-
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.
CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
_______
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
-MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
1. Reason for the Job
__________________
Refer to the MPD TASK: 577001-02
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R No specific circuit breaker(s) safety clip(s) No specific safety barriers No specific warning notices No specific access platform 3.8 m (12 ft. 6 in.) No specific access platform 3 m (9 ft. 10 in.)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R 27-50-00-866-008 27-50-00-866-009 27-60-00-866-002 27-64-41-000-001 27-64-41-400-001 NTM 57-70-01 PART 6 ASRM 577000 57-71-00-991-005 Extension of the Flaps on the GroundRetraction of the Flaps on the GroundExtension-Retraction of the Spoilers for MaintenanceRemoval of the Spoiler 1Installation of the Spoiler 1 (for corrective action)Fig. 605
3. Job Set-up__________
Subtask 57-71-00-941-053
A. Safety Precautions
(1) Put the safety barriers in position.
(2) Put warning notices in the cockpit to tell persons not to operate the spoilers.
(3) Put warning notices in the cockpit to tell persons not to operate the flaps or slats.
R R (4) Put the access platform below the applicable wing at spoiler 1, zone 580(680).
Subtask 57-71-00-860-054
B. Aircraft Maintenance Configuration
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) Fully extend the spoiler 1 (Ref. TASK 27-60-00-866-002).
(2) Fully extend the flaps (Ref. TASK 27-50-00-866-008).
R (3) Make sure that the COLLAR-SAFETY, SPOILER is installed on the spoiler actuator.
R (4) Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is installed on the flap/slat control lever on the panel 114VU.
Subtask 57-71-00-865-055
R C. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 105VU FLT CTL/SEC1/STBY SPLY 22CE B01 121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18
Subtask 57-71-00-010-052
D. Get Access
(1) Put the access platform in position below the zone 582(682).
(2) Remove the actuator hinge-pin (Ref. TASK 27-64-41-000-001).
4. Procedure_________
(Ref. Fig. 605/TASK 57-71-00-991-005)
CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING_______ EDGE: - DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS. - DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS. - MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
Subtask 57-71-00-220-050
R A. Inspection
R R (1) Do a special detailed inspection of the actuator bracket on spoiler 1 (Ref. NTM 57-70-01 PART 6).
R R R R NOTE : If necessary, refer to the ASRM (Ref. ASRM 577000) for the____ correct repair procedure. If the defect is not included in this repair, you must request a procedure from Airbus Industrie.
Actuator Bracket - Spoiler 1 - Inspection Area
Figure 605/TASK 57-71-00-991-005
1EFF : ALL 1 57-71-00 Page 624
1 1 Feb 01/98
1 1
1CES 1
5. Close-up________
Subtask 57-71-00-410-052
A. Close Access
(1) Install the actuator hinge-pin (Ref. TASK 27-64-41-400-001).
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