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  AIRSPEED  575  575 KNOTS  KNOTS  INDICATED  AIRSPEED - KNOTS  200  300  400  500  I 600  NEGATIVE  LIMIT LOAO FACTOR  STALL  NEGATIVE ULTIMATE  LOAD FACTOR  \  Figure 5.3. Flight Strength Diagram 