-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific blanking caps
No specific circuit breaker(s) safety clip(s)
No specific tie-wrap
No specific access platform 2.2 m (7 ft. 3 in.)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-80-00-866-005 Retracting the Slats on the Ground 32-12-00-010-001 Open the Main Gear Doors for Access 27-85-11-991-001 Fig. 401
3. Job Set-up
__________ Subtask 27-85-11-010-050
A. Open the main doors of the main gear (Ref. TASK 32-12-00-010-001).
Subtask 27-85-11-860-050
B. Aircraft Maintenance Configuration
(1)
Put the access platform in position at the opening of the main doors of the main gear.
(2)
Make sure that the slats are in the fully retracted position (Ref. TASK 27-80-00-866-005).
Subtask 27-85-11-865-050
C. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
R 49VU FLIGHT CONTROLS/SLT FLP/POS/IND 1 1CN B12 49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 R 121VU FLIGHT CONTROLS/SLT FLP/POS/IND2 2CN P16 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
4. Procedure
_________
(Ref. Fig. 401/TASK 27-85-11-991-001)
Subtask 27-85-11-020-050
A. Removal of the Instrumentation Position Pick-Off Unit NOTE : Do not remove the Instrumentation Position Pick-off Unit when the
____ Pressure-off Brakes are removed from the Power Control Unit.
(1)
Remove the electrical connectors 4CN-A and 4CN-B from the Instrumentation Position Pick-off Unit (IPPU).
(2)
Put blanking caps on the disconnected electrical connectors.
(3)
Remove the screws (1) and the washers (2).
(4)
Remove the IPPU carefully from the gearbox.
(5)
Put a tie-wrap (3) behind the locking plate to prevent retraction of the locking plate.
Instrumentation Position Pick-Off Unit
Figure 401/TASK 27-85-11-991-001
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TASK 27-85-11-400-001 Installation of the Instrumentation Position Pick-Off Unit WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform 2.2 m (7 ft. 3 in.) R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-002 USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00) Material No. 05-054 ZINC POWDER(USE WITH 05-002) (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-80-00-866-005 Retracting the Slats on the Ground
27-84-00-710-001 Operational Test of the Slat System
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