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REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
Material No. 19-010 USA AMS 5687
LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
(Ref. 20-31-00)
C. Referenced Information
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REFERENCE DESIGNATION
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24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 33-21-12-400-001 Installation of the Cabin Entrance Light Dimming Switch (310LG) 52-51-00-710-002 Operational Test of the Cockpit Door Lock System (CDLS)
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-217,
52-51-00-991-003 Fig. 504
R **ON A/C 106-149, 221-299, 301-399, 401-499,
52-51-00-991-003-B Fig. 504A
**ON A/C 218-220,
52-51-00-991-003-A Fig. 504B
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-217,
52-51-00-991-004 Fig. 505
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REFERENCE DESIGNATION
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R **ON A/C 106-149, 218-299, 301-399, 401-499,
52-51-00-991-004-A Fig. 505A
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-217,
52-51-00-991-005 Fig. 506
**ON A/C 218-220,
52-51-00-991-005-A Fig. 506A
**ON A/C ALL
52-51-00-991-009 Fig. 507
3. Job Set-up
__________
Subtask 52-51-00-860-071
A. Aircraft Maintenance Configuration
(1)
Make sure that the cockpit door is closed.
(2)
Make sure that the aircraft electrical circuits are energized (Ref. TASK 24-41-00-861-002).
Subtask 52-51-00-865-062
B. Open, safety and tag this(these) circuit breaker(s):
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PANEL DESIGNATION IDENT. LOCATION
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122VU DOORS/PAX/MONG 1MQ 13 T
R 1EFF : ALL 1 52-51-00Page 543 1 1 Aug 01/05 1 1 1CES 1
4. Procedure
_________ **ON A/C 001-049, 051-099, 101-105, 151-199, 201-217,
Subtask 52-51-00-820-050
A. Adjustment of the Cockpit Door (Ref. Fig. 504/TASK 52-51-00-991-003)
(1) Adjust the upper clearance "A" of the cockpit door as follows:
(a) Measure the clearance "A" between the top of the closed cockpit door (2) and the cockpit wall panel (1).
NOTE : The clearance "A" must have a minimum of 4 mm (0.1574
____ in.).
(b) If the clearance "A" is less than the limit , adjust it as follows:
1_ Remove the locknut (5) from the top hinge (9).
2_ Turn the adjustment nut (4) until the clearance "A" is
correctly adjusted.
3_ Install the locknut (5) on the upper hinge (9).
(2)
Make sure that the limit switch 310LG in the cockpit wall is correctly adjusted (Ref. TASK 33-21-12-400-001).
(3)
Adjust the lateral clearances "B" and "C" of the cockpit door as follows:
WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______ MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE
_______ THIS/THESE MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES.
R 1EFF : ALL 1 52-51-00Page 544 1 1 Aug 01/05 1 1 1CES 1
(a) Measure the clearance "B" between the cockpit door (2) and the inboard edge of the safety angle (13) installed on the galley wall (12).
NOTE : The clearance "B" must have a minimum of 3.7 mm (0.1456
____
in.).
(b) Measure the clearance "C" between the cockpit door (2) and the lavatory wall (15). 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM DOORS 舱门7(45)
