-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 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER
1EFF : ALL 1 27-51-00Page 595 1 1 May 01/05R 1 1 1CES 1
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-50-00-866-009 Retraction of the Flaps on the Ground 27-51-00-820-008 Adjustment of the Flap Rigged Position With the Sharks Fin Tool (A318/319/320) 27-51-00-820-009 Adjustment of the Flap Rigged Position With the Sharks Fin Tool (A321) R 27-51-00-991-015-A Fig. 515
3. Job Set-up
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Subtask 27-51-00-941-067
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Put a warning notice on panel 114VU to tell persons not to operate the flap/slat controls.
Subtask 27-51-00-860-060
B. Aircraft Maintenance Configuration 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 aircraft weight is on the landing gear when you do the flap rigged position procedure.
(2)
Make sure that the flaps are fully retracted (Ref. TASK 27-50-00-866-009).
(3)
Install the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) on the flap/slat control lever.
4. Procedure
_________
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 27-51-00-480-052
A. Preparation for Adjustment of the Forward Eccentrics
(1) At the track 3 and track 4 positions, install the sharks fin flap rigging kit (Ref. TASK 27-51-00-820-008).
**ON A/C 301-399,
Subtask 27-51-00-480-052-A
A. Preparation for Adjustment of the Forward Eccentrics
(1) At the track 3 and track 4 positions, install the sharks fin flap rigging kit (Ref. TASK 27-51-00-820-009).
R **ON A/C 001-049, 053-061, 101-105, 201-203,
Subtask 27-51-00-820-053
B. Adjustment of the Forward Eccentrics R (Ref. Fig. 515/TASK 27-51-00-991-015-A)
(1)
Remove and discard the cotter pin (5) from the nut (4).
(2)
At the track 3 position, remove the nut (4), the washer (3), the bolt
(1) and the serrated plate (2).
(3)
At the track 4 position, remove the bolt (7), the washer (8) and the serrated plate (9).
R R Forward Eccentrics - Location and Detail Figure 515/TASK 27-51-00-991-015-A
1EFF : 1 1 1CES ALL 1 111 27-51-00 Page 598 Aug 01/05
(4) Adjust the forward eccentrics (6) and (10) in sequence. Make sure that the adjustments are in small equal increments, to move the flap deflection by the same amount.
NOTE : Flap movement is opposite to the value shown on the label____ attached to the flap track 3 beam assembly. For a '+' label value the flap must be moved down. For a '-' label value the flap must be moved up.
(5) At the track 3 position, temporarily install the serrated plate (2) with the bolt (1), the washer (3) and the nut (4).
(6) At the track 4 position, temporarily install the serrated plate (9) with the bolt (7) and the washer (8).
(7) Make sure that the punched/painted marks on the forward eccentrics align.
(8) Remove the sharks fin flap rigging kit (Ref. TASK 27-51-00-820-008) or (Ref. TASK 27-51-00-820-009).
R **ON A/C 051-052, 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
R Subtask 27-51-00-820-053-A
R R B. Adjustment of the Forward Eccentrics (Ref. Fig. 515/TASK 27-51-00-991-015-A)
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本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵4(61)
