(4)
Make sure that the access platform is in position below the applicable zone 575(675).
(5)
Make sure that the applicable access panels are removed:
-
FOR 33CE1, 33CE3
panels 575AT, 575KB, 590AB
-
FOR 33CE2, 33CE4
panels 675AT, 675KB, 690AB.
Subtask 27-14-51-865-051
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
4. Procedure
_________
**ON A/C 001-003, 051-052,
(Ref. Fig. 401/TASK 27-14-51-991-001)
R **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
(Ref. Fig. 401A/TASK 27-14-51-991-001-A) **ON A/C 001-003, 051-052,
(Ref. Fig. 402/TASK 27-14-51-991-002)
R **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
(Ref. Fig. 402A/TASK 27-14-51-991-002-A)
**ON A/C ALL
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.
**ON A/C 001-003, 051-052,
Subtask 27-14-51-420-059
A. Preparation for Installation
If the aileron servo control is safetied with STA-LOK nuts, do the steps that follow:
(1)
Clean the component interface and/or the adjacent area with a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026):
-
for 33CE1(33CE2), the pins (19) and (23)
-
for 33CE3(33CE4), the pins (18) and (22)
-
the flanged bushes (6) and (8)
-
the interfaces of the aileron and rear-spar jack-brackets.
(2)
Make sure that the parts retained from the removed component are clean and in the correct condition.
(3)
Do an inspection of the component interface and/or the adjacent area.
(4)
Make sure that the hydraulic line end-fittings are serviceable.
(5)
Lubricate these parts with SPECIAL MATERIALS (Material No. 05-002):
-
for 33CE1(33CE2), the pins (19) and (23)
-
for 33CE3(33CE4), the pins (18) and (22)
-
the flanged bushes (6) and (8)
-
the installed bushes in the outboard-flanges of the aileron and rear-spar jack-brackets.
If the aileron servo control is safetied with ABS 0738 nuts, do the steps that follow:
(6)
Clean the component interface and/or the adjacent area with a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026):
-
for 33CE1(33CE2), the pins (23) and (27)
-
for 33CE3(33CE4), the pins (22) and (26)
-
the flanged bushes (8) and (10)
-
the interfaces of the aileron and rear-spar jack-brackets.
(7)
Make sure that the parts retained from the removed component are clean and in the correct condition.
(8)
Do an inspection of the component interface and/or the adjacent area.
(9)
Make sure that the hydraulic line end-fittings are serviceable.
(10) Lubricate these parts with SPECIAL MATERIALS (Material No. 05-002):
-
for 33CE1(33CE2), the pins (23) and (27)
-
for 33CE3(33CE4), the pins (22) and (26)
-
the flanged bushes (8) and (10)
-
the installed bushes in the outboard-flanges of the aileron and rear-spar jack-brackets.
Subtask 27-14-51-420-050
B. Installation of the Aileron Servo Control (ASC)
If the aileron servo control is safetied with STA-LOK nuts, do the steps that follow:
(1)
Install the flanged bushes (6) and (8) into the inboard-flanges of the aileron and rear-spar jack-brackets.
(2)
Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to the eye-ends of the piston rods on the rounded sides only.
NOTE : Do not get Material 15-007 on the Servocontrol Spherical
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱1(110)
