Single-engine two-seat aircraft, developed in the late 1940s as the PA-15. A version with dual controls, a different engine, and shock-absorbing landing gear was produced, and designated as the PA-17. A total of 601 were produced.
https://en.wikipedia.org/wiki/Piper_PA-15_Vagabond
https://www.flugzeuginfo.net/acdata_php/acdata_pa15_en.php
GENERAL STATS (PA-15 Vagabond)
Crew: 1
Capacity: 1 passenger
Length: 18 feet 8 inches (5.69 meters)
Wingspan: 29 feet 3 1/8 inches (8.92 meters)
Height: 6 feet (1.8 meters)
Wing area: 147.5 square feet (13.70 meters squared)
Gross weight: 1,100 pounds (499 kilograms)
Fuel capacity: 12 US gallons (45 liters, 10 imperial gallons)
Powerplant: x1 Lycoming O-145 four-cylinder piston engine, 65 HP
Max speed: 100 MPH (160 KMH, 87 knots)
Stall speed: 45 MPH (72 KMH, 39 knots)
Range: 250 miles (400 kilometers, 200 nautical miles)
Service ceiling: 10,000 feet (3,000 meters)
The Piper PA-15 Vagabond and PA-17 Vagabond are both two-seat, high-wing, conventional gear light aircraft that were designed for personal use and for flight training and built by Piper Aircraft starting in 1948.
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