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时间:2011-03-27 08:44来源:蓝天飞行翻译 作者:admin
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 (b)
 Other damage (cracks, scratches, stress, marks, dents, bumps...):


 -If you find this type of damage, refer to the Structural Repair Manual (Ref. SRM 511100,P.Block 001) for damage classification and corrective action.
 4. Procedure
_________
 Subtask 53-11-00-250-057
 A. Inspection
 (Ref. Fig. 619/TASK 53-11-00-991-075)

 (1)
 Do a special detailed inspection of the internal side of the lower attachment of the windshield side post. This inspection is applicable at FR4, left and right sides. Refer to the Non-destructive Testing Manual (Ref. NTM 531133,P.Block-601).

 (2)
 Make a report of the damage after the NDT inspection:

 (a)
 Corrosion damage:

 -If you find damage, refer to the Structural Repair Manual (Ref. SRM 512200,P.Block 001) for types, inspection, removal and corrosion protection.

 (b)
 Other damage (cracks, scratches, stress, marks, dents, bumps...):

 


 -If you find this type of damage, refer to the Structural Repair Manual (Ref. SRM 511100,P.Block 001) or damage classification and corrective action.
 5. Close-up
________
 Subtask 53-11-00-410-069
 A. Close Access
 (1)
 Install the lining panel 211NW (212NW) on the side post at FR4.

 (2)
 Install the lining panel 211PW (212PW).

 

R  EFF : 001-049, 051-099, 101-105, 151-154, 53-11-00Page 675 201-207, May 01/05
 CES


 (3)
 Close the sliding window.

 (4)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (5)
 Close the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-410-001).

 (6)
 Remove the access platform(s).

 

R  EFF : 001-049, 051-099, 101-105, 151-154, 53-11-00Page 676 201-207, May 01/05
 CES  **ON A/C ALL


 TASK 53-11-00-210-026
 Special Detailed Inspection of Windshield Side Post at Frame 4, Upper
 Attachment, Internal Side, LH/RH

 1. Reason for the Job
__________________
R Refer to the MPD TASK: 531135-01
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific  access platform 3.50 m (11 ft. 6 in.)
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 09-005  USA MIL-S-81733 CLASS C CORROSION INHIBITIVE INTERFAY SEALANT (Ref. 20-31-00)
 Material No. 11-004  USA MIL-T-81533
 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM)
 (Ref. 20-31-00)

 Material No. 19-003  USA AMS 3819
 LINT-FREE COTTON CLOTH (Ref. 20-31-00)

 EFF : ALL


53-11-00Page 677


 C. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
52-10-00-010-001 Opening of the Passenger/Crew Door
 52-10-00-410-001 Closing of the Passenger/Crew Door
 56-12-11-010-001 Opening of the Cockpit Sliding Windows
 56-12-11-410-001 Closing of the Cockpit Sliding Windows
 NTM 531135,P.Block-601
 SRM 511100,P.Block 001 (for corrective action)
 SRM 512200,P.Block 001 (for corrective action)
 53-11-00-991-041 Fig. 620

R  53-11-00-991-042-A Fig. 621 53-11-00-991-069-A Fig. 622
 3. Job Set-up
__________
 Subtask 53-11-00-010-066
 A. Get Access
R (1) Put an access platform in position at zone 831 (841).
 (2)
 Open the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-010-001).

 (3)
 Open the sliding window (Ref. TASK 56-12-11-010-001).

 (4)
 Remove the lining panels 211NW (212NW).
 (Ref. Fig. 620/TASK 53-11-00-991-041)


 (5)
 Remove the lining panels 211BC, 211KC, 211LC (212BC, 212KC, 212LC). (Ref. Fig. 620/TASK 53-11-00-991-041)


 Subtask 53-11-00-020-062
 B. Removal of the Components R (Ref. Fig. 621/TASK 53-11-00-991-042-A)
 (1) Remove the 3 bolts (1) and the nuts (2).
 EFF : ALL


53-11-00Page 678
 
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