Cirrus SR20 G6 — Flight Manual

This Pilot’s Operating Handbook (POH) serves as the FAA Approved Airplane Flight Manual for the Cirrus SR20, specifically for aircraft serials 2220, 2339, and subsequent models equipped with the Cirrus Perspective+ Avionics System. It is essential for pilots and operators to familiarize themselves with the operational procedures, performance data, and safety information contained within this manual. The POH is structured to provide comprehensive guidance on the aircraft's systems, limitations, emergency procedures, and normal operations, ensuring safe and efficient flight operations. The manual must be carried on board the aircraft at all times and kept accessible to the pilot during all flight operations.

• Total fuel capacity: 58.5 U.S. gallons (221.0 L), usable fuel: 56.0 U.S. gallons (212.0 L).
• Maximum gross weight for takeoff: 3150 lb (1429 kg).
• Engine: Lycoming IO-390-C3B6, 215 HP @ 2700 RPM.
• Propeller: Hartzell, constant speed, three-blade, 74.0" diameter.
• Oil capacity: 7 U.S. quarts (6.6 L).
• Wing loading: 21.7 lb/sq ft; power loading: 14.7 lb/HP.
• Best glide speed (VG) and other airspeed terminology defined for operational clarity.