-
FOR 31CE7
disconnect the unions (30) and (31)
-
FOR 31CE8
disconnect the unions (32) and (33)
-
FOR 31CE9 disconnect the unions (34), (36), (37), (38) and (40)
-
FOR 31CE10 disconnect the unions (41), (42), (43), (45), (46) and (47).
(3)
Remove all the drops of hydraulic fluid from the adjacent aircraft
structure.
(4)
Remove the applicable hydraulic pipes:
-
FOR 31CE1, 31CE2
remove the pipe (3)
-
FOR 31CE3
remove the pipes (22) and (26)
-
FOR 31CE4
remove the pipes (6) and (9)
-
FOR 31CE5
remove the pipe (19)
-
FOR 31CE6
remove the pipe (14)
-
FOR 31CE9
remove the pipe (35) and the connector (39)
-
FOR 31CE10
remove the pipe (44) and (49) and the connector (48).
(5)
Put blanking plugs on the disconnected line ends.
(6)
Disconnect the electrical connector (73).
(7)
Put blanking caps on the disconnected electrical connectors.
(8)
Install the correct spoiler support strut:
-
for spoiler 1, install STRUT SUPPORT - SPOILER 1 (98D27604002000)
-
for spoilers 2 thru 5, install STRUT SUPPORT - SPOILER 2, 3, 4, AND 5 (98D27604001000).
(9)
Remove and discard the cotter pin (70) from the locking cap (69).
(10)
Remove the locking cap (69), the nut (68) and the washer (67).
(11)
Remove the special bolt (65) and the sliding bush (66) from the spoiler attachment bracket.
(12)
Remove the bolts (61) and the washers (60).
(13)
Remove all the drops of hydraulic fluid from the adjacent aircraft structure.
(14)
Move the servo control approximately 6 mm (0.2362 in.) away from the structure to disengage the location dowels.
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(15)
Move the servo-control away from the applicable hydraulic line connector:
-
FOR 31CE1, 31CE2
the connector (1)
-
FOR 31CE5
the connector (21)
-
FOR 31CE6
the connector (12)
-
FOR 31CE7
the connectors (30) and (31)
-
FOR 31CE8
the connectors (32) and (33).
(16)
Remove the spoiler servo-control.
(17)
Remove the flanged bush (64).
(18)
Remove the COLLAR-SAFETY, SPOILER from the piston rod of the spoiler servo-control.
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TASK 27-64-51-400-004
Installation of the Spoiler Servo-Control 31CE1 thru 31CE10
WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______ NOTICES ARE IN POSITION.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
_______
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
-MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers No specific warning notice No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft) No specific Torque Wrench : range 1.00 to 10.00 m.daN
(8.00 to 75.00 lbf.ft) SL90-313-7500 1 TOOL - INSTALLATION, TAB WASHERS STA-LOK NSA5454 SL90-315-7500 1 WRENCHES - NOTCHED, TIGHTENING OF NUTS NSA5454 98D27603002000 1 SPOILER MAINTENANCE KEY 98D27603002001 1 SPOILER MAINTENANCE KEY 98D27604000000 1 COLLAR-SAFETY, SPOILER
1EFF : ALL 1 27-64-51Page 418 1 1 May 01/05R 1 1 1CES 1
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本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵7(19)
