NOTE : No wear is permitted between the bolt (3) and the bush (4).
____
(1) If necessary, replace the bolt (3) and/or the bush (4).
Subtask 27-24-51-220-053
D. Measurement of the Fits and Clearances
-------------------------------------------------------------------------------| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS | | DETAIL |---------------------------------------|----------------------------| | AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. | | ITEM | MM (IN.) | MM (IN.) | MM (IN.) | ALLOW. | | NO. |-------------------|-------------------|---------|---------| CLEAR. | | | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |MM (IN.)| |--------|---------|---------|---------|---------|---------|---------|--------| | C,D | 22.984 | 23.000 | | | 22.984 | | | | OD 4 |(0.9048) |(0.9055) | | |(0.9048) | | | | | | | 0.000 | 0.037 | | | 0.037 | | | | | (0.0000)| (0.0014)| | |(0.0014)| | C,D | 23.000 | 23.021 | | | | 23.021 | | | ID 5 |(0.9055) |(0.9063) | | | |(0.9063) | | -------------------------------------------------------------------------------
NOTE : No wear is permitted between the bush (4) and the bush (5).
____
(1) If necessary, replace the bush (4) and/or the bush (5) (Ref. CMM 55-41-13).
5. Close-up
________
Subtask 27-24-51-410-055
A. Install the rudder servo control (Ref. TASK 27-24-51-400-001).
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RUDDER POSITION INDICATING - DESCRIPTION AND OPERATION
______________________________________________________
1. General
_______ (Ref. Fig. 001) The position of the rudder is shown on the lower display unit of the ECAM system. This position is transmitted to the SDAC through a position transducer. A triangle NSA950200 is sticked on the tail cone structure. At the zero position, the center of gravity of this triangle is in line with the rudder lower trailing edge
NOTE : The rudder trim travel is shown on the rudder trim indicator in the
____ form of a digital value. This information is supplied by the FAC through a position transducer installed on trim actuator (Ref.27-22).
Special Reference Mark
Figure 001
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1 1 Feb 01/98
1 1
1CES 1
RUDDER POSITION INDICATING - ADJUSTMENT/TEST
____________________________________________ TASK 27-25-00-820-001 Adjustment of the Rudder Position Indicating WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
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 CONTROL SURFACES ARE
_______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform 5.87 m (19 ft. 3 in.) 98D27207516000 1 RIGGING PIN SUPSD BY 98D27207545000 TO 98D27207549000 98D27207546000 1 PIN - RIGGING
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific Lockwire corrosion resistant steel dia 0.8 mm (0.03 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 27-24-00-710-001 Operational Test of the Rudder Hydraulic Actuation 27-24-00-820-001 Adjustment of the Rudder Neutral Position 29-10-00-863-003 Pressurize the Blue Hydraulic System 29-10-00-864-003 Depressurize the Blue Hydraulic System 29-23-00-863-001 Pressurize the Green Hydraulic System from the Yellow
Hydraulic System through the PTU with the Electric Pump 29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU 29-24-00-863-001 Pressurize the Yellow Hydraulic System with the
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