R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
27-51-44-991-003 Fig. 403
**ON A/C 301-399,
27-51-44-991-003-A Fig. 403A
**ON A/C ALL
3. Job Set-up
__________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 403/TASK 27-51-44-991-003)R **ON A/C 301-399,
R (Ref. Fig. 403A/TASK 27-51-44-991-003-A) R **ON A/C ALL
Subtask 27-51-44-941-062
A. Safety Precautions
(1)
Make sure that the safety barriers are in position.
(2)
Make sure that the warning notice is in position to tell persons not to operate the flap/slat controls.
Subtask 27-51-44-860-061
B. Aircraft Maintenance Configuration
(1)
Make sure that the lower kink seal, the cushion seals and the upper kink seals are removed from the flaps (Ref. TASK 27-54-61-000-002).
(2)
Make sure that the flaps are extended at position 1 (Ref. TASK 27-50-00-866-009).
(3)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) (Ref. TASK 27-00-00-480-002) is on the flap/slat control lever.
(4)
Make sure that the access platform is in position:
-for the left wing, below zone 580
-for the right wing, below zone 680.
Subtask 27-51-44-865-071
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
4. Procedure
_________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 403/TASK 27-51-44-991-003)
**ON A/C 301-399,
(Ref. Fig. 403A/TASK 27-51-44-991-003-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.
Subtask 27-51-44-420-058
A. Preparation for Installation
(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).
(2)
Do an inspection of the component interface and/or the adjacent area.
(3)
Make sure that the parts retained from the removed component are clean and in the correct condition.
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 27-51-44-420-052
B. Installation of the Proximity Sensor
(1)
Put the applicable proximity sensor (1) in position on the bracket (3): FOR 37CV, 38CV
(a) Install the bolts (5), the washers (4) and the nuts (2). Do not tighten the nuts (2).
(2)
Put the applicable proximity sensor (14) in position on the bracket (8): FOR 39CV, 40CV
(a) Install the bolts (6), the washers (7) and the nuts (9). Do not tighten the nuts (9).
(3)
Install the PIN-SETTING (98D27504031000) in the interconnecting strut (15).
(4)
Make sure that the dimension X is between 0.3 mm (0.02 in.) and 0.7 mm (0.03 in.).
(5)
Tighten the applicable nuts (2) or (9).
(6)
Make sure that the dimension X has stayed correct.
(7)
Remove the blanking cap from the electrical applicable connector (10) or (13).
(8)
Connect the applicable electrical connector (11) or (12).
(9)
Remove the PIN-SETTING from the interconnecting strut (15).
(10) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) from the slat/flap control lever.
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-51-44Page 434 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
R **ON A/C 301-399,
R Subtask 27-51-44-420-052-A
R B. Installation of the Proximity Sensor
R (1) Put the applicable proximity sensor (1) in position on the bracket
R (3):
R FOR 37CV, 38CV
R (a) Install the bolts (5), the washers (4) and the nuts (2). Do not
R tighten the nuts (2).
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4(113)
