(b)
Disconnect the torque shaft (9) from the input universal joint (6).
(2)
Disconnect the torque shaft 6006CM (26) as follows:
(a)
Remove the nuts (7) and the bolts (8) which connect the torque shaft (26) to the left input universal joint (22) of the tee gearbox (1).
(b)
Disconnect the torque shaft (26) from the left input universal joint (22).
(c)
Remove the left input universal joint (22) from the tee gearbox (1).
(3)
Remove the tee gearbox (1) as follows:
(a)
Hold the tee gearbox (1) so that it can not fall.
(b)
Remove the bolts (18) and the washers (19) which attach the tee gearbox (1) to the support bracket.
(c)
Carefully move the tee gearbox (1) away from the input universal joint (15) and remove the tee gearbox (1).
(d)
Move the spring (5) and remove the pin (10).
(e)
Remove the input universal joint (6) from the tee gearbox (1).
Tee Gearbox (Sheet 1)
Figure 401/TASK 27-84-42-991-001
1EFF : ALL 1 27-84-42 Page 404
1 1 Feb 01/98
1 1
1CES 1
Tee Gearbox (Sheet 2)
Figure 402/TASK 27-84-42-991-002
1EFF : ALL 1 27-84-42 Page 405
1 1 Feb 01/98
1 1
1CES 1
TASK 27-84-42-400-001
Installation 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 warning notice
No specific access platform 2.2 m (7 ft. 3 in.) R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft)
No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft) 98D27504030001 2 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-018
GENERAL PURPOSE ASSEMBLY PASTE (Ref. 20-31-00)
Material No. 05-005 USA MIL-C-16173 GRADE II
CORROSION PREVENTIVE (Ref. 20-31-00)
Material No. 09-013 USA MIL-PRF-81733 TYPE I CLASS A
CORROSION INHIBITING BRUSH CONSISTENCY
(Ref. 20-31-00)
Material No. 09-019 USA AMS 3267/3
LOW ADHESION CORROSION INHIBITING SEALANT
(Ref. 20-31-00)
Material No. 11-002 USA MIL-PRF-680
DRY CLEANING SOLVENT (VARSOL/WHITE SPIRIT)
(Ref. 20-31-00)
Material No. 16-003 F ASNB70720
COATING (OBSOLETE USE 16-021) (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
20-28-00-912-004 Electrical Bonding of Components With Conductive
Bolts and Screws and Bonding Straps in the Fuselage R and in the Wings (this does not include the tanks)-27-00-00-080-002 Removal of the Flap/Slat Control-Lever Locking Tool
(98D27803000000) 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 27-84-00-710-001 Operational Test of the Slat System 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized
Configuration before Maintenance Action
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(106)
