The effect of a ventral fin on the static stability of an aeroplane is as follows: (1=longitudinal, 2=lateral, 3=directional)
Domanda 134, Principles of Flight - ATPL - Airline Transport Pilot license
| 1: positive, 2: negative, 3: negative |
| 1: negative, 2: positive, 3: positive |
| 1: no effect, 2: negative, 3: positive |
| 1: no effect, 2: positive, 3: negative |
