3. Job Set-up
__________
**ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
Subtask 27-92-16-010-050
A. Get Access
(1)
Put the access platform in position at the access door 825.
(2)
Open the access door 825.
(3)
Remove the sidewall panel :
FOR 12CE1, 12CE3
131MW
FOR 12CE2, 12CE4
132MW
(4)
Put the access platform in position at the access door 822.
(5)
Open the access door 822
(6)
At the battery power center 105VU:
-loosen the two screws and remove the protective cover. R **ON A/C 151-199, 401-499,
Subtask 27-92-16-010-050-A
A. Get Access
(1)
Put the access platform in position at the access door 825.
(2)
Open the access door 825.
(3)
Remove the sidewall panel :
FOR 12CE1, 12CE3
131GW
FOR 12CE2, 12CE4
132KW
(4)
Put the access platform in position at the access door 822.
(5)
Open the access door 822
(6)
At the battery power center 105VU:
-loosen the two screws and remove the protective cover.
**ON A/C ALL
Subtask 27-92-16-865-050
B. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------FOR 12CE1
49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 FOR 12CE2 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 105VU FLT CTL/SEC1/STBY SPLY 22CE B01
FOR 12CE3 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
FOR 12CE4 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18
4. Procedure
_________
**ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
(Ref. Fig. 401/TASK 27-92-16-991-001)
R **ON A/C 151-199, 401-499,
(Ref. Fig. 401A/TASK 27-92-16-991-001-A)
Flight Control Accelerometer
Figure 401/TASK 27-92-16-991-001
R 1EFF : 001-049, 051-099, 101-149, 201-299, 1 27-92-16Page 404 1301-399, 1May 01/05 1 1 1CES 1
Flight Control Accelerometer
Figure 401A/TASK 27-92-16-991-001-A
R 1EFF : 151-199, 401-499, 1 27-92-16Page 405 1 1 Aug 01/05 1 1 1CES 1R **ON A/C ALL
Subtask 27-92-16-020-050
A. Removal of the Flight Control Accelerometer
(1)
Disconnect the electrical connector (3) from the accelerometer (1).
(2)
Put blanking caps on the electrical connectors (3) and (6).
(3)
Remove the screws (5) and the washers (4).
(4)
Remove the accelerometer (1).
TASK 27-92-16-400-001
Installation of the Flight Control Accelerometer (12CE1,12CE2,12CE3,12CE4)
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific access platform 1.6 m (5 ft. 3 in.)
B. 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 31-21-00-750-002 Procedure to set the Clock
**ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
27-92-16-991-001 Fig. 401 R **ON A/C 151-199, 401-499,
27-92-16-991-001-A Fig. 401A **ON A/C ALL
3. Job Set-up
__________
**ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
Subtask 27-92-16-860-051
A. Aircraft Maintenance Configuration
(1)
Make sure that the access platform is in position at the access door
825. 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 FLIGHT CONTROLS 飞行操纵9(25)
