(2)
Make sure that the warning notice is in position to tell persons not to operate the flight controls.
Subtask 27-54-49-860-057
B. Aircraft Maintenance Configuration
R (1) Make sure that the flaps are fully extended (Ref. TASK 27-50-00-866-008).
(2)
Make sure the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is on the flap/slat control lever in the cockpit.
(3)
Make sure that the No. 2 and the No. 3 spoilers have been extended (Ref. TASK 27-60-00-866-002).
(4)
Make sure that there is a COLLAR-SAFETY, SPOILER on the piston rod of each servo-control.
(5) Make sure that the trailing edge of the flap is on supports. R (6) Make sure that the clamp holds the carriage in position.
(7)
Make sure that the access platform is below the applicable access panel.
(8)
Make sure that the applicable access panels are removed:
-
for the left wing, panels 573BB, 575AB, 575BB, 575CB, 575DB
-
for the right wing, panels 673BB, 675AB, 675BB, 675CB, 675DB.
(9)
Make sure that the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT are installed on the applicable torque shafts.
R 1EFF : ALL 1 27-54-49Page 491 1 1 May 01/04 1 1 1CES 1
(10) Make sure that the applicable torque shafts and the universal joint are removed.
Subtask 27-54-49-865-062
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
_________
**ON A/C 001-049, 051-061, 101-105, 201-203,
(Ref. Fig. 405/TASK 27-54-49-991-003)
R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
(Ref. Fig. 405A/TASK 27-54-49-991-003-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.
R **ON A/C 001-049, 051-061, 101-105, 201-203,
Subtask 27-54-49-560-051
A. Preparation for a Replacement Component
(1) Replacement actuator assemblies of flap track 3 are supplied in the Left Hand (LH) configuration. To change a replacement actuator of track 3 to a Right Hand (RH) configuration:
CAUTION : DO NOT DISENGAGE THESE ITEMS FROM THE OFFSET GEARBOX WHEN
_______ YOU CHANGE THE CONFIGURATION FROM LH TO RH :
-
THE TORQUE LIMITER
-
THE ROTARY ACTUATOR.
THESE ITEMS ARE NOT LRU'S AND ARE NOT INTERCHANGEABLE.
(a)
Remove the nuts (12), the bolts (15) and the washers (11).
(b)
Keep the mating surface of the torque limiter assembly (13) in contact with the offset gearbox (16). Turn the torque limiter assembly (13) until the arrow is aligned with the 'R' mark on the offset gearbox (16).
(c)
Install the bolts (15), the washers (11) and the nuts (12).
(d)
TORQUE all the nuts (12) to between 0.78 and 0.96 m.daN (69.02 and 84.95 lbf.in).
(e)
Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to the bolts (15), the washers (11) and the nuts (12).
(2) Make sure the arrow on the rotary actuator (17) is between the lines on the offset gearbox (16).
NOTE : The arrow on the rotary actuator (17) and the marks on the
____ offset gearbox (16) are the same for the LH and RH configurations.
(3) Make sure the flap track 3 actuator and the torque limiter are aligned.
R 1EFF : 001-049, 051-061, 101-105, 201-203, 1 27-54-49Page 493 1 1 May 01/05 1 1 1CES 1R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
Subtask 27-54-49-560-051-A
A. Preparation for a Replacement Component
(1) Replacement actuator assemblies of flap track 3 are supplied in the Left Hand (LH) configuration. To change a replacement actuator of track 3 to a Right Hand (RH) configuration:
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱5(121)
