(1) If the fault continues:
- do a check and repair the wiring from the upper release strike 30MQ 2/B to A/T COCKPIT SYST.CONTROL. (24MQ) (Ref. ASM 52-51/01).
(2) If the fault continues:
- replace the COCKPIT SYST.CONTROL. (24MQ).
B. If the FAULT lamp of the indication light 22MQ at the COCKPIT DOOR panel 119VU and STRIKE MID LED at the CKPT CONT panel 20VU are on:
- replace the ELECTRICAL STRIKE CTR. (31MQ) (Ref. AMM TASK 52-51-12-000-001) and (Ref. AMM TASK 52-51-12-400-001).
(1) If the fault continues:
- do a check and repair the wiring from the center release strike 31MQ 2/B to A/N COCKPIT SYST.CONTROL. (24MQ) (Ref. ASM 52-51/01).
(2) If the fault continues:
- replace the COCKPIT SYST.CONTROL. (24MQ).
C. If the FAULT lamp of the indication light 22MQ at the COCKPIT DOOR panel 119VU and STRIKE BOT LED at the CKPT CONT panel 20VU are on:
- replace the ELECTRICAL STRIKE (32MQ) (Ref. AMM TASK 52-51-12-000-001) and (Ref. AMM TASK 52-51-12-400-001).
(1) If the fault continues:
- do a check and repair the wiring from the lower release strike 32MQ 2/B to A/U COCKPIT SYST.CONTROL. (24MQ) (Ref. ASM 52-51/01).
(2) If the fault continues:
- replace the COCKPIT SYST.CONTROL. (24MQ).
D. If the FAULT lamp of the indication light 22MQ at the COCKPIT DOOR panel 119VU and the CHAN 1 LED at the CKPT CONT panel 20VU are on:
- replace the COCKPIT SYST.CONTROL. (24MQ) (Ref. AMM TASK 52-51-14-000-001) and (Ref. AMM TASK 52-51-14-400-001).
E. If the FAULT lamp of the indication light 22MQ at the COCKPIT DOOR panel 119VU and the CHAN 2 LED at the CKPT CONT panel 20VU are on:
- replace the COCKPIT SYST.CONTROL. (24MQ) (Ref. AMM TASK 52-51-14-000-001) and (Ref. AMM TASK 52-51-14-400-001).
F. 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 ∞∞52-51-00∞∞∞∞∞∞∞∞∞∞Page 202
May 01/04R
CES TASK 52-51-00-810-802
No Buzzer Function after Key Pad Operation
1. Possible Causes
_______________
- KEYPAD (25MQ)
- BUZZER (23MQ)
- CONTROL UNIT-COCKPIT DOOR LOCKING SYSTEM (24MQ)
- EMI filter (P/N 73124-1)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 52-51-00-710-003 Operational Test of the Emergency Access AMM 52-51-13-000-001 Removal of the Buzzer of the Cockpit-Door Locking System AMM 52-51-13-400-001 Installation of the Buzzer of the Cockpit-Door Locking System AMM 52-51-14-000-001 Removal of the Control Unit of the Cockpit-Door Locking System AMM 52-51-14-400-001 Installation of the Control Unit of the Cockpit-Door
Locking System
AMM 52-51-15-000-001 Removal of the Key Pad 25MQ
AMM 52-51-15-400-001 Installation of the Keypad 25MQ
ASM 52-51/01
3. Fault Confirmation
__________________
A. Do the operational test of the emergency access (Ref. AMM TASK 52-51-00-710-003).
4. Fault Isolation
_______________
R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-214,
A. If the buzzer at the cockpit ceiling panel 211HC does not come on:
- enter the emergency entry code and make sure that the green LED at the KEYPAD (25MQ) flashes.
(1) If the green LED at the KEYPAD (25MQ) flashes:
- do a check of 28 VDC at the BUZZER (23MQ).
(a) If there is no 28 VDC:
- do a check for continuity between the BUZZER (23MQ) and the CB(1MQ) (Ref. ASM 52-51/01).
「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 ∞∞52-51-00∞∞∞∞∞∞∞∞∞∞Page 203
May 01/05 CES 1 If there is no continuity:
_
- do a check and repair the wiring between the BUZZER (23MQ) and the CB(1MQ) (Ref. ASM 52-51/01).
2 If there is continuity:
_
- do a check for continuity between the CONTROL UNIT-COCKPIT DOOR LOCKING SYSTEM (24MQ) connector A/C and the BUZZER (23MQ) (Ref. ASM 52-51/01).
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 艙門 DOORS(120)
