-
THE FLIGHT CONTROLS
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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 blanking caps
No specific circuit breaker(s) safety clip(s)
No specific warning notices
No specific adjustable access platform 6.0 m (19 ft. 8 in.)
98D27207547000 1 PIN - RIGGING
R 98D27207548000 1 PIN - RIGGING
B. Referenced Information
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REFERENCE DESIGNATION
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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 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action 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
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R R 53-55-12-000-001 55-33-13-010-002 27-23-17-991-002 27-23-17-991-001
3. Job Set-up__________
Subtask 27-23-17-861-050
Removal of the Rudder Fairings 325AL and 325AR Opening/Removal of the Trailing Edge Access-Panels 325EL, 325ER, 325DL, 325DR, 325CL, 325CR, 325BL and 325BRFig. 401Fig. 402
A. Energize the aircraft electrical circuits. (Ref. TASK 24-41-00-861-002)
Subtask 27-23-17-865-053
B. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AUTO FLT/FAC1/28VDC 5CC1 B04 49VU AUTO FLT/FAC1/26VAC 14CC1 B03 121VU AUTO FLT/RUDDER/TRIM/IND 15CC M20 121VU AUTO FLT/FAC2/28VDC 5CC2 M19 121VU AUTO FLT/FAC2/26VAC 14CC2 M18
Subtask 27-23-17-860-051
C. Aircraft Maintenance Configuration
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES
_______ ARE CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
(1)
Pressurize the Blue hydraulic system with the electric pump. (Ref. TASK 29-10-00-863-003)
(2)
Put the rudder pedals in the neutral position.
(3)
On the center pedestal, on the panel 110VU, make sure that the RUD TRIM indicator shows 0.
(4) On the overhead panel 23VU, release the FLT CTL/FAC 1 pushbutton switch. The OFF legend comes on.
(5) On the overhead panel 24VU, release the FLT CTL/FAC 2 pushbutton switch. The OFF legend comes on.
(6) Put warning notices in the flight compartment to tell persons not to operate the flight controls.
(7) Depressurize the Blue hydraulic system (Ref. TASK 29-10-00-864-003) .
Subtask 27-23-17-865-050
D. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AUTO FLT/FAC1/28VDC 5CC1 B04 49VU AUTO FLT/FAC1/26VAC 14CC1 B03 121VU AUTO FLT/RUDDER/TRIM/IND 15CC M20 121VU AUTO FLT/FAC2/28VDC 5CC2 M19 121VU AUTO FLT/FAC2/26VAC 14CC2 M18
Subtask 27-23-17-860-050
E. Aircraft Maintenance Configuration
(1) Make sure that the hydraulic systems are depressurized and put them in the maintenance configuration. (Ref. TASK 29-00-00-864-001)
(2) De-energize the aircraft electrical circuits. (Ref. TASK 24-41-00-862-002)
(3) Put warning notices in position to tell persons not to operate the Green, the Yellow and the Blue hydraulic systems.
R Subtask 27-23-17-010-050-A
R F. Get Access
R (1) Put the adjustable access platform in position.
R (2) Open the access door 312AR.
(3) Open the access panel 325BL at the trailing edge of the vertical stabilizer (1) (Ref. TASK 55-33-13-010-002). 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵2(101)
