R 5. Close-up________
R Subtask 27-21-45-420-054
R A. Install the cable tension regulator assy (Ref. TASK 27-21-45-400-001).
QUADRANT - CABLE - REMOVAL/INSTALLATION
_______________________________________
TASK 27-21-46-000-001
Removal of the Cable Quadrant
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 notices No specific access platform 2.06 m (6 ft. 9 in.) No specific access platform 5.50 m (18 ft. 1 in.) 98A27901002000 1 PIN, RIGGING - RUDDER CONTROL 98D27207547000 1 PIN - RIGGING 98D27207548000 1 PIN - RIGGING
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific lockwire 0.6 mm (0.024 in.)
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground
Power Supply
52-41-00-010-002 Open the Avionics Compartment Doors for Access
53-22-12-000-001 Removal of the Cabin Floor Panels
53-32-12-000-002 Removal of the Cabin Floor Panels
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
27-21-46-991-001 Fig. 401
**ON A/C 301-399,
27-21-46-991-001-A Fig. 401A
**ON A/C ALL
27-21-46-991-002 Fig. 402
27-21-46-991-003 Fig. 403
3. Job Set-up
__________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 401/TASK 27-21-46-991-001)
**ON A/C 301-399,
(Ref. Fig. 401A/TASK 27-21-46-991-001-A)
Cable Quadrant
Figure 401/TASK 27-21-46-991-001
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-21-46Page 403 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
R Cable Quadrant
R Figure 401A/TASK 27-21-46-991-001-A
R 1EFF : 301-399, 1 27-21-46 Page 404
1 1 May 01/04
1 1
1CES 1
**ON A/C ALL
(Ref. Fig. 402/TASK 27-21-46-991-002, 403/TASK 27-21-46-991-003)
Subtask 27-21-46-865-053
A. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AUTO FLT/FAC1/28VDC 5CC1 B04 49VU AUTO FLT/FAC1/26VAC 14CC1 B03 121VU AUTO FLT/RUDDER/TRIM/IND 15CC M20 121VU AUTO FLT/FAC2/28VDC 5CC2 M19 121VU AUTO FLT/FAC2/26VAC 14CC2 M18
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499, 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2(38)
