Piper M600 — Specifications

This document provides a detailed specification comparison for various models of the Piper PA-46 aircraft series, including the Piper M600. It outlines key performance metrics, dimensions, and operational capabilities of each model, making it a valuable resource for pilots and aviation enthusiasts. The specifications include powerplant details, fuel capacity, cruise speeds, maximum altitude, range, maximum takeoff weight, seating configurations, and physical dimensions. This comparison allows users to understand the differences and similarities between the models, particularly focusing on the M600, which is the latest in the series with enhanced performance and capacity.

• Powerplant: Pratt & Whitney Canada PT6A-42A (600 shp)
• Max Cruise Speed: 274 knots
• Max Altitude: 30,000 feet
• Range with Max Fuel + Reserves: 1,484 nautical miles
• Max Takeoff Weight: 6,000 lbs
• Usable Fuel Capacity: 260 gallons
• Seating: 1 pilot + 5 passengers