-
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
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REFERENCE QTY DESIGNATION
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No specific access platform 1.5 m (4 ft. 11 in.)
98A27901002000 1 PIN, RIGGING - RUDDER CONTROL
B. Referenced Information
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REFERENCE DESIGNATION
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24-42-00-861-001 Energize the Ground Service Network from the External Power
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
R **ON A/C 001-049, 051-062, 101-105, 151-152, 201-205,
27-21-43-991-003 Fig. 401 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R **ON A/C 063-099, 106-149, 153-199, 206-299, 301-399, 401-499,
27-21-43-991-003-A Fig. 401A
**ON A/C 001-049, 051-062, 101-105, 151-152, 201-205,
27-21-43-991-004 Fig. 402 R **ON A/C 063-099, 106-149, 153-199, 206-299, 301-399, 401-499,
27-21-43-991-004-A Fig. 402A
**ON A/C ALL
27-21-43-991-005 Fig. 403
3. Job Set-up
__________
Subtask 27-21-43-861-051
A. Energize the ground service network
(Ref. TASK 24-42-00-861-001)
Subtask 27-21-43-010-052
B. Get Access
(1) Put the access platform in position.
(2) Open the access door 811.
Subtask 27-21-43-860-053
C. Aircraft Maintenance Configuration
(1)
Pressurize the Blue hydraulic system (Ref. TASK 29-10-00-863-003).
(2)
On the center pedestal, on the panel 110VU, make sure that the RUD TRIM indicator shows 0.
(3)
Install the PIN, RIGGING - RUDDER CONTROL (98A27901002000) (1) on the
yaw/brake bellcrank (2) (see detail B). **ON A/C 001-049, 051-062, 101-105, 151-152, 201-205,
R (Ref. Fig. 401/TASK 27-21-43-991-003) **ON A/C 063-099, 106-149, 153-199, 206-299, 301-399, 401-499,
(Ref. Fig. 401A/TASK 27-21-43-991-003-A) **ON A/C ALL
(4) Depressurize the Blue hydraulic system (Ref. TASK 29-10-00-864-003). 4. Procedure_________ **ON A/C 001-049, 051-062, 101-105, 151-152, 201-205,
R (Ref. Fig. 401/TASK 27-21-43-991-003) **ON A/C 063-099, 106-149, 153-199, 206-299, 301-399, 401-499,
(Ref. Fig. 401A/TASK 27-21-43-991-003-A) **ON A/C 001-049, 051-062, 101-105, 151-152, 201-205,
R (Ref. Fig. 402/TASK 27-21-43-991-004) **ON A/C 063-099, 106-149, 153-199, 206-299, 301-399, 401-499,
(Ref. Fig. 402A/TASK 27-21-43-991-004-A) **ON A/C ALL
(Ref. Fig. 403/TASK 27-21-43-991-005)
Rigging Pin Location
Figure 401/TASK 27-21-43-991-003
R 1EFF : 001-049, 051-062, 101-105, 151-152, 1 27-21-43Page 404 1201-205, 1May 01/05 1 1 1CES 1
Rigging Pin Location
Figure 401A/TASK 27-21-43-991-003-A
R 1EFF : 063-099, 106-149, 153-199, 206-299, 1 27-21-43Page 405 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1
Component Location
Figure 402/TASK 27-21-43-991-004
R 1EFF : 001-049, 051-062, 101-105, 151-152, 1 27-21-43Page 406 1201-205, 1May 01/05 1 1 1CES 1
Component Location
Figure 402A/TASK 27-21-43-991-004-A
R 1EFF : 063-099, 106-149, 153-199, 206-299, 1 27-21-43Page 407 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1
Rack Assembly Figure 403/TASK 27-21-43-991-005
1EFF : 1 1R 1CES ALL 1 11 1 27-21-43 Page 408 May 01/00
Subtask 27-21-43-020-055
A. Removal of the Pedal Position Adjuster Assembly
(1)
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱2(22)
