(5)
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).
(6)
Slowly, manually retract the slats to the fully retracted position.
(7)
Install the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT outboard of the removed torque shaft FIN 6010CM(6060CM) (Ref. TASK 27-50-00-400-003).
(8)
Look at the seal (85) to make sure that it touches the wing tip structure over its full length.
(9)
If the seal (85) does not touch the wing tip structure over its full length, do the adjustment again.
(10) When the adjustment is correct, 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).
1EFF : ALL 1 27-84-67Page 425 1 1 Nov 01/03R 1 1 1CES 1
(11) Manually extend the slats to the fully extended position.
(12) Install the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT outboard of the removed torque shaft FIN 6010CM(6060CM) (Ref. TASK 27-50-00-400-003).
(13) Fully tighten the screws (83).
Subtask 27-84-67-860-052
J. Aircraft Maintenance Configuration
R R (1) Use the pneumatic wrench and the ADAPTOR-DRIVE, SLAT (AND FLAP) to fully retract the slats to the zero position.
R (2) Energize the ground service network (Ref. TASK 24-42-00-861-001).
R R (3) On the MCDU display, make sure that the PPU DATA page is shown (to monitor the slats PPU position).
R R R R R R R (4) If necessary, use the pneumatic wrench and the ADAPTOR-DRIVE, SLAT (AND FLAP) to move the slat drive shaft until the PPU data (on the MCDU) shows the same values as recorded in Para. 3.B.: - the FPPU angle value must agree +/- 0.1 deg. - the APPU angle value must agree +/- 0.1 deg. - the FPPU and APPU angles must agree +/- 1.3 deg. - the LH APPU and the RH APPU angles must agree +/- 0.45 deg.
R (5) De-energize the ground service network (Ref. TASK 24-42-00-862-001).
R R (6) Remove the pneumatic wrench and the ADAPTOR-DRIVE, SLAT (AND FLAP) from the slat drive shaft.
R R (7) 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 27-84-67-865-054
K. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV, 9CV, 11CV.
Subtask 27-84-67-410-053
L. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Install the safety collars 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. Subtask 27-84-67-866-063
M. Move the Slats 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) Extend the slats fully (Ref. TASK 27-80-00-866-004). Subtask 27-84-67-410-054
N. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
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 27-84-67-866-064
P. Move the Slats 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) Retract the slats fully (Ref. TASK 27-80-00-866-005).
Subtask 27-84-67-220-054
Q. Check
(1) Do a check of the permitted aerodynamic tolerances between the slats 1 thru 5 (Ref. TASK 27-80-00-200-002).
Subtask 27-84-67-710-051
R. 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 27-84-67-942-052
A. Removal of Equipment
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the safety barriers.
(3)
Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever on panel 114VU.
(4)
Remove the warning notice(s).
(5)
Remove the access platform(s).
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵8(151)
