(2)
Operational test of the engine/autothrust system isolation.
-
With AIDS installed : (Ref. TASK 22-30-00-710-003)
-
With AIDS not installed : (Ref. TASK 22-30-00-720-002)
1EFF : ALL 1 05-51-43Page 502 1 1 Feb 01/05R 1 1 1CES 1
(3)
Operational test of the rudder travel limiting function (Ref. TASK 22-61-00-710-001).
(4)
Operational test of the rudder trim function (Ref. TASK 22-62-00-710-001).
(5)
Operational test of the yaw damper function (Ref. TASK 22-63-00-710-001).
(6)
Operational test of the AFS (Ref. TASK 22-96-00-710-001).
(7)
Operational test of the LAND CAT III capability (Ref. TASK 22-97-00-710-001).
R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-228, 301-302,
Subtask 05-51-43-710-052
B. Do these inspections to make sure that the basic functions of the ELECTRICAL POWER system operate correctly :
(1)
Integrity test of the electrical power (Ref. TASK 24-00-00-710-003).
(2)
Operational test of the emergency generation system (Ref. TASK 24-24-00-710-001).
(3)
Operational test of the Emergency Generator Control Unit (GCU) from Centralized Fault Display System (CFDS) (Ref. TASK 24-24-00-710-002).
(4)
Operational test of the Battery Charge Limiter (BCL), (with the CFDS) (Ref. TASK 24-38-00-710-001).
(5)
Operational test of the Ground Power Control Unit (GPCU) (Ref. TASK 24-41-00-740-002).
R **ON A/C 106-149, 229-299, 303-399, 401-499,
Subtask 05-51-43-710-052-A
B. Do these inspections make sure that the basic functions of the ELECTRICAL POWER system operate correctly :
(1)
Integrity test of the electrical power (Ref. TASK 24-00-00-710-003).
(2)
Operational test of the emergency generation system (Ref. TASK 24-24-00-710-001).
(3)
Operational test of the Emergency Generator Control Unit (GCU) from Centralized Fault Display System (CFDS) (Ref. TASK 24-24-00-710-002).
(4)
Operational test of the Battery Charge Limiter (BCL), (with the CFDS) (Ref. TASK 24-38-00-710-001).
(5)
Operational test of the Ground Auxiliary Power Control Unit (GAPCU) (Ref. TASK 24-41-00-740-002).
**ON A/C ALL
Subtask 05-51-43-710-053
C. Do these inspections to make sure that the basic functions of the FIRE PROTECTION system operate correctly :
(1) Operational test of the engine fire and overheat detection (Ref. TASK 26-12-00-710-001).
Subtask 05-51-43-710-054
D. Do these inspections to make sure that the basic functions of the FLIGHT CONTROLS system operate correctly :
(1)
Operational test of the flap and slat systems (Ref. TASK 27-54-00-710-002).
(2)
Integrity test of the flight control system (Ref. TASK 27-96-00-710-023).
Subtask 05-51-43-710-055
E. Do these inspections to make sure that the basic functions of the
HYDRAULIC POWER system operate correctly :
(1) Integrity test of the hydraulic power (Ref. TASK 29-00-00-710-001). Subtask 05-51-43-710-056
F. Do these inspections to make sure that the basic functions of the LANDING GEAR system operate correctly :
(1)
Integrity test of the braking system (Ref. TASK 32-42-00-710-006).
(2)
Integrity test of the nose wheel steering system (Ref. TASK 32-51-00-710-002).
Subtask 05-51-43-710-057
G. Do these inspections to make sure that the basic functions of the
NAVIGATION system operate correctly :
(1)
Test of the angle of attack warning (Ref. TASK 34-10-00-710-007).
(2)
Operational test of the AOA SENSOR TEST (Ref. TASK 34-13-00-710-006).
(3)
INTERFACE TEST of the ADR (Ref. TASK 34-13-00-740-002).
(4)
SYSTEM TEST of the ADR (Ref. TASK 34-13-00-740-003).
(5)
Read the CFDIU for ADR CURRENT STATUS (Ref. TASK 34-13-00-740-004).
(6)
Read the CFDIU for ADR INPUT STATUS (Ref. TASK 34-13-00-740-005).
(7)
Interface test of the IR (Ref. TASK 34-14-00-740-001).
(8)
Read the CFDIU for IR CURRENT STATUS (Ref. TASK 34-14-00-740-002).
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM 時間限制/維護檢查 4(135)
