__________
(Ref. Fig. 401/TASK 27-84-44-991-001)
Subtask 27-84-44-941-056
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Put a warning notice(s) in the cockpit to tell persons not to operate the slat controls.
(3)
Put a warning notice in position to tell persons not to operate the landing gear doors.
(4)
Make sure that the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) is on the slat/flap control lever.
Subtask 27-84-44-865-062
B. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
R 49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
Subtask 27-84-44-010-052
C. Get Access
(1)
Put an access platform in position below the applicable torque shaft.
(2)
Open the main gear doors (Ref. TASK 32-12-00-010-001).
(3)
Make sure that the GROUND LOCK SLEEVE in on the applicable main gear door actuator.
(4)
Remove the applicable torque shaft (6) (Ref. TASK 27-84-45-000-002): FOR 6007CM remove the torque shaft FIN 6006CM FOR 6057CM remove the torque shaft FIN 6056CM.
(5)
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).
Steady Bearings - Slat Power Transmission
Figure 401/TASK 27-84-44-991-001
1EFF : ALL 1 27-84-44 Page 403
1 1 Feb 01/98
1 1
1CES 1
4. Procedure
_________
(Ref. Fig. 401/TASK 27-84-44-991-001) Subtask 27-84-44-020-050
A. Removal of the Steady Bearing FIN 6007CM (6057CM)
(1)
Remove the bolts (3) and the nuts (1).
(2)
Remove the steady bearing (5) from the torque shaft (4) and the steady bearing bracket (2).
TASK 27-84-44-400-001
Installation of the Steady Bearing FIN 6007CM(6057CM)
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 No specific access platform 3.5 m (11 ft. 6 in.)
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 27-84-45-400-003 Installation of the Torque Shafts 6006CM(6056CM) 32-12-00-010-001 Open the Main Gear Doors for Access 32-12-00-410-001 Close the Main Gear Doors after Access
3. Job Set-up
__________
Subtask 27-84-44-941-062
A. Safety Precautions
(1)
Make sure that the safety barriers are in position.
(2)
Make sure that the warning notice is in the cockpit to tell persons not to operate the slat controls.
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