- repair the above wiring
- install the ADIRU2 (Ref. AMM TASK 34-12-34-400-001)
- install the ADIRS CDU (Ref. AMM TASK 34-12-12-400-001).
(b) If there is no short to ground:
- install a new ADIRS CDU
- install the ADIRU2.
1 If the fault continues:
_
- replace the ADIRU2. R
5. Close-up
________
A. Do the ADIRS stop procedure (Ref. AMM TASK 34-10-00-860-005).
1. Possible Causes
Only the NAV ADR3 FAULT ECAM Warning is shown in the POST FLIGHT REPORT (PFR) _______________
- ADIRU-3 (1FP3)
- CDU-ADIRS (2FP)
- wiring between the ADIRS CDU (2FP) and the ADIRU3 (1FP3)
2. Job Set-up Information______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R
R AMM 34-10-00-860-005 ADIRS Stop Procedure
R AMM 34-12-12-000-001 AMM 34-12-12-400-001 AMM 34-12-34-000-001 AMM 34-12-34-400-001 ASM 34-13/02 Removal of the ADIRS CDU (2FP)Installation of the ADIRS CDU (2FP)Removal of the ADIRU (1FP1, 1FP2, 1FP3)Installation of the ADIRU (1FP1, 1FP2, 1FP3)
3. Fault Confirmation__________________
A. Test
(1) Not applicable, you cannot confirm this fault on the ground.
4. Fault Isolation
_______________
R
A. If the POST FLIGHT REPORT gives the NAV ADR3 FAULT ECAM warning:
- do a check of the status of the ADR3 pushbutton switch on the ADIRS CDU.
(1) If the pilot pushed the ADR3 pushbutton switch during the flight:
- no maintenance action is necessary.
(2) If the pilot did not push the ADR3 pushbutton switch during the flight:
- remove the ADIRU-3 (1FP3) (Ref. AMM TASK 34-12-34-000-001)
- remove the CDU-ADIRS (2FP) (Ref. AMM TASK 34-12-12-000-001)
- do a check for a short to ground on the wiring between the ADIRS CDU (2FP) and the ADIRU3 (1FP3) between pin C/9 of the ADIRS CDU and pin AA/4C of the ADIRU3 (Ref. ASM 34-13/02).
「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 ∞∞34-13-81∞∞∞∞∞∞∞∞∞∞Page 222
Nov 01/00 CES
(a) If there is a short to ground:
- repair the above wiring
- install the ADIRU3 (Ref. AMM TASK 34-12-34-400-001)
- install the ADIRS CDU (Ref. AMM TASK 34-12-12-400-001).
(b) If there is no short to ground:
- install a new ADIRS CDU
- install the ADIRU3.
1 If the fault continues:
_
- replace the ADIRU3. R
5. Close-up
________
A. Do the ADIRS stop procedure (Ref. AMM TASK 34-10-00-860-005).
Different True Airspeed Indication between CAPT ND and F/O ND
1. Possible Causes
_______________
- SENSOR-TAT, 1 (11FP1)
- SENSOR-TAT, 2 (11FP2)
- ADIRU-1 (1FP1)
- ADIRU-2 (1FP2)
- ADIRU-3 (1FP3)
- aircraft wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
34-13-00-810-998 Altitude or Airspeed Discrepancy between CAPT PFD and
F/O PFD AMM 34-11-18-000-001 Removal of the TAT Sensor (11FP1, 11FP2) AMM 34-11-18-400-001 Installation of the TAT Sensor (11FP1, 11FP2) 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 34-13-00-720-009 Functional Test of the Altitude and Airspeed Data ASM 34-11/02
3. Fault Confirmation
__________________
A. Test
Not applicable, you cannot confirm this fault on the ground.
4. Fault Isolation
_______________
A. If the fault symptom is identified by the observation that follows: Different true airspeed indication between CAPT and F/O ND:
- do the functional test of the altitude and airspeed data (Ref. AMM TASK 34-13-00-720-009).
(1) If the test gives a different altitude value and/or a different airspeed value from the ADR1 (compared to the ADR2 and the ADR3), from the ADR2 (compared to the ADR1 and the ADR3) or from the ADR3 (compared to the ADR1 and the ADR2):
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