(2) If there is a ground signal:
- do the procedure (Ref. TASK 34-11-00-810-868).
「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 ∞∞34-11-00∞∞∞∞∞∞∞∞∞∞Page A258
May 01/05R CES
Erroneous TAT Value Read on the Lower ECAM DU on Ground
1. Possible Causes
_______________
- PHC-2 (6DA2)
- PHC-1 (6DA1)
- wiring between the PHC2 and the ADIRU2
- wiring between the ADIRU1 and the first terminal block
- wiring between the ADIRU3 and the first terminal block
- wiring between the PHC1 and the first terminal block
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 30-31-34-000-002 Removal of the Probe Heat Computer (PHC)
(6DA1,6DA2,6DA3)
AMM 30-31-34-400-002 Installation of the Probe Heat Computer (PHC)
(6DA1,6DA2,6DA3)
ASM 34-13/02
3. Fault Confirmation
__________________
A. Test
Not applicable, the fault is evident.
4. Fault Isolation
_______________
A. If the fault symptom is identified by the crew observation, ADIRS - TAT reading error of 11 deg. C on the lower ECAM DU:
(1) With the AIR DATA selector switch (15FP) and the ECAM/ND XFR selector switch (19WT) in the NORM positions:
- replace the PHC-2 (6DA2) (Ref. AMM TASK 30-31-34-000-002) and (Ref. AMM TASK 30-31-34-400-002).
(a) If the fault continues:
- do a check and repair the wiring between the PHC2 and the ADIRU2 for pin AA/4F of the ADIRU2 (Ref. ASM 34-13/02).
(2) With the AIR DATA selector switch (15FP) in the NORM position and the ECAM/ND XFR selector switch (19WT) in the F/O position:
- do a check and repair the wiring between the ADIRU1 and the first terminal block for pin AA/4F of the ADIRU1 (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 ∞∞34-11-00∞∞∞∞∞∞∞∞∞∞Page A259
May 01/05R CES
(3) With the AIR DATA selector switch (15FP) in the CAPT/3 position and the ECAM/ND XFR selector switch (19WT) in the F/O position:
- do a check and repair the wiring between the ADIRU3 and the first terminal block for pin AA/4F of the ADIRU3 (Ref. ASM 34-13/02).
(4) With the AIR DATA selector switch (15FP) in the NORM and CAPT/3 positions and the ECAM/ND XFR selector switch (19WT) in the F/O position:
- replace the PHC-1 (6DA1) (Ref. AMM TASK 30-31-34-000-002) and (Ref. AMM TASK 30-31-34-400-002).
(a) If the fault continues:
- do a check and repair the wiring between the PHC1 and the first terminal block for pin AA/<A of the PHC1 (Ref. ASM 34-13/02).
AIR DATA - FAULT ISOLATION PROCEDURES
_____________________________________
TASK 34-13-00-810-801 Internal Failure of the ADR 1
1. Possible Causes
_______________
- ADIRU-1 (1FP1)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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
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 ADIRU1 (1FP1):
- replace the ADIRU-1 (1FP1), (Ref. AMM TASK 34-12-34-000-001) and (Ref. AMM TASK 34-12-34-400-001).
「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 201
Feb 01/05R
CES Internal Failure of the ADR 1 Identified by the EIS1
1. Possible Causes
_______________
- ADIRU-1 (1FP1)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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