K10W1 trainer, copied from North American NA-16, built in 1941; production after first 26 given to Nippon.
1 engine
Watanabe E9W1 / Navy type 96 / Kyushu E9W1 / Nakajima E9N1

In January 1934, the Imperial Japanese Navy had a requirement for a two-seat reconnaissance seaplane to be operated from its J-3 type submarines, and placed an order with Watanabe Ironworks for design and development of an aircraft to meet this requirement.
The E9W was a two-seat single-engine twin-float unequal-span seaplane designed to be easily dismantled for hangar stowage on a submarine, capable of being reassembled in two minutes 30 seconds and disassembled in one minute 30 seconds. It was armed with a 7.7 mm (0.303 in) machine gun operated by the observer.

The first of three prototypes flying in February 1935.

Following successful testing of one of the prototypes on the submarine I-5, an order for a production batch of 32 aircraft, designated E9W1, was placed. It was also built by Nakajima as the E9N1.

The aircraft entered service in 1938 with the Imperial Japanese Navy Air Service as the Navy Type 96 Small Reconnaissance Seaplane with the last being delivered in 1940. Although it was in the process of being replaced by the Yokosuka E14Y monoplane, it was still in front line service at the time of the Japanese attack on Pearl Harbor, remaining in service until July 1942, being used to direct their parent submarines onto Chinese ships attempting to pass the Japanese blockade of the South China Sea. The E9W1 was given the reporting name Slim in 1942 by the Allies of World War II.

E9W1
Engine: 1 × Hitachi Tempu II, 224 kW (300 hp)
Wingspan: 9.91 m (32 ft 9½ in)
Wing area: 23.51 sq.m (252.95 sq.ft)
Length: 8.00 m (26 ft 3 in)
Height: 3.71 m (12 ft 2 in)
Empty weight: 882 kg (1,940 lb)
Gross weight: 1,253 kg (2,756 lb)
Maximum speed: 232 km/h (144 mph)
Cruising speed: 148 km/h (92 mph)
Range: 731 km (454 miles)
Endurance: 4.9 hours
Service ceiling: 6,740 m (22,100 ft)
Crew: 2 (pilot, observer)
Armament: 1 x 7.7mm (0.303in) machine gun



Wasp Airplane Co T-2 Air Coach
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
Wasp Airplane Co T-2 Air Coupe
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
Wasp Airplane Co Special

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
Washington Aeroplane Co Columbia

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.
Washington Aeroplane Co Miss Columbia

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

Warwick W-4 Hot Canary
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
Warwick Tiny Champ
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
Warwick Bantam

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