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|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | binding) | | | | | | | | | (Ref. TASK 78-31-00-710-042). | | | | | | ------------------------------------------------------------------------------- INSPECTION AFTER LIGHTNING STRIKE - INSPECTION/CHECK
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TASK 05-51-18-200-001
Inspection after Lightning Strike
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
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START A TASK ON OR NEAR:
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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
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After a lightning strike, before the aircraft continues in service, you must:
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do a general inspection of the total surface of the aircraft to find the strike areas,
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do a careful inspection of the strike areas to find the type and quantity of possible damage
-if you find damage, make a decision about the necessary repair/action.
NOTE : To do this inspection, you must have:
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-a set of access platforms, 2 m (6.56 ft.) to 11 m (36.1 ft.)
R - or an adjustable access platform, 2 m (6.56 ft.) to 11 m (36.1 ft.) - or a manlift aerial boom, 2 m (6.56 ft.) to 11 m (36.1 ft.)
2. Job Set-up Information
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A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notices
No specific adjustable access platform 11 m (36 ft. 1 in.)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
23-11-00-710-001 23-12-00-710-001 23-61-00-200-001
24-22-51-200-001
24-41-00-862-002
25-65-00-740-001
27-14-00-710-001
27-14-51-000-001 27-14-51-400-001 27-24-00-710-001 27-24-51-000-001
27-24-51-400-001
27-34-00-710-001
27-34-51-000-001 27-34-51-400-001 27-44-00-710-001
27-50-00-866-008 27-54-00-710-001 27-60-00-866-002 27-64-00-710-001 27-80-00-866-004 27-84-00-710-001 29-00-00-864-001
30-31-00-710-001 30-42-00-710-001
30-71-00-710-001
R 30-81-00-710-001 32-00-00-481-001
32-11-00-200-001 Operational Test of the HF SystemOperational Test of the VHF System
-Check Resistance of Tip to Retainer - Check Bonding of Retainer to StructureCheck of the Lightning Protection Modules (19XU1, 19XU2)De-energize the Aircraft Electrical Circuits Supplied from the External PowerEmergency Locator Transmitter (ELT) System - BITE TestOperational Test of the Aileron and Hydraulic ActuationRemoval of the Aileron Servo ControlInstallation of the Aileron Servo ControlOperational Test of the Rudder Hydraulic ActuationRemoval of the Rudder Servo Control 1025GM/2025GM/3025GMInstallation of the Rudder Servo Control 1025GM/2025GM/3025GMOperational Test of the Elevator and Hydraulic ActuationRemoval of the Elevator Servo ControlInstallation of the Elevator Servo ControlOperational Test of the Jamming Protection Device of the Trimmable Horizontal Stabilizer ActuatorExtension of the Flaps on the GroundOperational Test of the Flap SystemExtension-Retraction of the Spoilers for MaintenanceOperational Test of the Spoiler Hydraulic ActuationExtending the Slats on the GroundOperational Test of the Slat SystemPut the Related Hydraulic System in the Depressurized Configuration before Maintenance ActionOperational Test of the Probe Ice ProtectionOperational Test of the Windshield Anti-Icing and DefoggingOperational Test of the Drainmast Ice Protection Operational Test of the Ice Detection SystemInstallation of the Safety Devices on the Landing GearsInspection/Check of the Main Gear
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本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM 時(shí)間限制/維護(hù)檢查 4(49)
