Consolidated PT-1 Trusty Primary Trainer Aircraft (1924)
The PT-1 represented the first aircraft purchase of the Army Air Service since the closing shots of World War One.
Externally, the PT-1 appeared as a biplane aircraft with a simple two-wheel undercarriage, an engine mounted at the front of the design, a traditional tail section and twin side-by-side seating for instructor and student. Internally, the aircraft featured a strengthened structure of welded tubing and a choice of a Clerget or Le Rhone engines. The Dayton-Wright Company approached the USAAS to replace their World War 1-era Curtiss JN-4 "Jenny" series of trainers and was in turn asked to deliver three TA-3 models for evaluation. Though the design itself proved promising enough, the TA-3 (designated with an "A" for its air-cooled engine operation) was delivered by request with an uprated Le Rhone engine of 110 horsepower. Still further evaluation models were ordered, this time with the requested Wright-Hispano I V-8, 150 horsepower engine of increased power (designated TW-3 with the "W" standing for its water-cooled engine process) finally culminating in an official order by the USAAS.
Production rights for the trainer were secured by the newly-created Consolidated Aircraft Company (established by Reuben Fleet of the Gallaudet firm) as General Motors was reviewing their commitment to aircraft production in a post-war world and would eventually shut down operations at Dayton-Wright altogether. The TW-3 was delivered by 1923 and became the first notable variant of the "Trusty" production line.
Improvements to the TW-3 design continued and included the removal of the engine cowling (for improved forward cockpit visibility) and a redesigned fuselage in a slimmer form with tandem instructor/student seating (this model being known as the "Camel" for the visible bump appearing between the two seating areas). The Camel was evaluated under the (unofficial) designation TW-8 and accepted into service as the PT-1 with 221 being delivered beginning 1924 and replacing the TW-3's in service. The PT-1 educated generations of aviators from the middle of the 1920's into the 1930's.
The PT-1 would eventually be replaced itself by the Consolidated PT-3 from 1928 onwards. Text ©2003-2013 www.MilitaryFactory.com • All Rights Reserved • No Reproduction Permitted
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Specifications for the
Consolidated PT-1 Trusty
Primary Trainer Aircraft
Country of Origin: United States
Manufacturer: Consolidated / Dayton-Wright - USA
Initial Year of Service: 1924
Production: 221
Focus Model: Consolidated PT-1 Trusty
Crew: 2
Length: 27.76ft (8.46m)
Width: 34.45ft (10.50m)
Height: 9.84ft (3.00m)
Weight (Empty): 1,806lbs (819kg)
Weight (MTOW): 2,577lbs (1,169kg)
Powerplant: 1 x Wright-Hispano E 8-cylinder water-cooled Vee engine delivering 180hp.
Maximum Speed: 92mph (148kmh; 80kts)
Maximum Range: 350miles (563km)
Service Ceiling: 13,448ft (4,099m; 2.5miles)
Rate-of-Climb: 690 feet per minute (210m/min)
Hardpoints: 0
Armament Suite:
None.
Variants:
TA-3 - Dayton-Wright Production; fitted with Le Rhone C-9 series engine of 80 horsepower.
TA-5 - Single Production Model Example; fitted with Lawrance J-1 series engine; based on the TA-3 production model.
TW-3 - Dayton-Wright and Consolidated production models; Dayton-Wright fitted with water-cooled Wright-Hispano E series engines of 150 horsepower and Consolidated fitted with Wright-Hispano E series engines of 180 horsepower.
PT-1 - Base Series Designation; fitted with Wright-Hispano E series engines of 180 horsepower; 221 examples produced; replaced TW-3.
XPT-2 - PT-1 model fitted with Wright R-790 series radial J-5 engine of 225 horsepower.
TW-8 - Unofficial Prototype Model Designation; known as the "Camel" for the visible hump between instructor and student seating positions.
Consolidated Model 1 - Consolidated Model Designation of the TW-8 prototype.
Operators: Siam and the United States of America.
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