(2)
Make sure that the access door 825 is open.
(3)
Make sure that the sidewall panel is removed:
FOR 12CE1, 12CE3
131MW
FOR 12CE2, 12CE4
132MW
(4)
Make sure that the access platform is in position at the access door
825.
(5)
Make sure that the access door 822 is open.
(6)
On the battery power center 105VU:
-make sure that the protective cover is removed. R **ON A/C 151-199, 401-499,
Subtask 27-92-16-860-051-A
A. Aircraft Maintenance Configuration
(1)
Make sure that the access platform is in position at the access door
825.
(2)
Make sure that the access door 825 is open.
(3)
Make sure that the sidewall panel is removed:
FOR 12CE1, 12CE3
131GW
FOR 12CE2, 12CE4
132KW
(4)
Make sure that the access platform is in position at the access door
825.
(5)
Make sure that the access door 822 is open.
(6)
On the battery power center 105VU:
-make sure that the protective cover is removed.
**ON A/C ALL
Subtask 27-92-16-865-051
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------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
_________
R **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)
**ON A/C ALL
Subtask 27-92-16-860-050
A. Aircraft Maintenance Configuration
(1) Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Do an inspection of the component interface and/or the adjacent area. Subtask 27-92-16-420-051
B. Installation of the Flight Control Accelerometer
(1)
Install the accelerometer (1) on its mount (2).
(2)
Install the washers (4), the screws (5) and tighten them.
(3)
Remove the blanking cap from the electrical connector (3).
(4)
Connect the electrical connector (3) to the accelerometer (1).
Subtask 27-92-16-861-050
C.
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002). Subtask 27-92-16-865-052
D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 12CE1 15CE1, 16CE1 FOR 12CE2 21CE1, 22CE FOR 12CE3 15CE2, 16CE2 FOR 12CE4 21CE2 Subtask 27-92-16-865-053
E. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
49VU FLIGHT CONTROLS/SLT FLP/POS/IND 1 1CN B12
49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11
49VU FLIGHT CONTROLS/FCDC1/SPLY 20CE1 B10
49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09
49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08
49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07
49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06
49VU AUTO FLT/FAC1/28VDC 5CC1 B04
49VU AUTO FLT/FAC1/26VAC 14CC1 B03
105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02
105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01
105VU FLT CTL/SEC1/STBY SPLY 22CE B01
105VU ELEC/HOT BUS/702PP SPLY 5PB2 D02
105VU ELEC/HOT BUS/701PP SPLY 5PB1 D01
105VU ELEC/HOT BUS/702PP SPLY 12PB2 E02
105VU ELEC/HOT BUS/701PP SPLY 12PB1 E01
121VU PTR/SPLY 6TW J21
121VU CFDS/TEST PLUG/2 10TW J20
121VU CFDS/TEST PLUG/1 9TW J19
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱9(26)
