Section V
Performance Charts
Performance information has been derived from actual flight tests and corrected to standart atmospheric conditions at 2200 pounds maximum gross weight. All performance is representative of the AA-5 equipped with the standart McCauley 1C172/SBTM7359 propeller.
Actual performance will vary from standart due to variations in atmospheric conditions, engine and propeller condition, mixture leaning technique, and other variables associated with the particular performance item.
- Take-Off Data
- Maximum-Rate-of-climb Data
- Cruise and Range Performance
- Landing Data
- Stall Speeds - MPH CAS
- Airspeed Correction Table
- Maximum Glide