Boeing 707 - Page 622

CAUTION
DO NOT APPLY PRESSURE OR STRONG FORCE ON THE TONGUE
OF THE TERMINAL LUG AT THE HOLES IN THE TONGUE. DAMAGE
TO THE TERMINAL LUG CAN OCCUR.
(10) Examine the terminal lug assembly.
Make sure that:
• The terminal lug has no cracks
• The tongue of the terminal lug does not have a bend that is more than 0.15 inch from the
longitudinal axis of the bottom surface of the tongue. Refer to Figure 18 and Figure 19.
• The forward edge of the crimp mark is not farther than 0.13 inch from the rear end of the
tongue of the terminal lug. Refer to Figure 20.
• The certification mark is in the center of the bottom of the crimp impression; refer to Figure
21.
• The mark is formed correctly; refer to Figure 21.
• The angle of the crimped end is less than 15 degrees from the longitudinal axis of the
terminal lug. Refer to Figure 22.
2449189 S00061545383_V1
TERMINAL LUG TONGUE-BENT UP
Figure 18
2449190 S00061545384_V1
TERMINAL LUG TONGUE-BENT DOWN
Figure 19
ASSEMBLY OF AMP (TYCO) COPALUM, MS25435 AND THOMAS & BETTS ALUMINUM
TERMINALS
707, 727-787
STANDARD WIRING PRACTICES MANUAL
20-30-14
Page 30
Oct 15/2017D6-54446
ECCN 9E991 BOEING PROPRIETARY - See title page for details