Subtask 27-84-45-710-053
G. Test
R R (1) Do an operational test of the slat power-transmission system (Ref. TASK 27-84-00-710-001). Make sure that the rotation of the torque shafts does not cause damage.
5. Close-up________
R (Ref. Fig. 401/TASK 27-84-45-991-001)
Subtask 27-84-45-865-070
A. 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 27-84-45-410-053
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other items.
R R (2) Install the applicable access panels: - FOR 6012CM install 521AB, 521BB, 521CB and 191BT - FOR 6062CM install 621AB, 621BB, 621CB and 192BT.
Subtask 27-84-45-865-071
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
Subtask 27-84-45-942-054
D. 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 27-84-45Page 449 1 1 Feb 01/00R 1 1 1CES 1
TASK 27-84-45-000-006
Removal of the Torque Shafts 6014CM(6064CM)/6028CM(6078CM)/6036CM(6086CM)/ 6038CM(6088CM)/6040CM(6090CM)/6042CM(6092CM)/6044CM(6094CM)
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.
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 circuit breaker(s) safety clip(s) No specific safety barriers No specific warning notice No specific adjustable access platform 4.0 m (13 ft. 1 in.) 98D27504030001 2 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-50-00-400-003 Installation of the Lock-Torque Shaft - Flaps and
Slats (98D27504030001) 27-80-00-866-005 Retracting the Slats on the Ground 27-84-45-991-001 Fig. 401 27-84-45-991-002 Fig. 402
1EFF : ALL 1 27-84-45Page 450 1 1 May 01/98R 1 1 1CES 1
3. Job Set-up
__________ (Ref. Fig. 401/TASK 27-84-45-991-001) Subtask 27-84-45-941-054
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Put a warning notice in position to tell persons not to operate the slat controls.
Subtask 27-84-45-860-069
B. Aircraft Maintenance Configuration
(1)
Retract the slats fully (Ref. TASK 27-80-00-866-005).
(2)
Make sure that the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) is on the flap/slat control lever on panel 114VU.
Subtask 27-84-45-865-054
C. 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 27-84-45-010-054
D. Get Access
(1)
Put the adjustable access platform in position below the applicable access panel.
(2)
Remove the applicable access panel(s):
-
FOR 6014CM
remove 521CB, 521EB
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱7(139)
