Cirrus SR20 G6 — Service Bulletins

This document is the Airplane Information Manual for the Cirrus SR20, specifically for aircraft serial numbers 1268 and subsequent. It serves as a reference for pilots and owners, providing essential information about the aircraft's systems, performance, and operational limitations. The manual is harmonized with the SR20 Pilot's Operating Handbook and is intended to assist in the safe operation of the aircraft. It includes details on the engine, propeller, fuel, oil, weights, dimensions, and various terminologies relevant to flight operations. While it is a comprehensive guide, it is important to note that this manual is not updated regularly and should not be used as a substitute for the official Pilot's Operating Handbook.

• Engine: Teledyne Continental IO-360-ES, 200 hp @ 2700 rpm
• Maximum Takeoff Weight: 3000 lb (1361 kg)
• Maximum Landing Weight: 2900 lb (1315 kg)
• Fuel Capacity: 60.5 U.S. gallons (usable: 56 U.S. gallons)
• VNE: 200 KIAS, VNO: 165 KIAS, VO: 131 KIAS at max gross weight