4. Fault Isolation
_______________
A. If the BITE test gives the maintenance message: SEC2 OR OUTPUT TO THS ACTR SERVO MOT3 9CE
- replace the SEC-2 (1CE2), (Ref. AMM TASK 27-94-34-000-001) and (Ref. AMM TASK 27-94-34-400-001).
(1) If the fault continues:
- replace the motor 3 assembly of the pitch trim actuator, (Ref. AMM TASK 27-44-57-000-003) and (Ref. AMM TASK 27-44-57-400-003).
(2) If the fault continues:
- do a check and repair the wiring of the command signal from the THS actuator (9CE) to the SEC 2 (1CE2), (Ref. ASM 27-94/13).
(3) If the fault continues:
- replace the pitch trim actuator, (Ref. AMM TASK 27-44-57-000-001) and (Ref. AMM TASK 27-44-57-400-001).
B. Do the tests given in Para. 3.
「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 ∞∞27-94-00∞∞∞∞∞∞∞∞∞∞Page 279
Feb 01/03R
CES Loss of the ADR 1 Bus 3 for the SEC 1
1. Possible Causes
_______________
- SEC-1 (1CE1)
- wiring of the DGI-06 signal from the SEC 1 (1CE1) to the first terminal block
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
34-11-00-810-861 Different Angle of Attack Value on the three ADIRUs 34-11-00-810-870 Airspeed Discrepancy on the PFD or on the Standby Airspeed Indicator 34-13-00-810-998 Altitude or Airspeed Discrepancy between CAPT PFD and F/O PFD 34-13-81-810-825 Runaway or Drift of One ADR3 Parameter Identified by
the ELACs and the SECs AMM 27-94-34-000-001 Removal of the SEC (1CE1,1CE2,1CE3) AMM 27-94-34-400-001 Installation of the SEC (1CE1,1CE2,1CE3) AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning) ASM 27-92/53
3. Fault Confirmation
__________________
A. Test
(1) Do the BITE test of the EFCS (ground scanning) (Ref. AMM TASK 27-96-00-740-001).
NOTE : If there is an EFCS message which is not related to an ADR
____ FAULT (NAV ADRX FAULT or ADR-STATUS), do not remove the ADIRU; refer to these procedures:
(a) If flight in turbulence:
- (Ref. TASK 34-11-00-810-870).
(b) If the fault continues:
- (Ref. TASK 34-13-00-810-998)
- (Ref. TASK 34-11-00-810-861).
「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 ∞∞27-94-00∞∞∞∞∞∞∞∞∞∞Page 280
Feb 01/03R
CES
4. Fault Isolation
_______________
A. If the BITE test gives the maintenance message: SEC1 OR BUS3 FROM ADR1
- read the Post Flight Report (PFR) for the maintenance messages ADR3 with AFS in IDENT or ADIRU 1/2/3 DISAGREE with the AFS source.
(1) If one of these maintenance messages comes into view on the PFR:
- do this trouble shooting procedure (Ref. TASK 34-13-81-810-825).
(2) If these maintenance messages do not come into view on the PFR:
- replace the SEC-1 (1CE1) (Ref. AMM TASK 27-94-34-000-001) and (Ref. AMM TASK 27-94-34-400-001).
(a) If the fault continues:
- do a check and repair the wiring of the DGI-06 signal from the SEC 1 (1CE1) to the first terminal block COM and MON parts (Ref. ASM 27-92/53).
B. Do the test given in Para. 3.
「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 ∞∞27-94-00∞∞∞∞∞∞∞∞∞∞Page 281
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 飛行操縱 3(111)
