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时间:2011-03-27 22:14来源:蓝天飞行翻译 作者:航空
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R R R  ____NOTE : : MAKE SURE ALL STRANDS OF WIRE PROTRUDE THROUGH THE HOLE IN THE BUSHING. 
R R R  ____NOTE : : At the option of the operator X-ray inspection may be used to ensure that all strands of wire protrude through the holes in the bushing. 
RR  - Engage the contact core (7) on the exposed end of wire. - Crimp the contact core (7) with the appropriate tool. 

 


 Fire Detection Plugs - Contact Layout
 NSA938683
 Figure 007

 

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 Fire Detection Plugs - P/N Characteristics and Layout
 NSA938683
 Figure 008

 

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 Fire Detection Plug - Wire Stripping and Crimping Tools
 NSA938683
 Figure 009

 

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 Engage the insulator bushing (8) into the connector body (9)
 (Male contact).
 NOTE : Make sure that the counterbored end of the bushing faces
 out of the connector body,

 -Install the nut (10) on the connector body (9) (Male contact).
 -Slide the connector body, with the insulator bushing, over the contact and the support.
 -Apply a small fillet of potting compound 1-100HT:D, mixed in accordance with the manufacturers instructions, around the back of the spring washers.
 -Lightly coat the threads of connector body with LOCTITE sealant, Grade AA and, using a suitable holding device, TORQUE sleeve to 0.565 m.daN (49.9999 lbf.in).
 -Crimp the rear of the sleeve (4) with appropriate tool. The potting compound must be cured as follows before proceeding : 3 hours at 65 deg.C (149.00 deg.F) 1 hour at 121 deg.C (249.80 deg.F) 1 hour at 177 deg.C (350.60 deg.F)
 -Brush the shank of the sleeve and the wire on a distance of three inches with SR 529 adhesive thinned with toluol or methyl-ethyl-ketone to a viscosity of 300 P.
 -
Install heat shrinkable sleeve (2) against shoulder of sleeve and shrink with a suitable heat gun, do not exceed 357 deg.C

 (674.60 deg.F)shrink temperature.

 -
Install the heat shrinkable sleeve (3).

 -
Install the spring (1) in the groove at rear of the sleeve (4).


 E. NSA938684 fire detection connector
 (1) P/N identification (Ref. Fig. 010)
 NSA938684  01
 |  |
 |  -------- Type of contact code | 01 = Male contact
 |  | 02 = Female contact
 |  | 03 = Nut

 ------------------ Standard P/N
 (2) P/N characteristics
 (a) Contact layout (Ref. Fig. 010)

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R


 Fire Detection Plug - P/N Identification and Torque Values
 NSA938684
 Figure 010

 

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 (3) Crimping procedure (Ref. Fig. 011)
 -Slide the spring (1) and the sleeve (2) on the wire.
 -Strip the wire to the size "A".
 -Insert the end of the wire though the bushing (3) and into the contact core (4).
 -Crimp the contact core (4) with the required tool.
 -Apply a small fillet of potting compound DOW CORNING R-7002 or equivalent inside the bushing (3).
 -Insert the contact core (4) fully into the contact body, through the nut (5).
 -Increase the wire diameter by adding 19 mm (0.7480 in.) adhesive tape (Material No. 08-032) around the wire.
 ____NOTE : Make sure that the sleeve (2) can slide freely
 -Lightly coat the threads of the sleeve (2) with LOCTITE sealant (Material No. 08-013) and manually tighten the contact body (6).
 -Crimp the sleeve (2) with the required tool.
 -Wrap KAPTON silicone tape or equivalent around the wire, starting 25 mm (0.9842 in.) from the rear of the ferrule, towards the aft ferrule.
 -Slide and tighten fully the spring onto the ferrule.
 -Shrink for 3mn between 150 deg.C (302.00 deg.F) and 170 deg.C
 (338.00 deg.F).
 ____
NOTE : Shrinking is not necessary if the wire is installed on the engine (shrinking will be done by the engine heat when running).

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 Miscellaneous Items - Wire stripping, Crimping Tools and Layout
 NSA938684
 Figure 011


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 Jan 01/03
R

 

 _________________
4. Manufacturer P/Ns Miscellaneous items with manufacturer P/Ns installed on the aircraft have the P/Ns that follow :
 -195PN01Y01
 -1X2002749
 -205PN01
 -205PN01Y01
 -24-457
 -2LA002692
 -2LA003717
 -2LA004626
 -2LA004891
 
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