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时间:2011-03-27 22:13来源:蓝天飞行翻译 作者:航空
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R  ____NOTE : : A table gives the list of wire gauges and related sections 
R  (Ref. 20-32-21) 
R  - Select the tool and setting applicable for the splice. 
R  - Make sure that it is in good conditions. 
R  - Position and center the splice in the indenter or between the tool 
R  dies. If the brazing seam is visible on the splice, place and 
R  center it opposite to the punch. 
R  - Squeeze the tool handles to hold the splice in the crimping 
R  position. 
R  - Insert the stripped cables in the splice and make sure that all 
R  strands are inserted.

 


R Parallel Splices - P/N Characteristics NSA936808
R Figure 004


20-43-12 Page 7

R Parallel Splices - Crimping and Shrinking Tools R NSA936808 R Figure 005


20-43-12 Page 8

R Parallel Splices - Examples of Uses of Compensation Sleeves R NSA936808 R Figure 006


20-43-12 Page 920-43-12 Page 10

R  - Move the two handles together or apply pressure to perform the 
R  crimping operation. Make sure complete crimping is obtained 
R  (ratchet release or automatic opening of dies). 
R  - Remove the crimped assembly. 
R  - Make sure that the connection is in the correct condition and that 
R  : 
R  .The cable insulator does not penetrate into the splice barrel. 
R  .The crimping indents are centered. 
R  .The stripped conductors do not prodrute excessively (visible 
R  length < 1.5 mm (0.0590 in.)). 
R  - If necessary, shrink the compensation sleeve(s). 
R  - Slide the insulation sleeve "B" in position and shrink it.

 


 _____________________________________________
CRIMP END SPLICES - DESCRIPTION AND OPERATION
 _______
1. General
 Crimp end splices installed on aircraft have the following codes : NSA936830 1 Conductor crimped end splices E0301 2 Conductors crimped end splices E0543 3 Conductors crimped end splices
 ___________________2. Crimped end Splices
 A. NSA936830
 (1) P/N identification NSA936830 | | | - 22|------------- Contact size

 ------------------------ Standard P/N
 (2) P/N characteristics (Ref. Fig. 001)
 (a) Temperature Minimum operating temperature is : -55 deg.C (-67.00 deg.F). Maximum operating temperature is : 175 deg.C (347.00 deg.F).
 B. E0301
 (1)
 P/N identification

 E0301  -01 | | | ------------- Reference No. | ---------------------- Standard P/N

 (2)
 P/N characteristics (Ref. Fig. 001)


 (a) Temperature Minimum operating temperature is : -55 deg.C (-67.00 deg.F). Maximum operating temperature is :175 deg.C (347.00 deg.F).
 C. E0543
 (1) P/N identification


20-43-13 Page 1

 Crimp End Splices - Contacts Layout
 E0301, E0543 and NSA936830
 Figure 001

 

20-43-13 Page 2

 E0543  - 01
 |  |
 |  ------------- Reference No.
 |

 ---------------------- Standard P/N
 (2) P/N characteristics (Ref. Fig. 001)
 (a) Temperature Minimum operating temperature is : -55 deg.C (-67.00 deg.F). Maximum operating temperature is : 175 deg.C (347.00 deg.F).


20-43-13 Page 3

 ________________
3. Connection Table (Ref. Fig. 002)


20-43-13 Page 4

 Crimp end Splices - Connection Table
 Figure 002

 

20-43-13 Page 5

 __________________________________________
PRESSURE SEALS - DESCRIPTION AND OPERATION

R _______
1. General

 This chapter concerns the description, installation and identification of pressure seals used on aircraft.
R  A. Grommet type Pressure Seals (Ref. 20-43-41) 
B. Compound Filled Pressure Seals (Ref. 20-43-42) 
R R C. Adhesive Sealant Pressure Seal (Ref. 20-43-43) 

 

20-43-40 Page 120-43-41 Page 1

 ________________________________________________________D.T.P. - TYPE PRESSURE SEALS - DESCRIPTION AND OPERATION
R R R R R R R R R R  _______1. General The grommet type pressure seals installed on aircraft have the following codes: - ABS0717 Feed Through ABS0834 Feed Through ABS1128 Feed Through E0073 (ex NSA934700) Feed Through - ABS0634 Fireproof ABS0681 Fireproof E0739 Fireproof NSA934501 Fireproof (2 passages) NSA934502 Fireproof (13 passages) NSA934504 Fireproof (4 passages)
 __________________________2. Feed Through Pressure Seal
 
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