Table 6.2 Aircraft Changes Which Affect Stability 6.7 STABILITY AND CONTROL ANALYSIS EXAMPLE: F-16A and F-16C Figure 6.15 illustrates an early model F-16A and a later F-16C. The differences between the stabilators of the two aircraft are apparent. The increase in stabilator area was made to all but the earliest F-16As to increase pitch control authority. Table 6.3 lists descriptive data for each aircraft.
