4. Fault Isolation
_______________
A. If the POST FLIGHT REPORT gives the maintenance message:
ELAC 1 AIL ORDER DISAGREE and ELAC 2 AIL ORDER DISAGREE
- replace the ELAC-1 (2CE1) (Ref. AMM TASK 27-93-34-000-001) and (Ref. AMM TASK 27-93-34-400-001).
(1) During the subsequent flight, if the fault occurs again:
- replace the SSTU-ROLL CTL, CAPT (4CE1) (Ref. AMM TASK 27-92-41-000-002) (Ref. AMM TASK 27-92-41-400-002).
(2) During the subsequent flight, if the fault occurs again:
- replace the SSTU-ROLL CTL, F/O (4CE2) (Ref. AMM TASK 27-92-41-000-002) (Ref. AMM TASK 27-92-41-400-002).
「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 ∞∞27-93-00∞∞∞∞∞∞∞∞∞∞Page B290
Aug 01/05R
CES (3) During the subsequent flight, if the fault occurs again:
- Do a visual inspection for quality of the contacts related to these wirings: ANI 1-3 of ELAC 1 and ELAC 2 (COM and MON part), ANI 1-4 of ELAC 1 and ELAC 2 (COM and MON part) (Ref. ASM 27-92/12).
「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 ∞∞27-93-00∞∞∞∞∞∞∞∞∞∞Page B291
Aug 01/05R
CES Disagree between COM and MON Aileron Order Signal in the ELAC1
1. Possible Causes
_______________
- ELAC-1 (2CE1)
- SSTU-ROLL CTL, CAPT (4CE1)
- SSTU-ROLL CTL, F/O (4CE2)
- ANI 1-3 of ELAC-1 and ELAC-2 (COM and MON part)
- ANI 1-4 of ELAC-1 and ELAC-2 (COM and MON part)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 27-92-41-000-002 Removal of the Transducer Units (4CE1,4CE2,4CE3,4CE4) AMM 27-92-41-400-002 Installation of the Transducer Units
(4CE1,4CE2,4CE3,4CE4)
AMM 27-93-34-000-001 Removal of the ELAC (2CE1,2CE2)
AMM 27-93-34-400-001 Installation of the ELAC (2CE1,2CE2)
ASM 27-92/12
3. Fault Confirmation
__________________
A. Test
(1) Not applicable, you cannot confirm this fault on the ground.
4. Fault Isolation
_______________
A. If the post flight report gives the maintenance message:
ELAC1 AIL ORDER DISAGREE
(1) Replace the ELAC-1 (2CE1), (Ref. AMM TASK 27-93-34-000-001) and (Ref. AMM TASK 27-93-34-400-001).
(2) During the subsequent flight, if the fault occurs again:
- replace the SSTU-ROLL CTL, CAPT (4CE1) and the SSTU-ROLL CTL, F/O (4CE2), (Ref. AMM TASK 27-92-41-000-002) and (Ref. AMM TASK 27-92-41-400-002).
(3) During the subsequent flight, if the fault occurs again:
- do a visual inspection for quality of the contacts related to these wirings: ANI 1-3 of ELAC-1 and ELAC-2 (COM and MON part), ANI 1-4 of ELAC-1 and ELAC-2 (COM and MON part) (Ref. ASM 27-92/12).
「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 ∞∞27-93-00∞∞∞∞∞∞∞∞∞∞Page B292
Aug 01/05R CES
SEC SYSTEM (SPOILER AND ELEVATOR COMPUTER) - FAULT ISOLATION PROCEDURES
_______________________________________________________________________
TASK 27-94-00-810-801
Loss of the Roll Signal on the CAPT Side Stick for the SEC 1
1. Possible Causes
_______________
- SEC-1 (1CE1)
- SSTU-ROLL CTL, CAPT (4CE1)
- wiring from the SEC 1 (1CE1) to the SSTU (4CE1)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 27-92-41-000-002 Removal of the Transducer Units (4CE1,4CE2,4CE3,4CE4) AMM 27-92-41-400-002 Installation of the Transducer Units
(4CE1,4CE2,4CE3,4CE4)
AMM 27-94-34-000-001 Removal of the SEC (1CE1,1CE2,1CE3)
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 飛行操縱 3(89)
