- do a check and repair the wiring of the ground signal at RUD TRIM/RESET pushbutton switch (8CC) (from pin 6 to the first terminal block) (Ref. ASM 22-68/03).
C. If the two tests give the maintenance message AFS : FAC2/RT RESET SW 8CC:
- do a check and repair the wiring of the ground signal from the ground point to the first terminal block (Ref. ASM 22-68/03).
D. 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 ∞∞22-62-00∞∞∞∞∞∞∞∞∞∞Page 228
May 01/98R
CES RUD TRIM/RESET Pushbutton Switch Inoperative on the FAC 1
1. Possible Causes
_______________
- P/BSW-RUD TRIM/RESET (8CC)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
22-62-00-810-813 Failure of the Rudder Trim/Reset Circuit of the FAC 1 AMM 22-62-00-710-001 Operational Test of the Rudder Trim Function AMM 22-96-00-710-001 Operational Test of the AFS
3. Fault Confirmation
__________________
A. Test
(1) Do the operational test of the rudder trim function (Ref. AMM TASK 22-62-00-710-001).
(2) Do the operational test of the AFS (Ref. AMM TASK 22-96-00-710-001) with the RUD TRIM/RESET pushbutton switch (8CC) pushed and read the result for the FAC 1.
4. Fault Isolation
_______________
A. If the reset is inoperative after the operational test of the rudder trim function:
(1) If the operational test of the AFS gives the maintenance message AFS:FAC1/RT RESET SW 8CC:
- do the procedure (Ref. TASK 22-62-00-810-813).
(2) If the operational test of the AFS does not give the maintenance message AFS : FAC1/RT RESET SW 8CC:
- replace the P/BSW-RUD TRIM/RESET (8CC).
B. Do the test given in Para. 3.A.(1).
「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 ∞∞22-62-00∞∞∞∞∞∞∞∞∞∞Page 229
May 01/98R CES
RUD TRIM/RESET Pushbutton Switch Inoperative on the FAC 2
1. Possible Causes
_______________
- P/BSW-RUD TRIM/RESET (8CC)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
22-62-00-810-814 Failure of the Rudder Trim/Reset Circuit of the FAC 2 AMM 22-62-00-710-001 Operational Test of the Rudder Trim Function AMM 22-96-00-710-001 Operational Test of the AFS
3. Fault Confirmation
__________________
A. Test
(1) Do the operational test of the rudder trim function (Ref. AMM TASK 22-62-00-710-001).
(2) Do the operational test of the AFS (Ref. AMM TASK 22-96-00-710-001) with the RUD TRIM/RESET pushbutton switch (8CC) pushed and read the result for the FAC 2.
4. Fault Isolation
_______________
A. If the reset is inoperative after the operational test of the rudder trim function:
(1) If the operational test of the AFS gives the maintenance message AFS : FAC2/RT RESET SW 8CC:
- do the procedure (Ref. TASK 22-62-00-810-814).
(2) If the operational test of the AFS does not give the maintenance message AFS : FAC2/RT RESET SW 8CC:
- replace the P/BSW-RUD TRIM/RESET (8CC).
B. Do the test given in Para. 3.A.(1).
「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 ∞∞22-62-00∞∞∞∞∞∞∞∞∞∞Page 230
May 01/98R CES
Failure of the Rudder Trim Indicator
1. Possible Causes
_______________
- IND-RUDDER TRIM (17CC)
- wiring of the 28VDC signal from the circuit breaker (15CC) to the rudder trim indicator (17CC)
- wiring of the ground signal at the rudder trim indicator (17CC)
- C/B-AUTO FLT/RUDDER/TRIM/IND (15CC)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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本文链接地址：A320 Trouble Shooting Manual 排故手册 AUTO FLIGHT 自动飞行1(102)
