R 1EFF : ALL 1 52-51-12Page 409 1 1 Aug 01/05 1 1 1CES 1
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R **ON A/C 106-149, 218-231, 301-399, 401-499,
R Post SB 25-1444 For A/C 218-231,301-302,
R 52-51-12-991-001-C Fig. 401C
**ON A/C ALL
3. Job Set-up__________
Subtask 52-51-12-860-050
A. Aircraft Maintenance Configuration
(1) Make sure that the access to the cockpit is available.
(2) Make sure that the aircraft electrical circuits are energized (Ref. TASK 24-41-00-861-002).
(3) Make sure that the cockpit door is open.
Subtask 52-51-12-865-051
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------122VU DOORS/PAX/MONG 1MQ 13 T
4. Procedure_________
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-217,
(Ref. Fig. 401/TASK 52-51-12-991-001-A)
R **ON A/C 218-299, 301-302,
(Ref. Fig. 401A/TASK 52-51-12-991-001-B)
R 1EFF : ALL 1 52-51-12Page 410 1 1 Aug 01/05 1 1 1CES 1
R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-217,
R Post SB 25-1444 For A/C 001-049,051-099,101-105,151-199,201-217,
R (Ref. Fig. 401B/TASK 52-51-12-991-001-D)
R **ON A/C 106-149, 218-231, 301-399, 401-499,
R Post SB 25-1444 For A/C 218-231,301-302,
R (Ref. Fig. 401C/TASK 52-51-12-991-001-C)
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-217,
Subtask 52-51-12-420-050-A
A. Installation of the Electric Release Strikes
(1) Clean the component interface and/or the adjacent area.
(2) Make sure that the electrical connectors are clean and in the correct condition.
(3) Carefully put the strike harness (3) through the grommet (13) and the release strike (14) into its installation position.
(4) Install the release strike (14) in the strike housing (12) with the screws (15) and (16).
(5) Put the strike housing (12) with the shim plates (9) and/or (10) into the lavatory wall housing (1) and install the spring sheets (11).
NOTE : The quantity of the shim plates (9) and/or (10) results from____ the position of the cockpit door.
(6) Connect the electrical connections.
CAUTION : REFER TO THE MATCH MARKS MADE DURING THE REMOVAL WHEN YOU_______ CONNECT THE ELECTRICAL WIRES. INCORRECT CONNECTION OF THE WIRES WILL CAUSE DAMAGE TO EQUIPMENT.
(a) Connect the electrical connectors of the strike harness (3) to the electrical connectors (13) of the fuselage wire harness (2) (Ref. ESPM 204825) (Ref. AWM 52-51-02).
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(7)
Put the cover plate (5) on the lavatory wall housing (1) and install the screws (4).
(8)
Put the cover profile (7) on the lavatory wall (8) and install the screws (6).
R **ON A/C 106-149, 218-299, 301-399, 401-499,
Subtask 52-51-12-420-050-B
A. Installation of the Electric Release Strikes
(1)
Clean the component interface and/or the adjacent area.
(2)
Make sure that the electrical connectors are clean and in the correct condition.
(3)
Carefully put the strike harness (3) through the grommet (13) and the release strike (14) into its installation position.
(4)
Install the release strike (14) in the strike housing (12) with the screws (15) and (17).
(5)
Put the strike housing (12) with the shim plates (9), (10) and/or
(16) into the lavatory wall housing (1) and install the spring sheets (11).
NOTE : The quantity of the shim plates (9), (10) or (16) result from
____
the position of the cockpit door.
(6) Connect the electrical connections. CAUTION : REFER TO THE MATCH MARKS MADE DURING THE REMOVAL WHEN YOU 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(58)
