Piper PA-34 Seneca V — Specifications
2 specifications references for the Piper PA-34 Seneca V.
The document provides detailed specifications and pricing information for the Piper PA-34 Seneca V, a twin-engine aircraft known for its turbocharged performance and advanced avionics. It is designed for pilots and aviation enthusiasts interested in the technical aspects and operational capabilities of the Seneca V. Key features include engine specifications, dimensions, weights, fuel capacity, performance metrics, and standard equipment. The document also outlines optional equipment and interior/exterior styling options, making it a comprehensive reference for potential buyers and operators.
- Engine: 2 x Continental TSiO-360-RB, 220 hp each
- Maximum Takeoff Weight: 4,750 lbs (2,155 kg)
- Cruising Speed: 200 KTAS (370 km/h)
- Range: 828 nm (1,534 km) with 45 min reserve
- Maximum Approved Altitude: 25,000 ft (7,620 m)
How many Specifications documents does Sprinkle have for the Piper PA-34 Seneca V?
Sprinkle has 2 Specifications documents on file for the Piper PA-34 Seneca V.
What year is the Piper PA-34 Seneca V Specifications?
The Piper PA-34 Seneca V Specifications on file is dated 2013.
How many pages is the Piper PA-34 Seneca V Specifications?
The Piper PA-34 Seneca V Specifications runs 4 pages.
Where does Sprinkle's Piper PA-34 Seneca V Specifications come from?
This Piper PA-34 Seneca V Specifications was originally published by cutteraviation.com and is hosted on Sprinkle with full text and specs.