Cirrus SR20 G3 — Systems Description

This document provides a comprehensive systems description for the 2009 Cirrus SR20 G3, specifically for aircraft N511RT. It includes critical specifications such as weight limits, fuel capacity, and engine details. The document is intended for pilots and aviation enthusiasts who require detailed knowledge of the aircraft's systems and performance characteristics. Key information includes the electrical system specifications, avionics suite, and various performance speeds essential for safe operation. The document serves as a reference for understanding the aircraft's capabilities and limitations, ensuring pilots can operate the SR20 G3 effectively and safely.

• Empty Weight: 1048.23 lbs
• Max T/O Weight: 3050 lbs
• Useful Load: 1000 lbs
• Fuel Capacity: 58.5 gallons (usable: 56 gallons)
• Max Crosswind Component: 20 knots at 90 degrees
• Minimum CAPS Deployment Altitude: 600 feet AGL
• VNE: 200 KIAS, VNO: 163 KIAS, VY: 96 KIAS