Piper PA-46 Meridian — Specifications
1 specifications reference for the Piper PA-46 Meridian.
This document provides specifications for the Piper PA-46-500TP Meridian, a single-engine turboprop aircraft. It details the aircraft's performance, dimensions, and operational capabilities, aimed at pilots and aviation enthusiasts. The Meridian is designed for efficiency and ease of operation, featuring advanced avionics and a powerful Pratt & Whitney engine. The document outlines critical performance metrics such as takeoff distances, climb rates, and cruise speeds, along with detailed specifications on weight, fuel capacity, and airspeeds. It serves as a comprehensive reference for understanding the capabilities and operational parameters of the Meridian.
- Max takeoff weight: 5,092 lb
- Max useful load: 1,750 lb
- Cruise speed: 260 KTAS at 25,000 ft
- Takeoff distance at sea level: 2,438 ft
- Max operating altitude: 30,000 ft
How many Specifications documents does Sprinkle have for the Piper PA-46 Meridian?
Sprinkle has 1 Specifications document on file for the Piper PA-46 Meridian.
What year is the Piper PA-46 Meridian Specifications?
The Piper PA-46 Meridian Specifications on file is dated 2003.
How many pages is the Piper PA-46 Meridian Specifications?
The Piper PA-46 Meridian Specifications runs 6 pages.
Where does Sprinkle's Piper PA-46 Meridian Specifications come from?
This Piper PA-46 Meridian Specifications was originally published by aeroresourcesinc.com and is hosted on Sprinkle with full text and specs.