Electric Release Strike Figure 401/TASK 52-51-12-991-001-A
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 52-51-12Page 403 1201-217, 1May 01/05 1 1 1CES 1

 Electric Release Strike Figure 401A/TASK 52-51-12-991-001-B
R 1EFF : 218-299, 301-302, 1 52-51-12Page 404 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 52-51-12-020-050-A
 A. Removal of the Electrical Release Strikes
 (1) Remove the screws (6) and the cover profile (7) from the lavatory wall (8).
 (2) Remove the screws (4) and the cover plate (5) from the lavatory wall housing (1).
 (3) Disconnect the electrical connections.
 CAUTION : MAKE MATCH MARKS ON ALL THE ELECTRICAL WIRES BEFORE YOU_______ DISCONNECT THEM. INCORRECT CONNECTION OF WIRES WILL CAUSE DAMAGE TO EQUIPMENT.
 (a) Disconnect the electrical connectors of the strike harness (3) from the electrical connectors (13) of the fuselage wire harness (2) (Ref. ESPM 204825) (Ref. AWM 52-51-02).
 (b) Make sure that the fuselage wire harness (2) and the strike harness (3) are safe and identified for easier installation.
 (4) Disassemble the spring sheets (11) and remove the release strike housing (12) with the shim plates (9) and/or (10) from the lavatory wall housing (1).
 NOTE : The quantity of the shim plates (9) and/or (10) result from____ the position of the cockpit door.
 (5) Remove the screws (15) and (16) from the release strike housing (12). 

R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 52-51-12Page 405 1201-231, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1R Electric Release Strike R Figure 401B/TASK 52-51-12-991-001-D

R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 52-51-12Page 406 1201-217, 1Aug 01/05 1 1 1CES 1R Electric Release Strike R Figure 401C/TASK 52-51-12-991-001-C

R 1EFF : 106-149, 218-231, 301-399, 401-499, 1 52-51-12Page 407 1 1 Aug 01/05 1 1 1CES 1

 (6) Remove the release strike (14) from the release strike housing (12). At the same time make sure that the strike harness (3) goes through the grommet (13) easily.
R **ON A/C 106-149, 218-299, 301-399, 401-499,
 Subtask 52-51-12-020-050-B
 A. Removal of the Electrical Release Strikes
 (1)
 Remove the screws (6) and the cover profile (7) from the lavatory wall (8).

 (2)
 Remove the screws (4) and the cover plate (5) from the lavatory wall housing (1).

 (3)
 Disconnect the electrical connections. CAUTION : MAKE MATCH MARKS ON ALL THE ELECTRICAL WIRES BEFORE YOU

_______ DISCONNECT THEM. INCORRECT CONNECTION OF WIRES WILL CAUSE DAMAGE TO EQUIPMENT.
 (a)
 Disconnect the electrical connectors of the strike harness (3) from the electrical connectors (13) of the fuselage wire harness

 (2) (Ref. ESPM 204825) (Ref. AWM 52-51-02).

 (b)
 Make sure that the fuselage wire harness (2) and the strike harness (3) are safe and identified for easier installation.

 (4) Disassemble the spring sheets (11) and remove the release strike housing (12) with the shim plates (9), (10) or (16) from the lavatory wall housing (1).
 NOTE : The quantity of the shim plates (9) or (10) or (16) result
____ from the position of the cockpit door.
 (5)
 Remove the screws (15) and (17) from the release strike housing (12).

 (6)
 Remove the release strike (14) from the release strike housing (12). At the same time make sure that the strike harness (3) goes through the grommet (13) easily.

 1EFF : ALL 1 52-51-12Page 408 1 1 Aug 01/05 1 1 1CES 1

 **ON A/C ALL
 TASK 52-51-12-400-001
 Installation of the Electric Release Strike
 1. Reason for the Job__________________
 Self Explanatory
 2. Job Set-up Information______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 24-41-00-862-002 52-51-00-710-002 52-51-00-820-001 ESPM 204825 AWM 52-51-02 Energize the Aircraft Electrical Circuits from the External PowerDe-energize the Aircraft Electrical Circuits Supplied from the External PowerOperational Test of the Cockpit Door Lock System (CDLS)Adjustment of the Cockpit Door, Electrical Release Strikes and Latch Mechanisms
　
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