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_
 - replace the P/BSW-TAKEOVER & PRIORITY, CAPT (8CE1) (Ref. AMM TASK 27-92-41-000-011) and (Ref. AMM TASK 27-92-41-400-011).
 a If the fault continues:
_
 - do a check and repair the wiring from the pushbutton switch (8CE1) pins 5, 6, 7, 8 to the first terminal block (Ref. ASM 27-92/17).
 (b) If the tests do not give a maintenance message:
 - replace the P/BSW-TAKEOVER & PRIORITY, F/O (8CE2) (Ref. AMM TASK 27-92-41-000-011) and (Ref. AMM TASK 27-92-41-400-011).
 1 If the fault continues:
_
 - do a check and repair the wiring from the pushbutton switch (8CE2) pins 5, 6, 7, 8 to the first terminal block (Ref. ASM 27-92/17).
 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 ∞∞27-92-00∞∞∞∞∞∞∞∞∞∞Page 228
 Aug 01/98R
 CES

R TASK 27-92-00-810-834

R  Unwanted Side Stick Indication on Primary Flight Display 
R  1. Possible Causes_______________ 
R  - LGCIU-1 (5GA1) 
R  - DMC-1 (1WT1) 
R  - LGCIU-2 (5GA2) 
R  - DMC-2 (1WT2) 
R  - wiring 
R  2. Job Set-up Information______________________ 
R  A. Referenced Information 
R  -------------------------------------------------------------------------------
R  REFERENCE  DESIGNATION 
R  -------------------------------------------------------------------------------

R  AMM 31-63-34-000-001  Removal of the DMC (1WT1,1WT2,1WT3) 
R  AMM 31-63-34-400-001  Installation of the DMC (1WT1,1WT2,1WT3) 
R  AMM 32-31-71-000-001  Removal of the LGCIU (5GA1, 5GA2) 
R  AMM 32-31-71-400-001  Installation of the LGCIU (5GA1, 5GA2) 
R  ASM 32-62/01 
R  ASM 32-62/02 
R  3. Fault Confirmation__________________ 
R  A. Test 

R (1) Not applicable, you cannot confirm this fault on ground.
R 4. Fault Isolation
_______________
R A. If the side stick indication is shown in flight on CAPT PFD:
R - replace the LGCIU-1 (5GA1) (Ref. AMM TASK 32-31-71-000-001) and (Ref.
R AMM TASK 32-31-71-400-001).

R (1) If the fault continues:
R - do a check and repair the wiring between LGCIU1 pin AB 2F and DMC1
R pin AB 2J (Ref. ASM 32-62/01).

R (2) If the fault continues:
R - replace the DMC-1 (1WT1) (Ref. AMM TASK 31-63-34-000-001) and (Ref.
R AMM TASK 31-63-34-400-001).

 「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 : ALL ∞∞27-92-00∞∞∞∞∞∞∞∞∞∞Page 229
 Nov 01/99 CES

R  B. If the side stick indication is shown in flight on F/O PFD: 
R  - replace the LGCIU-2 (5GA2) (Ref. AMM TASK 32-31-71-000-001) and (Ref. 
R  AMM TASK 32-31-71-400-001). 
R  (1) If the fault continues: 
R  - do a check and repair the LGCIU2 between wiring pin AB 2F and DMC2 
R  pin AB 2J (Ref. ASM 32-62/02). 
R  (2) If the fault continues: 
R  - replace the DMC-2 (1WT2) (Ref. AMM TASK 31-63-34-000-001) and (Ref. 
R  AMM TASK 31-63-34-400-001).

R **ON A/C 301-399,

R TASK 27-92-00-810-835 R Loss of the FCDC DGI 10 Bus R 1. Possible Causes
_______________ R - wiring of the DGI 10 signal from the FCDC to the first terminal block R 2. Job Set-up Information
______________________
R A. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R AMM 27-95-34-000-001 Removal of the FCDC (3CE1,3CE2)
R AMM 27-95-34-400-001 Installation of the FCDC (3CE1,3CE2)
R AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning)

R 3. Fault Confirmation

__________________ R A. Test R (1) Do the BITE test of the EFCS (ground scanning) (Ref. AMM TASK 27-96-
R 00-740-001). R 4. Fault Isolation
_______________
R A. If the test confirm the fault:
R - replace the FCDC (3CE1 or 3CE2) related to the maintenance message
R (Ref. AMM TASK 27-95-34-000-001) and (Ref. AMM TASK 27-95-34-400-001).

R (1) If the fault continues:
R - do a check of the wiring of the DGI 10 signal from the FCDC to the
R first terminal block related to the maintenance message.

R B. Do the test given in para. 3.
　
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