(2)
Install the access panel 191KB.
(3)
Remove the access platform(s).
GEARBOX - TEE (6005CM) - REMOVAL/INSTALLATION
_____________________________________________
TASK 27-84-42-000-001
Removal of the Tee Gearbox 6005CM
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
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.
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 warning notice No specific access platform 2.6 m (8 ft. 6 in.) 98D27504030001 2 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-00-00-480-002 Installation of the Flap/Slat Control-Lever Locking
Tool (98D27803000000) 27-80-00-866-005 Retracting the Slats on the Ground 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized
Configuration before Maintenance Action
27-84-42-991-001 Fig. 401
27-84-42-991-002 Fig. 402
3. Job Set-up
__________
Subtask 27-84-42-866-050
A. Retraction of the Slats
(1)
Retract the slats to the 0 degree position (Ref. TASK 27-80-00-866-005).
(2)
Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) (Ref. TASK 27-00-00-480-002) on the slat/flap control lever.
Subtask 27-84-42-865-050
B. 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
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
122VU AIR COND/PACK TEMP/CTL SYS1/2/115VAC 21HH W22 122VU AIR COND/PACK TEMP/CTL SYS1/2/28VDC 23HH W21 122VU AIR COND/PACK TEMP CTL SYS2/2/28VDC 24HH Y21 122VU AIR COND/PACK TEMP CTL SYS2/2/115VAC 22HH Y20R **ON A/C ALL
Subtask 27-84-42-860-050
C. Aircraft Maintenance Configuration
(1)
Put the access platform in position.
(2)
Depressurize the Green and Blue hydraulic systems and put them in the maintenance configuration (Ref. TASK 29-00-00-864-001).
(3)
Put the warning notice in position to tell persons not to pressurize the hydraulic systems.
(4)
Install the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (98D27504030001) to lock the left slat transmission.
(5)
Install the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (98D27504030001) to lock the right slat transmission.
Subtask 27-84-42-010-050
D. Get Access
(Ref. Fig. 401/TASK 27-84-42-991-001)
(1)
Remove the access panel 191BB.
(2)
Disconnect the V-clamp (4).
(3)
Disconnect the clamp (2).
(4)
Remove the bellows (3), the clamp (2) and the V-clamp (4).
4. Procedure
_________
(Ref. Fig. 402/TASK 27-84-42-991-002)
Subtask 27-84-42-020-050
A. Removal of the Tee Gearbox
(1)
Disconnect the torque shaft 6004CM (9) as follows:
(a)
Remove the nuts (7) and the bolts (8) which connect the torque shaft (9) to the input universal joint (6) of the tee gearbox (1).
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7(105)
