(8)
Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT, installed outboard of the removed torque shaft FIN 6010CM (6060CM) (Ref. TASK 27-50-00-000-003).
Subtask 27-84-65-865-054
H. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV, 9CV, 11CV
Subtask 27-84-65-480-050
J. Installation of Support Equipment
(1) Install the safety collar on the circuit breakers 9CV and 11CV.
1EFF : ALL 1 27-84-65Page 420 1 1 May 01/05R 1 1 1CES 1
Subtask 27-84-65-410-054
K. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
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.
(3)
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 27-84-65-220-055
L. Check
(1) Do a check of the permitted aerodynamic tolerances between the slats 1 thru 5 (Ref. TASK 27-80-00-200-002).
Subtask 27-84-65-710-051
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 27-84-65-942-053
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.
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SLAT 4 - REMOVAL/INSTALLATION_____________________________
TASK 27-84-66-000-001
Removal of the No. 4 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 R R WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR._______ MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
1. Reason for the Job__________________
Self Explanatory
2. Job Set-up Information______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R No specific No specific No specific No specific No specific No specific No specific 98D27803500001 98D27804001000 98D27804009001 blanking-coverscircuit breaker(s) safety clip(s)pneumatic wrenchsafety barrierssupport structure warning noticeadjustable access platform 3.5 m (11 ft. 6 in.) 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER1 ADAPTOR-DRIVE, SLAT (AND FLAP)1 SLING-SLATS
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R 24-42-00-861-001
R
R 24-42-00-862-001
R 27-50-00-000-003
27-50-00-400-003
27-80-00-000-001
27-80-00-400-001
27-80-00-866-005
27-84-45-000-004
27-84-69-000-001
R 31-32-00-860-006
R 57-41-37-000-006
27-84-66-991-002
27-84-66-991-003
27-84-66-991-001
3. Job Set-up
__________
Subtask 27-84-66-941-050
A. Safety Precautions Energize the Ground Service Network from the External Power De-energize the Ground Service Network Supplied from the External PowerRemoval of the Lock-Torque Shaft - Flaps and Slats (98D27504030001)Installation of the Lock-Torque Shaft - Flaps and Slats (98D27504030001)Removal of the Hoisting SlingInstallation of the Hoisting SlingRetracting the Slats on the GroundRemoval of the Torque Shaft 6010CM(6060CM)Removal of the Closing Plates for the Slat Tracks 1 thru 12 Procedure to Get Access to the SYSTEM REPORT/TEST F/CTL PageRemoval of the Access Panels 522FB(622FB), 522JB(622JB), 522KB(622KB), 522LB(622LB), 522NB(622NB), 522QB(622QB), 522SB(622SB), 522UB(622UB)Fig. 401Fig. 402Fig. 403
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