Cirrus SR20 G7 — V Speeds Reference

The AAFC SR20 Quick Reference Sheet provides essential operational and performance information for the Cirrus SR20 G7 aircraft. It is designed for pilots and aviation enthusiasts who require quick access to critical data regarding the aircraft's engine specifications, operational limits, and V-speeds. This document serves as a handy reference for flight planning and in-flight operations, ensuring that pilots can make informed decisions based on accurate and concise information.

• Engine: Lycoming IO-390-C3B6, 215 HP
• Maximum Gross Takeoff Weight: 3150 lbs
• Usable Fuel Capacity: 56 gallons
• Vso: 62 KIAS, Vs: 71 KIAS, VR: 71-75 KIAS
• Crosswind Limit: 20 KTS