3. Fault Confirmation
__________________
A. Test Do the Interface test of the ADR (system 1) (Ref. AMM TASK 34-13-00-740-002).
4. Fault Isolation
_______________
A. If the test gives the maintenance message AOA SENSOR1 (3FP1)/ ADIRU1 (1FP1):
- replace the SENSOR-ANGLE OF ATTACK, 1 (3FP1) (Ref. AMM TASK 34-11-19-000-001) and (Ref. AMM TASK 34-11-19-400-001).
(1) If the fault continues:
- replace the ADIRU-1 (1FP1) (Ref. AMM TASK 34-12-34-000-001) and (Ref. AMM TASK 34-12-34-400-001).
(a) If the fault continues:
- do a check and repair the wiring from the angle of attack sensor 1 (3FP1) to the AOA INPUTS 1 and 2 of the ADIRU 1 (1FP1) (Ref. ASM 34-11/02).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞34-13-00∞∞∞∞∞∞∞∞∞∞Page A210
Feb 01/05R CES
R **ON A/C 001-049, 101-105, 151-199, 201-210, 301-399, 401-499,
B. If the test is OK, do a visual inspection of the angle of attack sensors:
(1) If an angle of attack sensor is found damaged:
- replace the angle of attack sensor.
(2) If no external damage is found:
- keep the angle of attack sensor on the aircraft.
(3) If no external damage is found but the message is shown again:
- replace the angle of attack sensor.
(4) Reset the ADIRU (NAV-OFF-NAV) to clear the ECAM message. **ON A/C ALL
C. Do the test given in Para. 3.
Loss of the AOA 2 Input to the ADR 2
1. Possible Causes
_______________
- SENSOR-ANGLE OF ATTACK, 2 (3FP2)
- ADIRU-2 (1FP2)
- wiring from the angle of attack sensor 2 (3FP2) to the AOA INPUTS 1 and 2 of the ADIRU 2 (1FP2)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 34-11-19-000-001 Removal of the Angle of Attack Sensor (3FP1, 3FP2, 3FP3) AMM 34-11-19-400-001 Installation of the Angle of Attack Sensor (3FP1,
3FP2, 3FP3)
AMM 34-12-34-000-001 Removal of the ADIRU (1FP1, 1FP2, 1FP3)
AMM 34-12-34-400-001 Installation of the ADIRU (1FP1, 1FP2, 1FP3)
AMM 34-13-00-740-002 INTERFACE TEST of the ADR
ASM 34-11/02
3. Fault Confirmation
__________________
A. Test Do the Interface test of the ADR (system 2) (Ref. AMM TASK 34-13-00-740-002).
4. Fault Isolation
_______________
A. If the test gives the maintenance message AOA SENSOR2 (3FP2)/ ADIRU2 (1FP2):
- replace the SENSOR-ANGLE OF ATTACK, 2 (3FP2) (Ref. AMM TASK 34-11-19-000-001) and (Ref. AMM TASK 34-11-19-400-001).
(1) If the fault continues:
- replace the ADIRU-2 (1FP2) (Ref. AMM TASK 34-12-34-000-001) and (Ref. AMM TASK 34-12-34-400-001).
(a) If the fault continues:
- do a check and repair the wiring from the angle of attack sensor 2 (3FP2) to the AOA INPUTS 1 and 2 of the ADIRU 2 (1FP2) (Ref. ASM 34-11/02).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞34-13-00∞∞∞∞∞∞∞∞∞∞Page A212
Feb 01/05R CES
R **ON A/C 001-049, 101-105, 151-199, 201-210, 301-399, 401-499,
B. If the test is OK, do a visual inspection of the angle of attack sensors:
(1) If an angle of attack sensor is found damaged:
- replace the angle of attack sensor.
(2) If no external damage is found:
- keep the angle of attack sensor on the aircraft.
(3) If no external damage is found but the message is shown again:
- replace the angle of attack sensor.
(4) Reset the ADIRU (NAV-OFF-NAV) to clear the ECAM message.
**ON A/C ALL
C. Do the test given in Para. 3.
Loss of the AOA 3 Input to the ADR 3
1. Possible Causes
_______________
- SENSOR-ANGLE OF ATTACK, 3 (3FP3)
- ADIRU-3 (1FP3)
- wiring from the angle of attack sensor 3 (3FP3) to the AOA INPUTS 1 and 2 of the ADIRU 3 (1FP3)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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