- release the locking mechanism which is inside the blocked door
- replace the avionics compartment left door (Ref. AMM TASK 52-41-12-000-001) and (Ref. AMM TASK 52-41-12-400-001).
TASK 52-41-00-810-819
Impossibility to Open the Right Avionics Compartment Door
1. Possible Causes
_______________
- avionics compartment right door
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 52-41-13-000-001 Removal of the Avionics-Compartment Lateral-Right Door AMM 52-41-13-400-001 Installation of the Avionics-Compartment Lateral-Right Door
3. Fault Confirmation
__________________
A. Job Set-up
(1) Put the access platform in position at zone 126.
B. Test
(1) Make sure that you cannot open the right avionics compartment door.
4. Fault Isolation
_______________
A. If the test confirms the fault:
- get access to the avionics compartment by another avionics compartment door
- release the locking mechanism which is inside the blocked door
- replace the avionics compartment right door (Ref. AMM TASK 52-41-13-000-001) and (Ref. AMM TASK 52-41-13-400-001).
TASK 52-41-00-810-820
Impossibility to Open the Aft Avionics Compartment Door
1. Possible Causes
_______________
- avionics compartment aft door
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 52-41-14-000-001 Removal of the Avionics-Compartment Aft Door AMM 52-41-14-400-001 Installation of the Avionics-Compartment Aft Door
3. Fault Confirmation
__________________
A. Job Set-up
(1) Put the access platform in position at zone 128.
B. Test
(1) Make sure that you cannot open the aft avionics compartment door.
4. Fault Isolation
_______________
A. If the test confirms the fault:
- get access to the avionics compartment by another avionics compartment door
- release the locking mechanism which is inside the blocked door
- replace the avionics compartment aft door (Ref. AMM TASK 52-41-14-000-001) and (Ref. AMM TASK 52-41-14-400-001).
PASSENGER COMPARTMENT FIXED INTERIOR DOORS - FAULT ISOLATION PROCEDURES
_______________________________________________________________________
TASK 52-51-00-810-801
Fault of the Cockpit Door Lock System - General
1. Possible Causes
_______________
- ELECTRICAL STRIKE (30MQ)
- COCKPIT SYST.CONTROL. (24MQ)
- ELECTRICAL STRIKE CTR. (31MQ)
- ELECTRICAL STRIKE (32MQ)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 52-51-00-710-002 Operational Test of the Cockpit Door Lock System
(CDLS)
AMM 52-51-12-000-001 Removal of the Electric Release Strike
AMM 52-51-12-400-001 Installation of the Electric Release Strike
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 ASM 52-51/01
3. Fault Confirmation
__________________
R
A. Test
(1) Do the operational test of the Cockpit Door Lock System (Ref. AMM
TASK 52-51-00-710-002). R
4. Fault Isolation
_______________
R
A. If the FAULT lamp of the indication light 22MQ at the COCKPIT DOOR panel 119VU and STRIKE TOP LED at the CKPT CONT panel 20VU are on:
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320 Trouble Shooting Manual 排故手册 舱门 DOORS(119)
