EasyManua.ls Logo

Boeing 707 - Page 1012

Boeing 707
1020 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
A. This Subject gives the procedures to assemble these nickel plated Copalum terminals with
aluminum or copper wire.
B. 2297683-1, 1958058-1 and 1958-054-1.
C. This subject gives the procedure to post insulate the BACY12M( ) terminals for use in the IDG
and APU. Refer to Subject 20-30-22 for the procedure to assemble BACT12M( ) terminals.
1. PART NUMBERS AND DESCRIPTION
(1) Nickel Plated Copalum Terminal Part Numbers
Table 1
NICKEL PLATED COPALUM TERMINAL PART NUMBERS
Crimp Barrel
Aluminum Part
Number
Supplier Wire
Size (AWG)
Copper Wire
Size (AWG)
Stud Size
Tong
Configuration
Plating Part Number Supplier
2 4
Straight Nickel
2297683-1
TE/AMP
1/0 2 2300538-1
1/0 2 2300882.1
2/0 1/0 or2 1958058-1
3/0 2/0 2300872-1
4/0 3/0 1958054-1
- 4/0 2300884-1
2. TERMINAL ASSEMBLY
(1) Selecting the Terminal and Wire.
(a) Identify the wire type.
(b) Select a terminal from Table 2/DESCRIPTION OF THE TERMINALS. Make sure the outside
diameter of the wire insulation is within the minimum/maximum insulation diameter range of
the terminal. Refer to Table 2/DESCRIPTION OF THE TERMINALS.
Table 2
DESCRIPTION OF THE TERMINALS
Description Part Number
Wire Size (AWG) Insulation Diameter Range (inch)
AL CU Minimum Maximum
Terminal, ring
tongue, single
hole, straight, 260°
temperature-rated,
nickel-plated,
Copalum
2297683-1 2 4 0.340 0.380
2300538-1 1/0 2 0.425 0.470
1958058-1 2/0 1/0 or 2 0.500 0.574
1958054-1 4/0 3/0 0.590 0.683
ASSEMBLY OF TE/AMP NICKEL PLATED COPALUM TERMNAL LUGS
707, 727-787
STANDARD WIRING PRACTICES MANUAL
20-30-23
Page 2
Feb 15/2021D6-54446
ECCN 9E991 BOEING PROPRIETARY - See title page for details

Table of Contents