedure to Get Access to the SYSTEM REPORT/TEST/ENG Page
R **ON A/C 001-049, 052-099, 101-149, 151-199, 201-299, 301-399, 401-499,
77-32-34-991-937 Fig. 504
**ON A/C 051-051,
77-32-34-991-937-A Fig. 504A
**ON A/C ALL
3. Job Set-up
__________
Subtask 77-32-34-861-064
A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
F 『 EEFF : ALL E Page 51177-32-34
E E Aug 01/05 E E ECES E
F 『
E C F M E
E E
E 56-5B E
E E
Subtask 77-32-34-865-073
B. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
121VU ENGINE/ENG1 AND 2/EVMU 1EV R44
Subtask 77-32-34-869-091
C. On the MCDU 1(2), get the SYSTEM REPORT/TEST ENG page (Ref. TASK 31-32-00-860-012).
4. Procedure
_________
Subtask 77-32-34-860-054
A. Change the Configuration of the Accelerometer
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. Push the line key adjacent to the The EVMU menu comes into view.
EVMU indication.
2. Push the line key adjacent to the The configuration of the left and right ACC RECONFIGURATION indication to engines comes into view. get the ACC RECONFIGURATION program.
R **ON A/C 001-049, 052-099, 101-149, 151-199, 201-299, 301-399, 401-499,
(Ref. Fig. 504/TASK 77-32-34-991-937)
**ON A/C 051-051,
(Ref. Fig. 504A/TASK 77-32-34-991-937-A)
**ON A/C ALL
Detail A.
F 『 EEFF : ALL E Page 51277-32-34
E E Aug 01/05 E E ECES E F 『 EEFF : ALL E Page 51377-32-34
F 『
E C F M E
E E
E 56-5B E
E E
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------3. Push the line key adjacent to the The indication for the new indication of the engine on which accelerometer comes into view under the you must change the indication of the related engine.
R **ON A/C 001-049, 052-099, 101-149, 151-199, 201-299, 301-399, 401-499,
(Ref. Fig. 504/TASK 77-32-34-991-937)
**ON A/C 051-051,
(Ref. Fig. 504A/TASK 77-32-34-991-937-A)
**ON A/C ALL
accelerometer. Detail B.
NOTE : The EVMU shows the state of the switching mode:____ - There is no accelerometer failure SWITCH MODE ON indication comes into view.
R **ON A/C 001-049, 052-099, 101-149, 151-199, 201-299, 301-399, 401-499,
(Ref. Fig. 504/TASK 77-32-34-991-937)
**ON A/C 051-051,
(Ref. Fig. 504A/TASK 77-32-34-991-937-A)
**ON A/C ALL
- If there is an accelerometer failure SWITCH MODE OFF/ ONE (MORE) ACCLM. DEFECT comes into view.
R **ON A/C 001-049, 052-099, 101-149, 151-199, 201-299, 301-399, 401-499,
(Ref. Fig. 504/TASK 77-32-34-991-937)
E E Aug 01/05 E E ECES E F 『 E C F M E E E
E 56-5B E
Reconfiguration of the Accelerometer Figure 504/TASK 77-32-34-991-937- 13 (SHEET 1)
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊 AMM ENGINE INDICATING 發(fā)動機(jī)指示(60)
