D. If the rudder pedals are not locked with AP1 then AP2 engaged:
(1) Replace the SOLENOID-RUDDER ARTF FEEL (16CA) (Ref. AMM TASK 27-23-17-000-001) and (Ref. AMM TASK 27-23-17-400-001).
(2) If the fault continues:
- replace the C/B - AUTO FLT/RUDDER/ARTF/FEEL (14CA) (Ref. IPC 22840801)
(3) If the fault continues:
- do a check and repair the wiring from the circuit breaker (14CA) to the first terminal block, pin 2 to the terminal block 1871VT (Ref. ASM 22-85/01).
「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 : ALL ∞∞27-93-00∞∞∞∞∞∞∞∞∞∞Page B278
Aug 01/05 CES
E. 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 B279
Aug 01/05R
CES Side Stick not Locked in AP Mode
1. Possible Causes
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- SOLENOID-PITCH & ROLL LOCK, CAPT (12CA1)
- SOLENOID-PITCH & ROLL LOCK, F/O (12CA2)
- RELAY-STICK LOCK 1/CAPT (21CA)
- RELAY-STICK LOCK 1/F/O (23CA)
- RELAY-STICK LOCK 2/CAPT (22CA)
- RELAY-STICK LOCK 2/F/O (24CA)
- FMGC-1 (1CA1)
- FMGC-2 (1CA2)
- CAPT side stick assembly
- wiring from the solenoid (12CA1) to the first terminal block
- wiring from the solenoid (12CA1) to the ground
- F/O side stick assembly
- wiring from the solenoid (12CA2) to the first terminal block
- wiring from the solenoid (12CA2) to the ground
- wiring from the relay (21CA) to the first terminal block
- wiring from the relay (23CA) to the first terminal block
- wiring from the relay (22CA) to the first terminal block
- wiring from the relay (24CA) to the first terminal block
- C/B - AUTO FLT/STICK/LOCK (13CA)
- wiring from the circuit breaker (13CA) to the first terminal block
- wiring of the STICK LOCK COM and STICK LOCK MON signals from the FMGC1 to the first terminal block
- wiring of the STICK LOCK COM and STICK LOCK MON signals from the FMGC2 to the first terminal block
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
IPC 22840802
AMM 22-10-00-710-002 Operational Test of Autopilot Disengagement and Locking Devices of the Side Stick Controller and Rudder Pedals
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 27-92-41-000-001 Removal of the Side Stick Assembly 19VU (18VU)
AMM 27-92-41-000-004 Removal of the Solenoid (12CA1,12CA2)
AMM 27-92-41-400-001 Installation of the Side Stick Assembly 19VU (18VU)
AMM 27-92-41-400-004 Installation of the Solenoid (12CA1,12CA2)
ASM 22-84/08
ASM 22-85/01
「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 B280
Aug 01/05R CES
3. Fault Confirmation
__________________
A. Test Do the operational test of autopilot disengagement and locking devices of the side stick controller and rudder pedals (Ref. AMM TASK 22-10-00-710-002).
4. Fault Isolation
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A. Table of the circuit breakers used in this procedure:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
121VU AUTO FLT/STICK/LOCK 13CA N16
B. If the CAPT side stick is not locked with AP1 then AP2 engaged:
(1) Replace the CAPT side stick assembly (Ref. AMM TASK 27-92-41-000-001) and (Ref. AMM TASK 27-92-41-400-001).
(2) If the fault continues:
- replace the SOLENOID-PITCH & ROLL LOCK, CAPT (12CA1) (Ref. AMM TASK 27-92-41-000-004) and (Ref. AMM TASK 27-92-41-400-004).
(3) If the fault continues:
- do a check of the wiring from the solenoid (12CA1) to the first terminal block, pin A/A to the terminal block 1871VT (Ref. ASM 22-85/01)
- do a check and repair the wiring from the solenoid (12CA1) to the ground, pin A/B (Ref. ASM 22-85/01). 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 飛行操縱 3(85)
