Subtask 27-84-66-865-054
J. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV, 9CV, 11CV.
Subtask 27-84-66-410-053
K. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Install the safety collar on the circuit breakers 9CV and 11CV.
(3)
Install the applicable torque shaft (Ref. TASK 27-84-45-400-005):
-
for the left wing, install FIN 6010CM
-
for the right wing, install FIN 6060CM.
(4)
Install the applicable access panel (Ref. TASK 57-41-37-400-006):
-
for the left wing, install 522NB
-
for the right wing, install 622NB.
Subtask 27-84-66-220-054
L. Check
(1) Do a check of the permitted aerodynamic tolerances between the slats 1 thru 5 (Ref. TASK 27-80-00-200-002).
1EFF : ALL 1 27-84-66Page 421 1 1 May 01/05R 1 1 1CES 1
Subtask 27-84-66-710-051
M. Test
(1) The operational test of the slat system (Ref. TASK 27-84-00-710-001), was done during the installation of the torque shaft FIN 6010CM (6060CM).
5. Close-up
________ Subtask 27-84-66-942-053
A. Removal of Equipment
(1)
Remove the safety barriers.
(2)
Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever on panel 114VU.
(3)
Remove the warning notice(s).
(4)
Remove the access platform(s).
(5)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
SLAT 5 - REMOVAL/INSTALLATION
_____________________________
TASK 27-84-67-000-001
Removal of the No. 5 Slat
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.
R WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______ R MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR R DAMAGE.
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-covers No specific circuit breaker(s) safety clip(s) No specific pneumatic wrench No specific safety barriers No specific support structure No specific warning notice No specific adjustable access platform 3.5 m (11 ft. 6 in.) 98D27504030001 1 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT 98D27804001000 1 ADAPTOR-DRIVE, SLAT (AND FLAP) 98D27804009001 2 SLING-SLATS
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External Power 24-42-00-862-001 De-energize the Ground Service Network Supplied from the External Power 27-50-00-000-003 Removal of the Lock-Torque Shaft - Flaps and Slats (98D27504030001) 27-50-00-400-003 Installation of the Lock-Torque Shaft - Flaps and
Slats (98D27504030001) 27-80-00-000-001 Removal of the Hoisting Sling 27-80-00-400-001 Installation of the Hoisting Sling 27-80-00-866-005 Retracting the Slats on the Ground 27-84-45-000-004 Removal of the Torque Shaft 6010CM(6060CM) 27-84-69-000-001 Removal of the Closing Plates for the Slat Tracks 1
thru 12 31-32-00-860-006 Procedure to Get Access to the SYSTEM REPORT/TEST F/CTL Page
57-41-37-000-006 Removal of the Access Panels 522FB(622FB),
522JB(622JB), 522KB(622KB), 522LB(622LB),
522NB(622NB), 522QB(622QB), 522SB(622SB),
522UB(622UB)
27-84-67-991-001 Fig. 401
**ON A/C 001-049, 051-061, 101-105, 201-203,
27-84-67-991-002 Fig. 402
R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
27-84-67-991-002-A Fig. 402A
**ON A/C ALL
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱8(144)
