The 1928 T-2 Air Coach was a five place cabin high wing monoplane. The price was $6,500.
Engine: 200hp Anzani (later 220hp Wright J-5)
Wingspan: 38’6″
Length: 25’0″
Useful load: 1100 lb
Max speed: 140 mph
Cruise speed: 110 mph
Stall: 52 mph
Range: 400 mi
Seats: 5
The 1928 T-2 Air Coupe was a three place cabin high wing monoplane. The price was $2,345.
Engine: 120hp Anzani
Wingspan: 38’0″
Length: 25’0″
Useful load: 500 lb
Max speed: 110 mph
Cruise speed: 90 mph
Stall: 53 mph
Range: 400 mi
Seats: 3
Designed by W H Woerner, the sole 1927 Wasp Special NX7571 c/n 2 was a Dole Race entry but it spun in and crashed prior to the race.
Engine: 80hp Anzani
Seats: 1
A seaplane for USN testing of pontoons was designed and built by a Lt Holden Richardson at the Washington Shipyard. A three place open cockpit biplane, power was from two engines.
One Seaplane / Richardson 82-A was built, A82, and three 3 ordered and s/ns issued. The last two, A83 and A84 were cancelled before construction.
The Columbia monoplane was entered for the 1912 Gordon Bennett aviation race held in Chicago, to be piloted by Paul Peck, known as “The Birdman of West Virginia”, powered by a rotary rated at 50 hp. In 1912 Peck was killed while flying the Columbian at a Chicago exhibition. Peck started a steep spiral, ignoring a sudden storm, the engine came loose, cut through the pilot’s seat with its whirling propeller, and the airplane disintegrated in the air.
The 1913 Washington Aeroplane Co Miss Columbia was built on special order for a customer. The wings mounted above a sleek, wooden boat hull.
Engine: Gyro, 80hp
Wingspan: 38’0″
Length: 29’0″
Seats: 2
The 1969 W-4 Hot Canary single place open cockpit biplane was intended for pylon racing in the sport biplane class. Featuring negative stagger, the W-4 was registred N4777W.
Engine: Lycoming O-290D, 125hp
Wingspan: 14’9″
Length: 17’0″
Useful load: 314 lb
Max speed: 195 mph
The 1960 Tiny Champ single place cabin high wing monoplane was registered N3632G.
Engine: Continental A-65, 65hp
Wingspan: 20’0″
Length: 19’0″
Useful load: 250 lb
Max speed: 115 mph
Cruise speed: 105 mph
Stall: 60 mph
Range: 250 mph
Bill Warwick built his third plane, the Bantam, first flying in 1966. The first Bantam, N2258B, first flew in June 1966.
Designed for simple fabrication, the Bantam uses no compound curves and very few simple ones. The cockpit area is a steel tube structure taking all wing, gear and engine mount loads. The steerable front wheel has a spring leaf shock absorber. The remaining is wood construction with a plywood cover.
The Bantam is a single-seat, low-wing plane that can use any engine from 65 to 100 hp.
Blueprints cost US$55 in 1972.
Engine: Lycoming O-145, 65 hp
Wingspan: 18 ft 6 in
Length: 13 ft 9 in
Height: 6 ft 0 in
Gross weight: 790 lb
Empty Wt. 535 lbs
Fuel capacity 11.5 USG
Top speed: 140 mph
Cruise speed: 105 mph
Stall 52 mph
ROC: 1000 fpm
TO run: 550 ft
Ldg run: 500 ft
Circa 1930 Warrior Aeronautical Corp built a Salmson powered single place open cockpit mid-wing monoplane registered prototype N950W c/n 501. The registration was cancelled in 1933.
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