(12) Tighten the nut (13) and safety with cotter pin (14). Subtask 27-92-13-420-052
B. Connection of the electrical connectors and the bonding straps
(1)
Remove the blanking caps from the electrical connectors (3) and receptacles (2).
(2)
Connect the electrical connectors (3) to the receptacles (2).
(3)
Connect the bonding strap (9) with the bolt (8), the washer (10) and the nut (11).
(4)
Apply a coat of STRUCTURE PAINTS (Material No. 16-003) to the bonding connection.
5. Close-up
________ Subtask 27-92-13-410-050
A. Visual Inspection
(1) Make sure that the work area is clean and clear of tool(s) and other items.
Subtask 27-92-13-010-050
B. Close Access
(1) Close the trailing edge access panels 334BT,334DB and/or 344BT,344DB. (Ref. TASK 55-13-11-400-001).
Subtask 27-92-13-942-050
C. Remove Ground Equipment
(1)
Remove the warning notice(s).
(2)
Remove the access platform(s).
Subtask 27-92-13-081-050
D. Remove Locking Devices
(1) Remove the PIN-SIDE STICK LOCKING from the CAPT and F/O side stick
controllers. R
Subtask 27-92-13-865-053
E. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s): R 19CE1, 19CE2, 19CE3, 15CE1, 16CE1.
Subtask 27-92-13-720-050
F. Operational Test
(1) Do an operational test of the elevator and hydraulic actuation (Ref. TASK 27-34-00-710-001).
LEVER - SPEED BRAKE CONTROL ASSEMBLY (7CE) - REMOVAL/INSTALLATION
_________________________________________________________________
TASK 27-92-14-000-001
Removal of the Speedbrake Control Transducer Unit (7CE)
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.
R CAUTION : TO PREVENT POSSIBLE CROSS-CONNECTION OF THE ELECTRICAL CONNECTORS,
_______ R MAKE SURE THAT PLUGS AND RECEPTACLES ARE CLEARLY IDENTIFIED.
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 access platform 1.6 m (5 ft. 3 in.)
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
27-92-14-000-002 Removal of the Lighted Plate 29-10-00-864-003 Depressurize the Blue Hydraulic System 29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems
after Operation of the PTU
29-24-00-864-001 Depressurize the Yellow Hydraulic System
27-92-14-991-001 Fig. 401
3. Job Set-up
__________ Subtask 27-92-14-860-050
A. Aircraft Maintenance Configuration
(1)
Make sure that the SPEED BRAKE control lever is in the RET position.
(2)
Make sure that hydraulic systems are depressurized (Ref. TASK 29-23-00-864-001) (Ref. TASK 29-24-00-864-001) (Ref. TASK 29-10-00-864-003)
Subtask 27-92-14-010-050
B. Get Access
(1)
Put the access platform in position at the access door 822.
(2)
Open the access door 822.
(3)
On the battery power center 105VU:
-loosen the two screws and remove the protective cover. Subtask 27-92-14-865-050
C. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 105VU FLT CTL/SEC1/STBY SPLY 22CE B01 121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18 122VU LIGHTING/INSTL LT/MAIN INST/PNL AND/PED 4LF Y04
4. Procedure
_________
(Ref. Fig. 401/TASK 27-92-14-991-001) Subtask 27-92-14-020-050
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱9(18)
