Rod End Installation Method - Piper PA-44-180 SEMINOLE Maintenance Manual

AIRPLANE MAINTENANCE MANUAL
CHART 2701. CABLE TENSION VS. AMBIENT TEMPERATURRE
120
110
100
90
80
70
60
50
40
30
20
-10 -8
RIGGING LOAD CORRECTION, POUNDS
Figure 27-1. Rod End Installation Method
PIPER AIRCRAFT
PA-44-180/180T
-2
-6 -4 0 2 4 6
SUBTRACT ADD
1K4
10
8
Revised: June 20, 1995
27-00-00
Page 27-2