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时间:2011-03-28 13:46来源:蓝天飞行翻译 作者:航空
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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)
 ASM 27-92/52

 3. Fault Confirmation
__________________
 A. Do the BITE test of the EFCS (ground scanning) (Ref. AMM TASK 27-96-00-740-001).
 4. Fault Isolation
_______________
 A. If the BITE test gives the maintenance message:
 ELAC1 OR BUS FROM ELAC2

 - replace the ELAC-1 (2CE1) (Ref. AMM TASK 27-93-34-000-001) and (Ref. AMM TASK 27-93-34-400-001).
 (1) 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).

 (2) If the fault continues:

 (a) Do a check of the wiring of the DGO 05 signal from the ELAC 2 (2CE2) COM part to the ELAC 1 (2CE1) (Ref. ASM 27-92/52).

 - if there is no continuity, repair the above wiring

 - if there is continuity, see Para. (b).

 

 (b) Do a check and repair the wiring of the DGO 05 signal from the ELAC 2 (2CE2) MON part to the ELAC 1 (2CE1) (Ref. ASM 27-92/52).

 


 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞27-93-00∞∞∞∞∞∞∞∞∞∞Page B215
 May 01/04R CES


 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 ∞∞27-93-00∞∞∞∞∞∞∞∞∞∞Page B216
 May 01/04R
 CES  Failure of the ELAC 2


 1. Possible Causes
_______________
 - ELAC-2 (2CE2)

 - RELAY-ELAC 2 ANN SPLY (40CE2)

 - FCDC-1 (3CE1)

 - FCDC-2 (3CE2)

 - ELAC-1 (2CE1)

 - SSTU-ROLL CTL, CAPT (4CE1)

 - SSTU-ROLL CTL, F/O (4CE2)

 - wiring of the RLY ELAC FAULT signal from the relay to the ELAC 2

 - wiring of the RLY ELAC FAULT signal from the relay to the ELAC 2.

 - wiring of the DSI 4/2 (ELAC2 FAILED) signals

 - wiring of the DGO 01 signal

 - wiring of the DGO 04 signal

 - wiring of the DGO 05 signal

 - wiring of the DGI 04 signal

 - wiring of the DGI 05 signal

 - wiring of the DSO 06 signal

 - wiring of the ELAC DECONNECTED IN THE RACK signal

 - wiring of the DSI 07 signal

 - wiring of the DSI 10 signal

 - wiring of the DSI 13 signal

 - wiring of the DSI 17 signal

 - wiring of the PIN PROGRAM ELAC2 signal

 - wiring of the PWR SPLY + 28VDC signal

 - wiring of the PWR SPLY GND signal

 - wiring of the CTL + 28VDC and ELAC2 ENGAGED (DSI 50) signals

 - wiring from the pushbutton switch (6CE2) pin A/C3 to the first terminal block

 - P/BSW-FLT CTL/ELAC 2 (6CE2)


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R 27-93-00-810-947 False ELAC Warning due to Faulty Yellow Hydraulic
R Pressure Switch
 31-32-00-810-932 Failure of the Discrete Links
 31-32-00-810-934 Failure of the Digital Links
 IPC 27920802
 IPC 27920803
 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)
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞27-93-00∞∞∞∞∞∞∞∞∞∞Page B217
 Aug 01/05 CES -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------


AMM  27-92-41-400-002 
AMM  27-93-00-710-001 
AMM  27-93-34-000-001 
AMM  27-93-34-400-001 
AMM  27-95-34-000-001 
AMM  27-95-34-400-001 
AMM  27-96-00-740-001 
ASM  27-92/02
 ASM  27-92/03
 ASM  27-92/40
 ASM  27-92/44
 ASM  27-92/49
 ASM  27-92/50
 ASM  27-92/52
 ASM  27-95/04
 ASM  27-95/05


 
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