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ACTION RESULT -------------------------------------------------------------------------------- remove the vacuum pump from the - the electrical release strikes pressure sensor hole. operate automatically to lock the cockpit door.
R
5. Close-up________
R
Subtask 52-51-00-860-067
A. Put the aircraft back to the serviceable condition.
(1) Make sure that the work area is clean and clear of tool(s) and other items.
(2) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
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R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-220,
TASK 52-51-00-720-003
Functional Check of the Adjustment of the Cockpit Door, Electrical Release Strikes and Latch Mechanism
1. Reason for the Job__________________
Refer to the MPD TASK: 525111-06
2. Job Set-up Information______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 24-41-00-862-002 52-51-00-820-001 Energize the Aircraft Electrical Circuits from the External PowerDe-energize the Aircraft Electrical Circuits Supplied from the External PowerAdjustment of the Cockpit Door, Electrical Release Strikes and Latch Mechanisms
R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-217,
R 52-51-00-991-013 Fig. 501
R **ON A/C 218-220,
R 52-51-00-991-013-A Fig. 501A
R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-217,
R 52-51-00-991-014 Fig. 502
R **ON A/C 218-220,
R 52-51-00-991-014-A Fig. 502A
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-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-220,
R 52-51-00-991-015 Fig. 503
3. Job Set-up__________
Subtask 52-51-00-860-108
A. Aircraft Maintenance Configuration
(1) Make sure that the cockpit door is closed.
(2) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
4. Procedure_________
R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-217,
Subtask 52-51-00-720-053
A. Measurement of the Clearances
R R R (1) Measure the clearances around the cockpit door as follows: (Ref. Fig. 501/TASK 52-51-00-991-013)
(a) Measure the clearance "A" between the top of the cockpit door (2) and the cockpit door wall panel (1).
NOTE : The clearance "A" must have a minimum of 4.0 mm (0.1574____ in.).
(b) Measure the lateral clearance "B" between the cockpit door (2) and the inboard edge of the safety angle (13).
NOTE : The clearance "B" must have a minimum of 3.7 mm (0.1456____ in.).
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R 1 1
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R Cockpit Door - Measurement of Clearances
R Figure 501/TASK 52-51-00-991-013- 12 (SHEET 1)
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R Cockpit Door - Measurement of Clearances
R Figure 501/TASK 52-51-00-991-013- 22 (SHEET 2)
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(c) Measure the lateral clearance "C" between the cockpit door (2) and the lavatory wall (15).
NOTE : The clearance "C" must be between 8.0 mm (0.3149 in.) and
____ 10.0 mm (0.3937 in.).
(d) Measure the operlap "D" of the safety angle (13) and the cockpit door (2).
NOTE : The overlap "D" must be more than 2.0 mm (0.0787 in.).
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