Failure of the ELAC2 at the AP Engagement
1. Possible Causes
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- FMGC-1 (1CA1)
- ELAC-2 (2CE2)
- FMGC-2 (1CA2)
- SSTU-ROLL CTL, F/O (4CE2)
- SSTU-PITCH CTL, F/O (4CE4)
- SSTU-ROLL CTL, CAPT (4CE1)
- SSTU-PITCH CTL, CAPT (4CE3)
- wiring
2. Job Set-up Information
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A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
31-32-00-810-932
31-32-00-810-934
AMM 22-83-34-000-001
AMM 22-83-34-400-001
AMM 24-41-00-861-002
AMM 27-92-41-000-002
AMM 27-92-41-400-002
AMM 27-93-34-000-001
AMM 27-93-34-400-001
AMM 27-96-00-740-001
AMM 29-10-00-863-003
AMM 29-10-00-864-003
AMM 29-23-00-863-001
AMM 29-23-00-864-001
AMM 29-24-00-863-001
AMM 29-24-00-864-001 AMM 34-10-00-860-004 ASM 22-82/06 ASM 22-85/03 ASM 22-86/02 ASM 27-92/44 ASM 27-92/52Failure of the Discrete LinksFailure of the Digital LinksRemoval of the FMGC (1CA1,1CA2)Installation of the FMGC (1CA1,1CA2)Energize the Aircraft Electrical Circuits from the External PowerRemoval of the Transducer Units (4CE1,4CE2,4CE3,4CE4)Installation of the Transducer Units (4CE1,4CE2,4CE3,4CE4)Removal of the ELAC (2CE1,2CE2)Installation of the ELAC (2CE1,2CE2)BITE Test of the EFCS (Ground Scanning)Pressurize the Blue Hydraulic System with a Ground Power SupplyDepressurize the Blue Hydraulic SystemPressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric PumpDepressurize the Green and Yellow Hydraulic Systems after Operation of the PTUPressurize the Yellow Hydraulic System with the Electric PumpDepressurize the Yellow Hydraulic SystemIR Alignment Procedure
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : 001-049, 051-099, 101-105, 151-199, ∞∞27-93-00∞∞∞∞∞∞∞∞∞∞Page B269
201-214, Aug 01/05R
CES
3. Fault Confirmation
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A. Job Set-Up
(1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(2) On the overhead panel 20VU:
- on the ADIRS CDU, set the OFF/NAV/ATT selector switches to NAV and align the IRs (Ref. AMM TASK 34-10-00-860-004).
(3) On the overhead panel 23VU:
- make sure that the FLT CTL/SEC1 pushbutton switch is pushed (on this pushbutton switch, the OFF legend is off).
(4) On the overhead panel 24VU:
- make sure that the FLT CTL/ELAC2, FLT CTL/SEC2 and FLT CTL/SEC3 pushbutton switches are pushed (on these pushbutton switches, the OFF legends are off).
(5) On the overhead panel 23VU:
- release the FLT CTL/ELAC1 pushbutton switch (on this pushbutton switch, the OFF legend comes on).
(6) Pressurize the aircraft hydraulic systems (Ref. AMM TASK 29-10-00-863-003), (Ref. AMM TASK 29-23-00-863-001), (Ref. AMM TASK 29-24-00-863-001).
B. Test
(1) On the FCU:
- push the AP1 pushbutton switch to engage the AP1
- push the AP2 pushbutton switch to engage the AP2.
(2) Do the BITE test of the EFCS (Ground Scanning) (Ref. AMM TASK 27-96-00-740-001).
(3) Depressurize the aircraft hydraulic systems (Ref. AMM TASK 29-10-00-864-003), (Ref. AMM TASK 29-23-00-864-001), (Ref. AMM TASK 29-24-00-864-001).
4. Fault Isolation
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A. If the F/CTL ELAC2 FAULT warning comes into view 1 second after the AP1 engagement:
(1) Replace the FMGC-1 (1CA1) (Ref. AMM TASK 22-83-34-000-001) and (Ref. AMM TASK 22-83-34-400-001).
(2) If the fault continues:
- replace the ELAC-2 (2CE2) (Ref. AMM TASK 27-93-34-000-001) and (Ref. AMM TASK 27-93-34-400-001).
「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 : 001-049, 051-099, 101-105, 151-199, ∞∞27-93-00∞∞∞∞∞∞∞∞∞∞Page B270
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) 飛行操縱 3(81)
