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时间:2011-03-27 00:06来源:蓝天飞行翻译 作者:admin
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R  (e) Put the covers (35) and (36) in position and attach them with the screws (32) the washers (33) and the plug fasteners (34). 
R R  (9) Do a visual check for the correct adjustment of the three latch tenons (22). 
R R  NOTE : The rear face of each latch tenon has three arrow marks. If____ you can see only the last (inboard) arrow mark with the cockpit door closed, then their adjustment is correct.
 Subtask 52-51-00-865-063
 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1MQ.
 Subtask 52-51-00-710-053
 E. Do an operational test of the cockpit door and latch mechanism (Ref. TASK 52-51-00-710-002).
 5. Close-up________
 Subtask 52-51-00-860-072
 A. Put the aircraft back to the serviceable condition.
 (1) Make sure that the cockpit door is open.
 (2) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).

 

 PASSENGER COMPARTMENT FIXED INTERIOR DOORS - INSPECTION/CHECK
_____________________________________________________________
 TASK 52-51-00-220-001
 Detailed Inspection of Mechanical Parts of Cockpit Door
 1.
 Reason for the Job

__________________
 Refer to the MPD TASK: 525111-01


 2.
 Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE  QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
 No specific 1 BRUSH - BRISTLED, SOFT

 B. Consumable Materials
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
Material No. 11-010  USA TT-I-735 GRADE A
 ISOPROPYL ALCOHOL (Ref. 20-31-00)
 Material No. 19-003 USA AMS 3819
 LINT-FREE COTTON CLOTH (Ref. 20-31-00)

 C. 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 R 52-51-00-991-010 Fig. 601
 1EFF : ALL 1 52-51-00Page 601 1 1 May 01/04 1 1 1CES 1 1EFF : ALL 1 52-51-00Page 602 1 1 May 01/04 1 1 1CES 1R


R
 3. Job Set-up__________ 
R
 Subtask 52-51-00-860-086
 A. Aircraft Maintenance Configuration
 (1) Make sure that the access to the cockpit is available.
 (2) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
 Subtask 52-51-00-865-073 
R  B. Open, safety and tag this(these) circuit breaker(s): 
R R R R  -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------122VU DOORS/PAX/MONG 1MQ 13 T 
R
 Subtask 52-51-00-010-054
 C. Get Access (Ref. Fig. 601/TASK 52-51-00-991-010)
 (1) Remove the plugs (1) from the screws (2).
 (2) Remove the screws (2), the washers (3), the fasteners (4) and the covers (5) and (6) from the cockpit door (7).
 (3) Remove the screws (8) and the cover profile (9) from the lavatory wall (10).
 (4) Remove the screws (11) and the cover plates (12) from the lavatory wall housing (13).

 

 4. Procedure
_________
R (Ref. Fig. 601/TASK 52-51-00-991-010)
 Subtask 52-51-00-110-050
 A. Clean the Cockpit Door Bolting Mechanism:
 (1) Clean the subsequent components with a lint-free cotton cloth, MISCELLANEOUS (Material No. 19-003), or a BRUSH - BRISTLED, SOFT and the CLEANING AGENTS (Material No. 11-010)
 -
the latch assemblies (25), (26) and (27)

 -
the latch tenons (28)

 -
the D-ring mechanism (30)

 -
the tie-rods (29)

 -
the eye-ends (32)

 -
the connecting levers (33).


 (a) Dry the cleaned components with a dry and clean lint-free cotton cloth MISCELLANEOUS (Material No. 19-003).
 Subtask 52-51-00-220-054
 B. Detailed Inspection of the Mechanical Parts of the Door Locking System
 
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