Cirrus SR20 G3 — Avionics Manual

1 avionics manual reference for the Cirrus SR20 G3.

Overview

PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL for CIRRUS DESIGN SR20 · 2005

This Pilot's Operating Handbook (POH) serves as the FAA Approved Airplane Flight Manual for the Cirrus Design SR20. It is specifically tailored for airplanes registered in Brazil and operating under the Agência Nacional de Aviação Civil requirements. The handbook includes essential operational procedures, performance data, and maintenance information necessary for the safe and efficient operation of the SR20. Pilots and operators are required to comply with the limitations and instructions outlined in this manual to ensure airworthiness and adherence to FAA regulations. The document is structured to provide clear guidance on various aspects of the aircraft, including general information, limitations, emergency procedures, and performance data.

Total fuel capacity: 60.5 U.S. gallons (229.0 L), usable fuel: 56 U.S. gallons (212.0 L).
Maximum gross weight for takeoff: 3000 lb (1361 kg).
Standard empty weight: 2050 lb (930 kg).
Maximum landing weight: 2900 lb (1315 kg).
Engine specifications: Teledyne Continental IO-360-ES, 200 hp @ 2700 rpm.

1 document