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|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | 1 | 2 | 3 | 4 | 5 | 6 | 7 | 8 | |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - for the lockstay assembly | | | | | | | | | (Ref. TASK 32-11-17-400-001) | | | | | | | | | - for the side-stay assembly | | | | | | | | | (Ref. TASK 32-11-16-400-001). | | | | | | | | | | | | | | | | C. | | Inspection of the fuselage | | | | | | | | | | | | | | | | | | (1)If damage are found during the | X | | | | | | | | inspections of the landing gears | | | | | | | | | in phase one: | | | | | | | | | (a)Examine the top of the | | X | | | | | | | fuselage, from frame 31 to 35 | | | | | | | | | between stringer 18 LH and | | | | | | | | | 18 RH, for distortion, cracks, | | | | | | | | | pulled or torn fasteners and | | | | | | | | | damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | - tell Airbus Industrie about | | | X | | | | | | the results. | | | | | | -------------------------------------------------------------------------------
5. Close-up
________
Subtask 05-51-41-410-050
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(3)
Close the Main Gears Doors (Ref. TASK 32-12-00-410-001).
(4)
Close the Nose Gear Doors (Ref. TASK 32-22-00-410-001).
INSPECTION AFTER VERY HIGH WINDS ON GROUND - INSPECTION/CHECK
_____________________________________________________________
TASK 05-51-42-200-001
Inspection after Very High Winds on Ground
WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A
_______ FALL CAN INJURE OR KILL YOU.
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.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION
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No specific warning notices
No specific adjustable access platform 11 m (36 ft. 1 in.)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power 27-24-00-710-001 Operational Test of the Rudder Hydraulic Actuation 27-34-00-710-001 Operational Test of the Elevator and Hydraulic
Actuation 27-50-00-866-008 Extension of the Flaps on the Ground 27-54-00-710-001 Operational Test of the Flap System 27-60-00-866-002 Extension-Retraction of the Spoilers for Maintenance 27-64-00-710-001 Operational Test of the Spoiler Hydraulic Actuation 27-80-00-866-004 Extending the Slats on the Ground
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REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-84-00-710-001 Operational Test of the Slat System
29-00-00-864-001 Put the Related Hydraulic System in the Depressurized
Configuration before Maintenance Action
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