(2) If you can get access to the SFCC menu, and FLP class 3 faults, the fault has gone. The system is also serviceable if "PIN PROGRAM DISAGREE INSTALLATION" is shown in class 3 faults, no further action is required. The fault has gone but it has been recorded.
(3) If you cannot get access to the SFCC menu, do the fault isolation procedure.
4. Fault Isolation
_______________
A. Procedure
(1) If the message "pin prog disagree" is shown, go to Para. (3).
(2) If the message "pin prog disagree flp" is shown, go to Para. (4). NOTE : If the message "pin prog disagree slt" is shown, go to the
____ procedure (Ref. TASK 27-81-00-810-833).
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NOTE : During this procedure when you interchange, remove or install
____ an SFCC, the AMM procedures (Ref. AMM TASK 27-51-34-000-001) and (Ref. AMM TASK 27-51-34-400-001) must be used.
(3) If you cannot get access to the SFCC menu and the message "pin prog disagree" is shown:
(a) Interchange the SFCC's and try to access the SFCC menu of the two SFCC's, Ref. Para. 3. A. (1).
(b) If the fault moves to the other SFCC position: 1 Put the SFCC's back in their initial position.
_
2 Replace the SFCC-1 (21CV) or SFCC-2 (22CV) that has the fault.
_
3 Do the test in Para. 3. A. (1).
_
(c) If the fault does not move to the other SFCC position: 1 Put the SFCC's back in their initial positon.
_ 2 Do a check of the aircraft wiring at the SFCC flap channel
_
(Ref. ASM 275108S01).
3 Repair any defect found.
_
4 Do the test in Para. 3. A. (1).
_
(4) If the message "pin prog disagree flp" is shown:
(a) Interchange the SFCC's.
(b) Do the test in Para. 3. A. (1).
(c) If the fault moves to the other SFCC position: 1 Put the SFCC's back in their initial position.
_
2 Replace the SFCC that has the fault.
_
3 Do the test in Para. 3. A. (1).
_
(d) If the fault does not move to the other SFCC position: 1 Put the SFCC's back in their initial position.
_
2 Do a check of the aircraft wiring, Ref. Para. (3) (c)2_.
_
3 Repair any defect found.
_
4 Do the test in Para. 3. A. (1).
_
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Standard of SFCC-1 and SFCC-2 Does Not Agree With Aicraft Type
1. Possible Causes
_______________
- SFCC-1 (21CV)
- SFCC-2 (22CV)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 27-51-34-000-001 Removal of the SFCC (21CV,22CV)
AMM 27-51-34-400-001 Installation of the SFCC (21CV,22CV)
AMM 31-32-00-860-001 Procedure to Get Access to the SYSTEM REPORT/TEST
Menu Page
3. Fault Confirmation
__________________ R **ON A/C 001-049, 051-099, 101-149, 201-299,
A. Procedure
(1) Get access to the Flight Controls (F/CTL) SYSTEM REPORT/TEST page (Ref. AMM TASK 31-32-00-860-001).
(2) Do a check of the Part Numbers (P/N) of the SFCC-1 (21CV) and the SFCC-2 (22CV):
(a) Push in the line key adjacent to SFCC-1.
(b) Push in the line key adjacent to LRU IDENT.
(c) Record the manufacturers P/N of the SFCC-1.
(d) Push in the line key adjacent to RETURN.
(e) Do steps (a) to (c) for the SFCC-2.
(f) Push in the line key adjacent to RETURN until the F/CTL SYSTEM REPORT/TEST page is shown.
(3) Compare the P/Ns of the SFCC-1 and the SFCC-2 with the permitted interchangeability given in the IPC and the permitted mixability given in the SIL 27-116:
- if the mix of SFCC P/Ns does not agree with those permitted, do the fault isolation procedure in Para 4.A.
R **ON A/C 151-199, 401-499,
A. Procedure
(1) Get access to the Flight Controls (F/CTL) SYSTEM REPORT/TEST page (Ref. AMM TASK 31-32-00-860-001).
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 飛行操縱 2(14)
