Engine: Rotax 912, 100 hp
HP range: 85-160
Length: 17.6 ft
Wing span: 28 ft
Wing area: 94 sq.ft
Empty weight: 750 lb
Gross weight: 1356 lb
Fuel capacity: 40 USG
Cruise: 175 mph
Stall: 40 mph
Range: 980 sm
Rate of climb: 1500 fpm
Takeoff dist: 500 ft
Landing dist: 600 ft
Seats: 2
Landing gear: nosewheel
Engine: Lycoming O-290, 125 hp
HP range: 85-150
Length: 16 ft
Wing span: 16.6 ft
Wing area: 80 sq.ft
Empty weight: 606 lb
Gross weight: 1000 lb
Fuel capacity: 16 USG
Cruise: 125 mph
Stall: 52 mph
Rate of climb: 1500 fpm
Seats: 1
Cockpit width: 18 in
Landing gear: tailwheel
LSA: yes
Built in 1948, the A-1 Special was a Goodyear-class racer registered NX64573 and piloted by Harold Neumann and Warren Siem, and powered by an 85hp Continental C-85.
It competed in 1948 as Townsend Special, reportedly modified as a two-place with a 245hp Jacobs and re-registered N794T as Loose Racer.
The Townsend Thunderbird was assembled in 1955 from parts of at least four different planes. The fuselage structure (20′ in length) appears to be a cut-down Fairchild PT-26 with its canopy. The cowling is from a Stearman, the landing gear from a Cessna 190 or 195. Its wings, vertical and horizontal stabs are from a Vultee BT-13 or -15. The wings are just the outer panels (wing span is 25′) and the stabs have been cut down in size. Engine is a Wright R-975, which suggests BT-15.
Registered N749T, the aircraft started out fabric covered, but was later metalized.
In September 2002 Tony Pileggi purchased the home-built Thunderbird. With quite a history and, while it’s a shame to change all that, it was not safe to fly. Actually, it was really great in the air. Take-off and landing were scary. It was too short-coupled and over-powered, and it had an aft c/g or not enough horizontal stabiliser. The tail would not come off the runway until about 65 mph with full forward stick.
During flight-testing, the clean power-off stall speed was about 80 mph. At the first flap setting, the power-off stall speed was between 85 and 90, with a very abrupt snap into a spin. Attempting to recover from the spin under 100 mph resulted in a secondary stall, again with a tight spin. This was attributed to the very small flap size as they ran from the fuselage outboard only 16″. The size of the flaps created a thicker wing section at the root, and so caused the tips to stall long before the roots.
Tony Pileggi decided to disassemble the ship after the landing gear collapsed and made for a very exciting landing. When he removed the forward fuselage aluminium, he found some old cracks and some scary welding on the frame. A first impulse was to scrap the entire aircraft, but he then began thinking about redesigning it and building a replica of a WWII-era fixed-gear fighter. After extensive research, he found a plane that the Thunderbird most closely resembled, the Nakajima Ki-27.
Thunderbird
Engine: Jacobs R-755-9, 245hp
Wingspan: 27’5″
Length: 21’3″
Empty wt: 1800 lb
Max speed: 220 mph
Cruise speed: 152 mph
Stall: 75 mph
Range: 200 mi
Seats: 1
1948:
K R Townsend,
Tulsa OK.
USA
circa.1956:
Gid Townsend,
Ocala FL.
USA
Built the Townsend Thunderbird circa 1956.
The Towner Thunderbolt was a single-place cabin, low wing monoplane, based on the Culver Dart design. It was aerobatic and powered by a 220hp Continental engine.
A 1931 eight-passenger high-wing cantilever monoplane amphibian flying-boat, it was powered by two 225hp radial Packard DR-980 diesel engines mounted on muitistrut pylons on the wing upper surface. The TA-3 received certification ATC 2-291.
Towle TA-2 was built as a successor to the WC model. In 1930 one was built, NX491H, powered by two 240hp Wright Whirlwind J-6 on a faired housing and wing struts were omitted. Only the one was built.
Engines: 2 x Wright Whirlwind J-6, 240hp
Wingspan: 56’0″
Length: 42’0″
Useful load: 2257 lb
Max speed: 120 mph
Cruise speed: 100 mph
Stall: 55 mph
Range: 500 mi
Thomas Towle was an engineer who had been involved with many early aircraft designs. Having just co-designed the Eastman E2 Sea Rover, Towle was commissioned by Henry McCarroll to promote Detroit’s aviation production capabilities.
The 1928 Towle WC was built for businessman H G McCarroll and USN Lt George Pond by a group of Detroit engineers under the direction of Towle. An all-metal wing design (Towle F-2) essentially eliminated ribs and spars with its unique, internal zig-zag pattern of corrugated aluminum as a framework. The covering also was corrugated sheet aluminum. Wings were strut-braced. One WC was built, NX7956.
Priced at $25,000, the WC flying boat was first flown in November 1928. The prototype WC flew as far as Brazil before engine reliability issues forced the cancellation of the round-the-world flight attempt.
The 1930 TA-1 was the first production version of the WC with 150hp Comet engine. The one bult was registered NX5328.
WC
Engines: 2 x Comet, 150hp
Wingspan: 52’0″
Length: 35’0″
Useful load: 11,670 lb
Max speed: 115 mph
Cruise speed: 95 mph Stall: 45 mph
Range: 350 mi
Seats: 6
TA-1
Engines: 2 x Comet, 150hp
Towle Marine Aircraft Engineering Company was an American aircraft manufacturer of light amphibious aircraft.
Founded in 1927 in Detroit, Michigan, the Towle Marine Aircraft Engineering Company, and its successor Towle Aircraft Company (1928-1932) were founded by former Stout Metal Airplane Division of the Ford Motor Company engineer Thomas Towle. Incorporated initially to build a custom round-the world amphibious aircraft, and follow-on aircraft based on the design.
In a 1930 patent, Towle listed the Towle Aircraft Company as part of the Michigan Amphibian Airplane Corporation.
At the height of the depression, financing was difficult. Towle’s TA-3 used diesel engines on load from Packard, and was funded by Dr. Adams, a “painless dentist” of the Detroit region.
1933: Ended operations for other endeavors.
