standard tools and all other items.
1EFF : ALL 1 27-84-45Page 411 1 1 Feb 01/00R 1 1 1CES 1
TASK 27-84-45-000-002
R Removal of the Torque Shaft 6006CM(6056CM)
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.
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 98D27504030001 2 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL 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 32-12-00-010-001 Open the Main Gear Doors for Access 53-35-13-000-002 Removal of the Quick-Release Access Panels from the
Belly Fairing Structure
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 27-84-45-941-072
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Put a warning notice in position to tell persons not to operate the slat controls.
(3)
Put a warning notice in position to tell persons not to operate the landing gear doors.
Subtask 27-84-45-860-065
B. Aircraft Maintenance Configuration
(1)
Retract the slats fully (Ref. TASK 27-80-00-866-005).
(2)
Make sure that the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) is on the flap/slat control lever on panel 114VU.
Subtask 27-84-45-865-051
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 27-84-45-010-051
D. Get Access
(1)
Open the applicable main gear door (Ref. TASK 32-12-00-010-001).
(2)
Make sure that the GROUND LOCK SLEEVE is on the applicable main gear door actuator.
(3)
Remove the applicable access panels 191BB, 192FB (Ref. TASK 53-35-13-000-002).
1EFF : ALL 1 27-84-45Page 413 1 1 May 01/98R 1 1 1CES 1
4. Procedure
_________
(Ref. Fig. 401/TASK 27-84-45-991-001, 402/TASK 27-84-45-991-002) Subtask 27-84-45-020-051
A. Removal of the Torque Shafts 6006CM(6056CM)
(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 component - on the torque shaft, outboard of the applicable component.
(2)
Remove the nuts (10), the bolts (11) and the shaft (9).
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(129)
