**ON A/C ALL
3. Job Set-up
__________
**ON A/C 001-049, 051-061, 101-103, 201-203,
(Ref. Fig. 402/TASK 27-54-49-991-001)R **ON A/C 062-099, 106-149, 151-199, 204-299, 401-499,
(Ref. Fig. 402A/TASK 27-54-49-991-001-B)
**ON A/C 104-105,
(Ref. Fig. 402B/TASK 27-54-49-991-001-A)
**ON A/C 301-399,
(Ref. Fig. 402C/TASK 27-54-49-991-001-C)
**ON A/C ALL
Subtask 27-54-49-941-067
A. Safety Precautions WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
(1)
Make sure that the safety barriers are in position.
(2)
Make sure that the warning notice are in position to tell persons not to operate the flaps.
(3)
Make sure that the warning notice are in position to tell persons not to operate the landing gear doors.
Subtask 27-54-49-860-054
B. Aircraft Maintenance Configuration
(1)
Make sure that the flaps are extended fully (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 applicable MLG door is open (Ref. TASK 32-12-00-010-001).
(4)
Make sure that the GROUND LOCK SLEEVE is on the applicable MLG door actuator.
(5)
Make sure that the access platform is below the applicable access panel.
(6)
Make sure that the flap trailing edge is on a support.
(7)
Make sure that the clamp holds the carriage in position.
(8)
Make sure that the applicable access panels are removed:
(a) For the LH wing:
-
panels 193AB, 193BB
-
panels 573AB, 573BB (Ref. TASK 57-51-37-000-002).
(b) For the RH wing:
-
panels 194AB, 194BB
-
panels 673AB, 673BB (Ref. TASK 57-51-37-000-002).
(9)
Make sure that the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT is installed on the applicable torque shaft.
(10) Make sure that the torque shaft (1), the torque shaft (4) and the universal joint (3) have been removed (Ref. TASK 27-54-45-000-003) and (Ref. TASK 27-54-45-000-002).
Subtask 27-54-49-865-058
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, 051-061, 101-103, 201-203,
(Ref. Fig. 402/TASK 27-54-49-991-001)R **ON A/C 062-099, 106-149, 151-199, 204-299, 401-499,
(Ref. Fig. 402A/TASK 27-54-49-991-001-B)
**ON A/C 104-105,
(Ref. Fig. 402B/TASK 27-54-49-991-001-A)
**ON A/C 301-399,
(Ref. Fig. 402C/TASK 27-54-49-991-001-C)
**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, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 27-54-49-560-052
A. Preparation for a Replacement Component
(1) Replacement actuator assemblies of flap track 1 are supplied in the Right Hand (RH) configuration. To change a replacement actuator of track 1 to a Left Hand (LH) 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 bolts (6) and the washers (5).
(b)
Keep the mating surface of the torque limiter in contact with the offset gearbox. Turn the input bevel housing until its arrow aligns with the LH mark (11) on the offset gearbox case.
(c)
Install the bolts (6) and the washers (5).
