-
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
__________________
The manual extension of the flaps.
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 pneumatic right-angle wrench No specific safety barriers No specific warning notice No specific access platform 2.5 m (8 ft. 2 in.) 460005835 2 GROUND LOCK SLEEVE 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER 98D27804001000 1 ADAPTOR-DRIVE, SLAT (AND FLAP) 98D27804011000 1 BAR-TURNING
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B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External
Power 27-50-00-866-009 Retraction of the Flaps on the Ground 27-54-45-000-002 Removal of the Torque Shaft 6204CM(6254CM) 31-32-00-860-006 Procedure to Get Access to the SYSTEM REPORT/TEST
F/CTL Page 32-12-00-010-001 Open the Main Gear Doors for Access 27-50-00-991-005 Fig. 201
3. Job Set-up
__________
Subtask 27-50-00-941-060
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Put a warning notice in position on the panel 114VU to tell persons not to operate the flap/slat controls.
Subtask 27-50-00-860-061
B. Aircraft Maintenance Configuration
(1)
Make sure that the flaps are fully retracted (Ref. TASK 27-50-00-866-009).
(2)
Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER on the flap/slat control lever on panel 114VU.
(3)
Energize the ground service network
(Ref. TASK 24-42-00-861-001).
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(4) On the MCDU:
(a) Get access to the SYSTEM REPORT/TEST F/CTL page (Ref. TASK 31-32-00-860-006).
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the MCDU: On the MCDU:
-push the line key for <SFCC1(2) - the MCDU shows the SFCC1(2) menu page
1.
2. Push the NEXT PAGE button - the MCDU shows the SFCC1(2) menu page
2.
3.
Push the line key (2R) SYSTEM - the MCDU shows the flap SYSTEM DATA DATA FLP> submenu.
4.
Push the line key (1L) <PPU - the MCDU shows the PPU DATA page(s).
5.
Record the APPU data. Subtask 27-50-00-865-065
C. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/WTB/FLP/SYS2 12CV P20 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21 122VU FLIGHT CONTROLS/WTB/FLP/SYS1 10CV S07
Subtask 27-50-00-010-052
D. Get Access
(1)
Open the applicable MLG door (Ref. TASK 32-12-00-010-001).
(2)
Install the GROUND LOCK SLEEVE on the applicable main gear door actuator.
(3)
Put the access platform in position below the torque shaft assy 6204CM (6254CM) in the MLG bay.
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(4) Remove the torque shaft assy 6204CM (6254CM) (Ref. TASK 27-54-45-000-
002).
4. Procedure
_________ (Ref. Fig. 201/TASK 27-50-00-991-005) Subtask 27-50-00-866-057
A. Manual Extension of the Flaps with Pneumatic Wrench WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
(1)
Install the ADAPTOR-DRIVE, SLAT (AND FLAP) (98D27804001000) on the right angle gearbox 6203CM (6253CM).
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