The Amiot S.E.C.M. 110 C.1 : A Single-Seat Pursuit Monoplane (open access)

The Amiot S.E.C.M. 110 C.1 : A Single-Seat Pursuit Monoplane

Circular presenting a description of the Amiot S.E.C.M. 110 C.1, which is a single-seat pursuit monoplane. Some of the design principles that the aircraft was built from are provided. A description of the design, components, dimensions, flight characteristics, and photographs are provided.
Date: July 1929
Creator: unknown
System: The UNT Digital Library
The Avro "Gosport," 504 R: A New Training Airplane (open access)

The Avro "Gosport," 504 R: A New Training Airplane

Circular describing the Avro Gosport 504 R, which is a new training airplane that is lighter than other Avro training airplanes but is strong enough to withstand rough handling that may be encountered in training. Details of the fuselage, construction, ailerons, tail, struts, landing gear, fuel tanks, performance, characteristics, and photographs are provided.
Date: July 1927
Creator: unknown
System: The UNT Digital Library
The Gloster "Gambet" Airplane: A Deck-Landing Ship's Fighter Fitted With a 420 HP. Bristol Jupiter VI Engine (open access)

The Gloster "Gambet" Airplane: A Deck-Landing Ship's Fighter Fitted With a 420 HP. Bristol Jupiter VI Engine

Circular detailing the Glouster "Gambet", which is a new single-seat fighter for use from aircraft carriers. A description of the design, components, characteristics, photographs, and drawings are provided.
Date: July 1927
Creator: unknown
System: The UNT Digital Library
The Bernard 20 C.1 (French): A Single-Seat Pursuit Monoplane (open access)

The Bernard 20 C.1 (French): A Single-Seat Pursuit Monoplane

Circular presenting a description of the Bernard 20 C.1, which is made of wood and has four main parts: a one-piece wing with a fuselage in the middle, a rear section with the tail surfaces, an engine mount, and a landing gear.
Date: July 1929
Creator: unknown
System: The UNT Digital Library
René Couzinet Monoplane (French) (open access)

René Couzinet Monoplane (French)

Having been designed as a long range aircraft, it carries 6200 liters of fuel and 280 liters of oil and has three propeller groups, each with a 180 HP Hispano-Suiza engine capable of 230 HP. Details of the design, wings, ailerons, fuselage, fuel tanks, landing gear, characteristics, performances, tests, drawings, and photographs are provided.
Date: July 1928
Creator: Serryer, J.
System: The UNT Digital Library
The New De Havilland Commercial Airplane: The D.H. 66 With Three Bristol "Jupiter" Engines (open access)

The New De Havilland Commercial Airplane: The D.H. 66 With Three Bristol "Jupiter" Engines

The D.H. 66, constructed at Stag Lane Works of the De Haviland Aircraft Company built for Imperial Airways, Ltd. The fuselage has an all steel construction while the wings are made with box spars of wood and spruce ribs. It has a biplane tail and encloses the stabilizer trimming gear in a casing which serves to streamline the rear portion of the fuselage, but which is not part of the main structure. It weighs 9060 lbs. empty and 2500 lbs. after fueling with a total loaded weight of 14,700 lbs.
Date: July 1926
Creator: unknown
System: The UNT Digital Library
The Blackburn "Sprat": A Training Airplane Convertible Into Landplane or Seaplane (open access)

The Blackburn "Sprat": A Training Airplane Convertible Into Landplane or Seaplane

The Sprat is similar the Blackburn Swift and Dart models but is designed as a trainer. It is powered with a smaller 275 HP Rolls-Royce Falcon engine. It is a 2 seat biplane with equal sized upper and lower wings. It can quickly convert from a land to a seaplane.
Date: July 1926
Creator: unknown
System: The UNT Digital Library