(2)
 Do the ADIRS stop procedure (Ref. TASK 34-10-00-860-005).

 (3)
 Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).

 (4)
 De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).

 1EFF : ALL 1 27-21-00Page 539 1 1 Aug 01/04R 1 1 1CES 1

 TASK 27-21-00-820-002
 Adjustment of the Rudder Control-Cables Length
 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 TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______ MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
 CAUTION : MAKE SURE THAT THE AIRCRAFT IS IN THE TEMPERATURE CONDITIONS (STABLE
_______ AMBIENT TEMPERATURE) SPECIFIED IN THE AIRCRAFT MAINTENANCE CONFIGURATION PARAGRAPH. CHANGES IN THE TEMPERATURE CAN CAUSE INCORRECT MEASUREMENTS.
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific mirror No specific tensiometer No specific thermometer No specific warning notices No specific 1 ACCESS PLATFORM 2M (6 FT) No specific 1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE 98A27901002000 1 PIN, RIGGING - RUDDER CONTROL 98D27203500000 1 BRACKET TENSION REGULATOR-RUDDER CONTROL 98D27207516000 1 RIGGING PIN SET 98D27207547000 1 PIN - RIGGING
 1EFF : ALL 1 27-21-00Page 540 1 1 Aug 01/04R 1 1 1CES 1

 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific  Lockwire corrosion resistant steel dia 0.6 mm (0.02 in.)
 C. Expendable Parts
 -------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
8 locking clips 27-21-01 11B-010 8 locking clips 27-21-01 11D-010
 D. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-33-21-618-001 Pre-conditioning through the LP Ground Connection 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 27-21-00-820-004 Shortening of the Rudder Control Cable 27-21-00-840-001 Removal/Installation of the control rod on the rudder
 mechanical control 27-24-00-710-001 Operational Test of the Rudder Hydraulic Actuation 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground
 Power Supply 29-10-00-864-003 Depressurize the Blue Hydraulic System 52-41-00-410-002 Close the Avionics Compartment Doors after Access 53-12-11-000-001 Removal of the Cockpit Floor Panels from FR1 Thru
 FR12 53-12-11-400-001 Installation of the Cockpit Floor Panels from FR1
 thru FR12
 53-32-12-000-002 Removal of the Cabin Floor Panels
 53-32-12-400-002 Installation of the Cabin Floor Panels

R 27-21-45-000-001 Removal of the Cable Tension Regulator Assy (for
 corrective action) R 27-21-45-400-001 Installation of the Cable Tension Regulator Assy (for R corrective action)

 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
27-21-61-000-001 Removal of the Rudder Control Cables (for corrective action) 27-21-61-400-001 Installation of the Rudder Control Cables (for corrective action)
 **ON A/C 001-049, 051-099, 101-105, 151-199, 201-217,
 27-21-00-991-008 Fig. 507 R **ON A/C 106-149, 218-299, 301-399, 401-499,
 27-21-00-991-008-A Fig. 507A
 **ON A/C ALL
 27-21-00-991-009 Fig. 508
 3. Job Set-up
__________
 CAUTION : DO THIS PROCEDURE IN A HANGAR IF THERE ARE WIND GUSTS. WIND GUSTS

_______ CAN CAUSE DAMAGE TO THE LINKAGE WHEN THE RIGGING PINS ARE IN POSITION ON THE RUDDER CONTROL.
 Subtask 27-21-00-010-055
 A. Get Access
 (1)
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱1(148)