__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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 52-51-11-991-004 Fig. 403
3. Job Set-up
__________ Subtask 52-51-11-860-053
A. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
(2)
Make sure that the cockpit door is closed during the replacement procedure.
4. Procedure
_________ (Ref. Fig. 403/TASK 52-51-11-991-004) Subtask 52-51-11-020-052
A. Removal of the Door Escape Hatch
(1)
Pull the quick-release pins (2) of the door brackets (1) so that they come free from the hatch brackets (5).
(2)
Push the door escape hatch (3) in the rear direction until it becomes free from the cut out of the cockpit door (4).
1EFF : ALL 1 52-51-11Page 412 1 1 May 01/05R 1 1 1CES 1
Door Escape Hatch Figure 403/TASK 52-51-11-991-004
1EFF : 1 1R 1CES ALL 1 11 1 52-51-11 Page 413 May 01/04
Subtask 52-51-11-420-052
B. Installation of the Door Escape Hatch
(1) Put the door escape hatch (3) in its installation position at the cockpit door (4).
NOTE : An offset of 1.0 mm (0.0393 in.) is permitted between the
____ surface of the door escape hatch (3) and the cockpit door (4).
(2)
Install the quick-release pins (2) of the door brackets (1) into the hatch brackets (5).
(3)
Make sure that the quick-release pins (2) engage correctly with their related hatch brackets (5).
5. Close-up
________ Subtask 52-51-11-860-054
A. Put the aircraft back to its initial configuration.
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Make sure that the aircraft electrical circuits are de-energized (Ref. TASK 24-41-00-862-002).
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STRIKE - ELECTRIC RELEASE - REMOVAL/INSTALLATION________________________________________________
TASK 52-51-12-000-001
Removal of the Electric Release Strike
1. Reason for the Job__________________
Self Explanatory
2. Job Set-up Information______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 ESPM 204825 AWM 52-51-02 Energize the Aircraft Electrical Circuits from the External Power
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-217,
52-51-12-991-001-A Fig. 401
R **ON A/C 218-299, 301-302,
52-51-12-991-001-B Fig. 401A
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 52-51-12-991-001-D Fig. 401B
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R **ON A/C 106-149, 218-231, 301-399, 401-499, Post SB 25-1444 For A/C 218-231,301-302, 52-51-12-991-001-C Fig. 401C **ON A/C ALL
3. Job Set-up__________ Subtask 52-51-12-860-051
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). Subtask 52-51-12-865-050
B. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------122VU DOORS/PAX/MONG 1MQ 13 T 4. Procedure_________
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