(2)
Put a warning notice(s) in the cockpit to tell persons not to operate the slat controls.
(3)
Make sure that the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) is on the slat/flap control lever.
Subtask 27-84-44-865-069
B. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
Subtask 27-84-44-010-051
C. Get Access
(1)
Put an adjustable access platform in position below the applicable zone 522 (622).
(2)
Remove the applicable access panel:
-
FOR 6031CM
remove 522EB
-
FOR 6081CM
remove 622EB.
(3)
Remove the applicable torque shaft (43) (Ref. TASK 27-84-45-000-007):
-
FOR 6031CM
remove the torque shaft FIN 6030CM
-
FOR 6081CM
remove the torque shaft FIN 6080CM.
(4)
Make sure that the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (98D27504030001) is on the applicable torque shaft (Ref. TASK 27-50-00-400-003).
4. Procedure
_________
(Ref. Fig. 402/TASK 27-84-44-991-002) Subtask 27-84-44-020-055
A. Removal of the Steady Bearing FIN 6031CM (6081CM)
(1)
Remove the bolts (38) and the nuts (40).
(2)
Remove the steady bearing (42) from the torque shaft (41) and the nose rib (39).
TASK 27-84-44-400-006
Installation of the Steady Bearing FIN 6031CM(6081CM)
WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______ NOTICES ARE IN POSITION.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
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
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 09-018 USA AMS 3267/3 CORROSION INHIBITING LOW ADHESION SEALANT (Ref. 20-31-00)
Material No. 09-019 USA AMS 3267/3 LOW ADHESION CORROSION INHIBITING SEALANT (Ref. 20-31-00)
Material No. 11-004 USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (Ref. 20-31-00)
Material No. 15-007 AIB TN 10138 TYPE II GRADE 1 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
Material No. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-50-00-400-003 Installation of the Lock-Torque Shaft - Flaps and
Slats (98D27504030001) 27-84-00-710-001 Operational Test of the Slat System 27-84-45-400-008 Installation of the Torque Shafts
6016CM(6066CM)/6020CM(6070CM)/6026CM
(6076CM)/6030CM(6080CM)
3. Job Set-up
__________
Subtask 27-84-44-941-067
A. Safety Precautions
(1)
Make sure that the safety barriers are in position.
(2)
Make sure that the warning notice is in the cockpit to tell persons not to operate the slat controls.
(3)
Make sure that the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER is on the flap/slat control lever.
Subtask 27-84-44-860-055
B. Aircraft Maintenance Configuration
(1)
Make sure that the adjustable access platform is below the applicable zone 522 (622).
(2)
Make sure that the applicable access panel 522EB (622EB) is removed.
(3)
Make sure that a LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT is installed (Ref. TASK 27-50-00-400-003) as follows: - on the torque shaft, inboard of the applicable component - on the torque shaft, outboard of the applicable component.
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱7(125)
