Piper M600/SLS — Supplemental Type Certificate
1 supplemental type certificate reference for the Piper M600/SLS.
This document provides detailed specifications for the Piper M600/SLS aircraft, including performance data, engine specifications, weights, speeds, and cabin dimensions. It is intended for pilots, aviation enthusiasts, and potential buyers, offering a comprehensive overview of the aircraft's capabilities and features. The M600/SLS is a single-engine turboprop designed for efficiency and performance, equipped with advanced avionics and a spacious cabin. Key information includes engine details, maximum weights, fuel capacity, and operational ranges, making it a valuable resource for understanding the aircraft's operational parameters.
- Engine: Pratt & Whitney PT6A-42A, 500 shp, TBO 3,600 hours.
- Max Takeoff Weight: 5,092 lbs (2,310 kg).
- Max Cruise Speed: 260 ktas (482 km/h).
- Range: 1,000 nm (1,852 km) with 45 min reserve.
- Cabin Pressure: Max differential 5.5 psi.
How many Supplemental Type Certificate documents does Sprinkle have for the Piper M600/SLS?
Sprinkle has 1 Supplemental Type Certificate document on file for the Piper M600/SLS.
What year is the Piper M600/SLS Supplemental Type Certificate?
The Piper M600/SLS Supplemental Type Certificate on file is dated 2020.
How many pages is the Piper M600/SLS Supplemental Type Certificate?
The Piper M600/SLS Supplemental Type Certificate runs 4 pages.
Where does Sprinkle's Piper M600/SLS Supplemental Type Certificate come from?
This Piper M600/SLS Supplemental Type Certificate was originally published by www.piper.com and is hosted on Sprinkle with full text and specs.