Rearwin

Rearwin Airplanes was founded by Raymond Andrew (“Rae”) Rearwin in 1928, at Salina, KS.

Following Charles Lindbergh’s historic transatlantic flight in 1927, the world’s fascination with aviation grew significantly. Moreover, the Air Commerce Act of 1926 established the government certification program of pilots and aircraft that gave the fledgling industry safety and legitimacy.

Rearwin produced Junior two-seat light monoplane in 1931, followed by Speedster with American Cirrus engine.

Employing his two sons, Royce and Ken, the small company designed and built over 400 airplanes, including instrument trainers and gliders, despite the effects of the Great Depression.

Taken over in 1935 by partnership called Rearwin Airplanes. In 1937 bought assets of Le Blond Aircraft Corporation renamed as Ken-Royce motors. 1939: Renamed Rearwin Aircraft & Engines Inc.

Rae Rearwin sold the company to the Empire Ordinance Company in 1942. The company built about 275 more Skyrangers under the Commonwealth name before they closed their doors in 1946.

Rawdon T-1

Rawdon Brothers, a flying school operator, designed and built a Lycoming engined two-seat monoplane, the T-1, first produced in 1938. At least five were produced pe-war.

Rawdon T-1SD Article

The design was resurrected in 1953, powered by a 135 hp Lycoming engine.

The T-1S is an agricultural version equipped with spray tanks and spray bars.

Engine: Lycoming O-290
Max speed: 138 mph
Cruise: 120 mph
ROC: 900 fpm
Service ceiling: 18,000 ft
Range: 500 mi
Empty weight: 1300 lb
Loaded weight: 1900 lb
Wingspan: 33 ft 4 in
Length: 24 ft 2 in
Height: 7 ft 3 in

Ranger L-440 / 6-440C

The Ranger L-440 (company designation 6-440C) are six-cylinder inline inverted air-cooled aero-engines produced by the Ranger Aircraft Engine Division of the Fairchild Engine and Airplane Corporation of Farmingdale, New York, United States. The engine was mainly produced for Fairchild’s family of training aircraft in the mid-1930s.

Variants:
6-440C-2
175hp variant with a 6:1 compression ratio.

6-440C-3
180hp variant with a 6.2:1 compression ratio.

6-440C-4
190hp variant with a 6.8:1 compression ratio.

6-440C-5
200hp variant with a 7.5:1 compression ratio.

Applications:
Fairchild PT-19/26
Falconar SAL Mustang
Grumman Widgeon
Maestranza Central de Aviación HF XX-02
St. Louis PT-LM-4

Specifications:

6-440C-2
Type: Six-cylinder inline inverted air-cooled
Bore: 4 1⁄8 in (104.8 mm)
Stroke: 5 1⁄2 in (139.7 mm)
Displacement: 441 in³ (7.2 litres)
Length: 53.156 in (1.351 m)
Width: 21.954 in (0.549 m)
Height: 33.50 in (0.854 m)
Dry weight: 376 lb (170.7 kg)
Valvetrain: Underhead camshaft
Fuel system: Upright carburetor
Fuel type: 65 octane rating gasoline
Oil system: Full pressure type
Cooling system: air-cooled (pressure type cylinder baffles)
Power output: 175 hp at 2,450 rpm
Compression ratio: 6:1