Mooney M20M Bravo — Pilot's Operating Handbook

This document is the Aircraft Specification No. 2A3 for the Mooney M20 series, detailing specifications, operational limits, and equipment requirements for various models including the M20M. It serves as a reference for pilots and maintenance personnel, providing critical information on engine specifications, weight limits, fuel capacity, and control surface movements. The document outlines the history of the type certificate and includes essential data for safe operation and maintenance of the aircraft. It is crucial for understanding the performance characteristics and regulatory compliance of the Mooney M20 series.

• Engine: Textron-Lycoming O-320, 150 hp at 2700 RPM
• Maximum weight: 2450 lbs
• Fuel capacity: 49 gallons
• Maximum structural cruising speed: 150 mph (130 knots)
• Control surface movements: Flaps down to 21.5 degrees