LOAD 
FACTOR, 
n 
12- 
II- 
IO- 
9- 
B- 
7- 
6- 
5- 
4- 
3 
2- 
I-. 
-o-. 
-I- 
-2- 
-3- 
-4- 
-5- 
GROSS WEIGHT - 16.000 LBS 
CLEAN CONFIGURATION 
SEA LEVEL ALTITUDE 
SYMMETRICAL LOADING 
I ,.,/,,.~A~~‘~,, FACTOR i 
~/POSlT,VE LlMlT LOAD FACTOR i 
LIMIT LIMIT 
AIRSPEED AIRSPEED 
575 575 KNOTS KNOTS 
INDICATED INDICATED AIRSPEED - KNOTS AIRSPEED - KNOTS 
200 300 300 400 400 500 500 I 600 600 
NEGATIVE LIMIT LOAO FACTOR 
STALL 
NEGATIVE ULTIMATE LOAD FACTOR 
\ 
Figure 5.3. Flight Strength Diagram