CESSNA F-337 Skymaster G — Specifications
1 specifications reference for the CESSNA F-337 Skymaster G.
Overview
Specifications for the CESSNA F-337 Skymaster G
This document provides detailed specifications for the CESSNA F-337 Skymaster G, a unique aircraft known for its twin-engine configuration and distinctive design. It serves as a reference for pilots, maintenance personnel, and aviation enthusiasts interested in understanding the aircraft's performance, dimensions, and operational capabilities. The specifications include critical data such as weight limits, fuel capacity, engine details, and performance metrics, which are essential for safe and efficient flight operations.
- Maximum takeoff weight: 3,800 lbs (1,724 kg)
- Maximum cruise speed: 180 knots (207 mph)
- Stall speed in landing configuration: 60 knots (69 mph)
- Service ceiling: 20,000 feet (6,096 m)
- Total fuel capacity: 80 gallons (303 liters)
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