The regulations state:
Gyroscopic rate-of-turn indicator, except on the following aircraft:
(i) Airplanes with a third attitude instrument system usable through flight attitudes of 360 degrees of pitch and roll and installed in accordance with the instrument requirements prescribed in
This means I need a rate of turn unless I have a third attitude instrument/
My first one would be my artificial horizon. What does the FAA define as attitude instrument? Trying to decide what constitutes number two and three.
thanks
Gyroscopic rate-of-turn indicator, except on the following aircraft:
(i) Airplanes with a third attitude instrument system usable through flight attitudes of 360 degrees of pitch and roll and installed in accordance with the instrument requirements prescribed in
This means I need a rate of turn unless I have a third attitude instrument/
My first one would be my artificial horizon. What does the FAA define as attitude instrument? Trying to decide what constitutes number two and three.
thanks