Piper PA-44 Seminole — Specifications

This document is a vital specifications sheet for the Piper PA-44 Seminole, providing essential data for pilots and aviation enthusiasts. It includes critical weight limits, fuel capacities, operational speeds, oil specifications, and electrical system details. The information is crucial for safe operation and maintenance of the aircraft, ensuring that pilots are aware of the performance parameters and limitations of the Seminole. This reference is particularly useful for flight planning and pre-flight checks, as it consolidates important specifications into a single document.

• Max ramp weight: 3816 lbs
• Max takeoff weight: 3800 lbs
• Fuel capacity: 110 USG (usable: 108 USG)
• V A: 135 KIAS at 3800 lbs, 112 KIAS at 2700 lbs
• Max demonstrated cross-wind speed: 17 KIAS
• Oil capacity: 6 quarts (minimum: 2 quarts)
• Electrical system: 14 V, 60 Amps output per alternator