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