B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-92-15-991-001 Fig. 401
3. Job Set-up
__________
(Ref. Fig. 401/TASK 27-92-15-991-001) Subtask 27-92-15-860-050
A. Aircraft Maintenance Configuration
(1)
Put a warning notice to tell persons not to operate the pedals.
(2)
On the panel 110VU, put a warning notice to tell persons not to use the rudder trim.
(3)
Put the access platform in position at the access door 811.
(4)
Open the access door 811.
(5)
Put the access platform in position at the access door 822.
(6)
Open the access door 822.
(7)
On the battery power center 105VU:
-loosen the two screws and remove the protective cover.
(8)
Put the PIN, RIGGING - RUDDER CONTROL (98A27901002000) (19) in position on the yaw and braking bellcranks.
Pedal Position Transducer Unit
Figure 401/TASK 27-92-15-991-001
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Subtask 27-92-15-865-050
B. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 R 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 R 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 R
121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
4. Procedure
_________
(Ref. Fig. 401/TASK 27-92-15-991-001)
Subtask 27-92-15-020-050
A. Removal of the Transducer Unit
(1)
Disconnect the electrical connectors (13) and (14) from the transducer unit (12).
(2)
Put blanking caps on the electrical connectors (13) and (14) and on the electrical connectors of the transducer unit (12).
(3)
Remove and discard the cotter pin (8) remove the nut (7) and the washer (6).
(4)
Remove the bolt (2) and disconnect the rod (5).
(5)
Remove and discard the cotter pins (16) remove the nuts (15) and the washers (17).
(6) Remove the bolts (1) and remove the transducer unit (12).
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TASK 27-92-15-400-001
Installation of the Pedal Position Transducer Unit (25CE1,25CE2)
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific warning notice
No specific access platform 1.5 m (4 ft. 11 in.)
No specific access platform 1.6 m (5 ft. 3 in.)
98A27901002000 2 PIN, RIGGING - RUDDER CONTROL
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
No specific Lockwire corrosion resistant steel dia 0.8 mm (0.03 in.)
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
8 cotter pin 27-21-01 01 -010 R 8 cotter pin 27-21-01 01A-010 16 cotter pin 27-92-01 01 -010
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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(22)
