-
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
__________________
R R 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(s)
No specific access platform 3.5 m (11 ft. 6 in.)
98D27504030001 1 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT
98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL 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 27-84-44-000-006 Removal of the Steady Bearing FIN 6031CM(6081CM) 27-84-45-991-001 Fig. 401 27-84-45-991-002 Fig. 402
3. Job Set-up
__________ (Ref. Fig. 401/TASK 27-84-45-991-001) Subtask 27-84-45-941-074
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Put a warning notice(s) in position to tell persons not to operate the slat controls.
Subtask 27-84-45-860-073
B. Aircraft Maintenance Configuration
(1)
Retract the slats fully (Ref. TASK 27-80-00-866-005).
(2)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) is on the flap/slat control lever on panel 114VU.
Subtask 27-84-45-865-102
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 27-84-45-010-058
D. Get Access
(1)
Put the access platform in position below the applicable access panel 522FB(622FB).
(2)
Remove the applicable steady bearing (15) (Ref. TASK 27-84-44-000-006):
-
FOR 6032CM
remove the steady bearing FIN 6031CM
-
FOR 6082CM
remove the steady bearing FIN 6081CM.
1EFF : ALL 1 27-84-45Page 498 1 1 May 01/98R 1 1 1CES 1
(3) Remove the applicable access panel:
-
FOR 6032CM
remove 522FB
-
FOR 6082CM
remove 622FB.
4. Procedure
_________
(Ref. Fig. 402/TASK 27-84-45-991-002)
Subtask 27-84-45-020-060
A. Removal of the Torque Shafts 6032CM(6082CM)
(1)
Install a LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (98D27504030001) (Ref. TASK 27-50-00-400-003): - on the torque shaft, inboard of the applicable components - on the torque shaft, outboard of the applicable components.
(2)
Remove the nuts (16), the bolts (17) and the shaft (14).
(3)
Remove the retaining ring (18), the pin (12) and the universal joint (13).
1EFF : ALL 1 27-84-45Page 499 1 1 May 01/98R 1 1 1CES 1
TASK 27-84-45-400-012
Installation of the Torque Shaft 6032CM(6082CM)
WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______
NOTICES ARE IN POSITION.
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
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(11)
