____
be contavted.
Subtask 27-34-51-220-058-A
F. Fits and Clearances
(1) Complete an inspection of these dimensions.
-------------------------------------------------------------------------------| 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.)| |--------|---------|---------|---------|---------|---------|---------|--------| | F | 15.850 | 15.861 | | | 15.821 | | | | OD 5 |(0.6240) |(0.6244) | | |(0.6228) | | | | | | | 0.014 | 0.043 | | | 0.101 | | | | | (0.0005)| (0.0016)| | |(0.0039)| | F | 15.875 | 15.893 | | | | 15.922 | | | ID 9 |(0.6250) |(0.6257) | | | |(0.6268) | | -------------------------------------------------------------------------------
Subtask 27-34-51-220-059-A
G. Fits and Clearances
(1) Complete an inspection of these dimensions.
-------------------------------------------------------------------------------| 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.)| |--------|---------|---------|---------|---------|---------|---------|--------| | F | 19.480 | 19.493 | | | 19.456 | | | | OD 9 |(0.7669) |(0.7674) | | |(0.7659) | | | | | | | 0.007 | 0.041 | | | 0.089 | | | | | (0.0002)| (0.0016)| | |(0.0035)| | F | 19.500 | 19.521 | | | | 19.545 | | | ID 8 |(0.7677) |(0.7685) | | | |(0.7694) | | ------------------------------------------------------------------------------- NOTE : If bushing item 8 can be rotated by hand force, AIRBUS has to
____
be contacted.
5. Close-up
________ Subtask 27-34-51-410-059
A. Close Access
(1) Install the elevator servo control (Ref. TASK 27-34-51-400-001). Subtask 27-34-51-942-058
B. Removal of Equipment
(1) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
TRIMMABLE HORIZONTAL STABILIZER (THS) - DESCRIPTION AND OPERATION
_________________________________________________________________
1. General
_______ (Ref. Fig. 001) A trimmable horizontal stabilizer (THS) hinged on the rear part of the fuselage ensures the pitch trim control. The two elevators are hinged on the THS. An actuator with a fail-safe ball screwjack (Ref. 27-44) drives the THS, its structural attachments are also fail-safe. Three electric motors ensure the normal control of the actuator. They are under the control of the two ELACs and the two SECs. The actuator achieves the autotrim function of the manual or auto-flight modes and automatically places the THS at the center of the green band at touchdown. The standby control is mechanical. The pilots can override the electrical control via the mechanical control system, through the application of a sufficient force to the control wheels. An override mechanism in the THS actuator is used for that purpose. The override mechanism reverts to the electrical control after release of the mechanical control.
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Trimmable Horizontal Stabilizer
Figure 001
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TRIMMABLE HORIZONTAL STABILIZER (THS) - DEACTIVATION/REACTIVATION
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