6.
Push the line key < RETURN frequently until the CFDS menu page is shown.
7.
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
Subtask 27-84-48-820-050
G. Adjustment After BITE Test
On the MCDU:
-
the MCDU shows the SFCC 1 menu page
1.
-
the MCDU shows the SFCC 1 menu page
2.
-
the MCDU shows the SLAT SYSTEM DATA submenu.
-
the MCDU shows the PPU DATA page(s).
R (1) Compare the APPU and the FPPU angles (deg) with those that were R recorded before the actuator was removed (Ref. TASK 27-84-48-000-R 001). Make sure that: R - at position 0, the APPU/FPPU angles agree by 0.9 deg R R - at positions 1,2,3 and FULL, the APPU/FPPU angles agree by 1.3 deg R - the LH APPU and the RH APPU angles agree by 0.45 deg.
R (2) If the APPU/FPU angles are not in the specified limit:
R R (a) Disconnect the torque shaft outboard of the actuator (Ref. TASK 27-84-48-000-001).
R R (b) Turn the torque shaft in the applicable direction until the APPU and the FPU angles (deg) are in the specified limit.
R R NOTE : A turn of the torque shaft by one spline is equal to 0.11____ deg. of the PPU angle.
R (c) Connect the torque shaft outboard of the actuator (Ref. TASK 27-84-48-400-001).
Subtask 27-84-48-710-050
H. Test
(1) Do the operational test of the slat power-transmission system (Ref. TASK 27-84-00-710-001).
5. Close-up________
Subtask 27-84-48-942-050
A. Removal of Equipment
(1) Make sure that the work area is clean and clear of tool(s) and other items.
(2) Remove the safety barriers.
(3) Remove the warning notice(s).
(4) Remove the access platform(s).
(5) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
ACTUATOR ASSY - TYPE B (6027CM,6029CM,6033CM,6035CM,6037CM,6039CM,6041CM,
_________________________________________________________________________ 6045CM,6077CM,6079CM,6083CM,6085CM,6087CM,6089CM...) - REMOVAL/INSTALLATION
___________________________________________________________________________
TASK 27-84-49-000-001
Removal of the Type B Actuators 6027CM(6077CM)/6029CM(6079CM)/6035CM
(6085CM)/6039CM(6089CM)/6045CM(6095CM)
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 GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
No specific safety barriers
No specific warning notice(s)
No specific adjustable access platform 3.6 m (11 ft. 10 in.)
R 98D27504030001 2 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT R 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER 98D27804007000 2 TOOL-ALIGNMENT AND LOCKING (SLAT TRACKS 5 TO 12)
B. 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
27-50-00-400-003 27-80-00-866-005 27-84-45-000-006 27-84-45-000-007 27-84-45-000-012 27-84-45-000-013 27-84-48-400-001 31-32-00-860-006 Installation of the Lock-Torque Shaft - Flaps and Slats (98D27504030001)Retracting the Slats on the GroundRemoval of the Torque Shafts 6014CM(6064CM)/6028CM(6078CM)/6036CM(6086CM)/ 6038CM(6088CM)/6040CM(6090CM)/6042CM(6092CM)/6044CM(6 094CM)Removal of the Torque Shafts 6016CM(6066CM)/6020CM(6070CM)/6026CM(6076CM)/ 6030CM(6080CM)Removal of the Torque Shaft 6034CM(6084CM)Removal of the Torque Shaft 6046CM(6096CM)Installation of the Type A Actuators 6013CM(6063CM)/6015CM(6065CM)Procedure to Get Access to the SYSTEM REPORT/TEST F/CTL Page
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱8(22)
