(b) For the RH wing:
R R - 6092CM (inboard of the wing-tip brake) - 6094CM (outboard of the wing-tip brake).
(10) Make sure that you cannot see the groove on the splines of the universal joints.
(11) Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to: - the nuts (19), the bolts (20) and the studs on the the wing-tip brake (1) - the flanges of the universal joint (18) and the torque shaft.
(12) Remove the blanking plugs from the hydraulic lines.
(13) Make sure that the ends of the hydraulic lines are clean and in the correct condition.
(14) Lubricate the coupling nuts on the hydraulic lines (13), (16), (21) and (26) with HYDRAULIC FLUIDS (Material No. 02-003).
(15) Connect the hydraulic lines (13), (16), (21) and (26) to the wing-tip brake (1) and tighten the coupling nuts.
(16) Remove the blanking caps from the electrical connectors (7) and (10).
(17) Make sure that the electrical connectors (7) and (10) are clean and in the correct condition.
(18) Connect the electrical connectors (7) and (10) to the wing-tip brake (1).
R R (19) Connect the bonding strap (2) to the T-piece (3) with the bolt (4), the washer (5) and the nut (6) (Ref. TASK 20-28-00-912-004).
Subtask 27-81-51-860-054
C. Aircraft Maintenance Configuration
R R (1) Fill the Blue and the Green Hydraulic reservoirs (Ref. TASK 12-12-29-611-001) or (Ref. TASK 12-12-29-611-002).
(2) Remove the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER from the flap/slat control lever.
(3) Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT from each torque shaft (Ref. TASK 27-50-00-000-003).
R 1EFF : ALL 1 27-81-51Page 413 1 1 Feb 01/00 1 1 1CES 1 Subtask 27-81-51-865-052
D. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s): R 9CV, 11CV.
Subtask 27-81-51-480-050
E. Installation of Support Equipment
(1) Install the safety collar on the circuit breakers 9CV and 11CV.
Subtask 27-81-51-863-050
F. Pressurize the Hydraulic System WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES
_______ ARE CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
WARNING : MAKE SURE THAT THE CONTROLS AGREE WITH THE POSITION OF THE
_______ ITEMS THEY OPERATE BEFORE YOU PRESSURIZE A HYDRAULIC SYSTEM.
R (1) Pressurize the Blue and the Green Hydraulic systems (Ref. TASK 29-10-R 00-863-003) and (Ref. TASK 29-10-00-863-001).
NOTE : The hydraulic supplies to the wing-tip brake are bled
____
automatically.
Subtask 27-81-51-790-050
G. Test CAUTION : MAKE SURE THE POWER TRANSMISSION SYSTEM IS COMPLETE BEFORE YOU
_______
DO A PREPARATION FOR TEST OR A TEST.
(1)
Examine the wing-tip brake and the related hydraulic connections for leaks.
(2)
Do an operational test of the slats wing-tip brake (Ref. TASK 27-81-00-710-001).
INTENTIONALLY BLANK
R 1 1
27-81-51Page 415
1 1 Feb 01/00 1 1 1CES 1
INTENTIONALLY BLANK
R 1 1
27-81-51Page 416
1 1 Feb 01/00 1 1 1CES 1 (3) Do a leak check on the slats wing-tip brake:
-examine the four witness drain holes in the wing-tip brake for leaks.
NOTE : This area is not pressurized during normal operation, so leaks
____ will only show after the operational test.
5. Close-up
________ Subtask 27-81-51-410-050
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Install the access panels:
-
FOR 35CV
install 522QB, 522SB, 522UB
-
FOR 36CV
install 622QB, 622SB, 622UB.
Subtask 27-81-51-942-050
B. Removal of Equipment
(1)
Remove the safety barriers.
(2)
Remove the warning notice(s).
(3)
Remove the access platform(s).
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
1EFF : ALL 1 27-81-51Page 417 1 1 May 01/98R 1 1 1CES 1
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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(80)
