(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)
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本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵1(148)
