Textron Cessna 182S - Page 199

CESSNA
AIRCRAFT
COMPANY
MODEL 182/T182
WIRING DIAGRAM MANUAL
CAUTION: TENSION
LOADS ARE FOR A TEST
SAMPLE. DO NOT
PERFORM TENSION LOAD TEST ON WIRING INSTALLED IN
AN AIRPLANE.
Table 215. Minimum Tension Load for Installed Terminals and Splices
ALUMINUM WIRE AND TERMINALS
WIRE SIZE 8 6 4 2 1 0 00
LOAD IN POUNDS
130 200 300 500
700 900 1100
000 0000
1300 1500
OTHER TYPE WIRE AND TERMINALS
WIRE SIZE
24 22 20 18 16
14 12 10 8 6 4 2
0
LOAD IN POUNDS 10 15
19 38 50 70 110 15 220 300
400 550 700
20-10-06 Page 215
© Cessna
Aircraft Company
Mar
1/2004