1EFF : ALL 1 05-51-42Page 606 1 1 Nov 01/00R 1 1 1CES 1
-------------------------------------------------------------------------------
|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | 1 | 2 | 3 | 4 | 5 | 6 | 7 | 8 | |----|----|---------------------------------------|-----|-----|-----|----|----| | | | | | | | | | | | | (4) For the slats: | | | | | | | | | (Ref. TASK 27-84-00-710-001) | | | | | | | | | | | | | | | | | | (5) For the spoilers: | | | | | | | | | (Ref. TASK 27-64-00-710-001) | | | | | | -------------------------------------------------------------------------------
5. Close-up
________
Subtask 05-51-42-410-050
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Close the nose gear doors (Ref. TASK 32-22-00-410-001).
(3)
Close the main gear doors (Ref. TASK 32-12-00-410-001).
(4)
Remove the access platform(s).
(5)
Remove the warning notice(s).
INSPECTIONS AFTER WORK ON SYSTEM ELECTRICAL INSTALLATION - ADJUSTMENT/TEST
__________________________________________________________________________
TASK 05-51-43-700-001
Inspection after Work on System Electrical Installation
1. Reason for the Job
__________________
To give the list of all the inspections to do after work on the aircraft electrical installation (wiring, connectors, etc.). The purpose of this inspection is not to do a check of all the aircraft functions but to make sure that:
-basic functions of the aircraft systems operate correctly,
-there are no unwanted effects on the main functions of the systems not directly related to the work done.
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
22-10-00-710-002 Operational Test of Autopilot Disengagement and Locking Devices of the Side Stick Controller and Rudder Pedals
22-30-00-710-003 Operational Test of the Engine / Autothrust System Isolation (with AIDS) 22-30-00-720-002 Operational Test of the Engine / Autothrust System Isolation (without AIDS) 22-61-00-710-001 Operational Test of the Rudder Travel Limiting
Function 22-62-00-710-001 Operational Test of the Rudder Trim Function 22-63-00-710-001 Operational Test of the Yaw Damper Function 22-96-00-710-001 Operational Test of the AFS 22-97-00-710-001 Operational Test of the LAND CAT III Capability 24-00-00-710-003 Integrity Test of the Electrical Power 24-24-00-710-001 Operational Test of the Emergency Generation System 24-24-00-710-002 Operational Test of the Emergency Generator Control
Unit (GCU) from Centralized Fault Display System (CFDS) 24-38-00-710-001 Operational Test of the Battery Charge Limiter (BCL), (with the CFDS) 24-41-00-740-002 Operational Test of the Ground power Control Unit (GPCU) R 24-41-00-740-002 Operational Check of GAPCU via CFDS
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
26-12-00-710-001 27-54-00-710-002 27-96-00-710-023 29-00-00-710-001 32-42-00-710-006 32-51-00-710-002 34-10-00-710-007 34-13-00-710-006 34-13-00-740-002 34-13-00-740-003 34-13-00-740-004 34-13-00-740-005 34-14-00-740-001 34-14-00-740-002 34-14-00-740-003 71-00-00-710-001 73-21-60-720-040 73-25-34-710-043 74-00-00-710-043 77-32-34-710-040 78-31-00-710-042
3. Job Set-up
__________
Subtask 05-51-43-869-050
A. Not Applicable
4. Procedure
_________
Subtask 05-51-43-710-051Operational Check of Loop/SquibOperational Test of the Flap and Slat SystemsIntegrity Test of the Flight Control SystemIntegrity Test of the Hydraulic PowerIntegrity Test of the Braking SystemIntegrity Test of the Nose Wheel Steering SystemTest of the Angle of Attack WarningOperational Test of the AOA SENSOR TESTINTERFACE TEST of the ADRSYSTEM TEST of the ADRRead the CFDIU for the ADR CURRENT STATUSRead the CFDIU for the ADR INPUT STATUSInterface Test of the IRRead CFDIU for IR CURRENT STATUSRead CFDIU for IR INPUT STATUSDry Motoring CheckFunctional Test of the Electronic Control Unit (ECU)Operational Test of the Engine Interface UnitOperational Test of the Ignition SystemOperational Check of EVMU through CFDSOperational Test of the Thrust Reverser System
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM 时间限制/维护检查 2(141)
