- 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 Failure of the Discrete Links 31-32-00-810-934 Failure of the Digital Links AMM 22-83-34-000-001 Removal of the FMGC (1CA1,1CA2) AMM 22-83-34-400-001 Installation of the FMGC (1CA1,1CA2) AMM 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the
External Power 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) AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning) AMM 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground
Power Supply AMM 29-10-00-864-003 Depressurize the Blue Hydraulic System AMM 29-23-00-863-001 Pressurize the Green Hydraulic System from the Yellow
Hydraulic System through the PTU with the Electric Pump AMM 29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU AMM 29-24-00-863-001 Pressurize the Yellow Hydraulic System with the
Electric Pump
AMM 29-24-00-864-001 Depressurize the Yellow Hydraulic System
AMM 34-10-00-860-004 IR Alignment Procedure
ASM 22-82/06
ASM 22-85/03
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-105, 151-199, ∞∞27-93-00∞∞∞∞∞∞∞∞∞∞Page B264
201-214, Aug 01/05 CES -------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
ASM 22-86/02
ASM 27-92/44
ASM 27-92/50
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/ELAC1 and FLT CTL/SEC1 pushbutton switches are pushed (on these pushbutton switches, the OFF legend is off).
(4) On the overhead panel 24VU:
- make sure that the FLT CTL/SEC2 and FLT CTL/SEC3 pushbutton switches are pushed (on these pushbutton switches, the OFF and FAULT legends are off).
(5) On the overhead panel 24VU:
- release the FLT CTL/ELAC2 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).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-105, 151-199, ∞∞27-93-00∞∞∞∞∞∞∞∞∞∞Page B265
201-214, Aug 01/05 CES
4. Fault Isolation
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A. If the F/CTL ELAC1 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-1 (2CE1) (Ref. AMM TASK 27-93-34-000-001) and (Ref. AMM TASK 27-93-34-400-001).
(3) If the fault continues:
(a) Do the trouble shooting procedure (Ref. TASK 31-32-00-810-932) related to the DSI 07 and DSI 13 signals of the ELAC1 (2CE1) (Ref. ASM 27-92/44). If you find a defect:
- repair it
- do the test given in Para. 3.
If you do not find any defect, continue the trouble shooting.
(4) If the fault continues:
(a) Do the trouble shooting procedure (Ref. TASK 31-32-00-810-934) related to the DGI 04 Bus of the ELAC1 (2CE1) (Ref. ASM 27-92/50), (Ref. ASM 22-86/02). If you find a defect: 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320 Trouble Shooting Manual 排故手册 飞行操纵 3(79)
