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All-Metal Junkers Airplane, Type F 13

Description: Circular describing the all-metal Junkers airplane, specifically the F 13 type. The primary characteristics of the airplanes are the thick cantilever Junkers wing without stay-wires and the all-metal construction. A description of the design, flight characteristics, and some photographs are provided.
Date: May 1926
Partner: UNT Libraries Government Documents Department
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German Training Airplane, Arado "Ar. S.I."

Description: Circular presenting a description of the Arado Ar. S.I., which is a wireless biplane that is both physically attractive and highly performing. A description of the components, controls, construction, characteristics, flying qualities, drawings, and photographs are provided.
Date: May 1926
Creator: Manigold, G.
Partner: UNT Libraries Government Documents Department
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Two 'Gloster' Airplanes: The 'Grouse II,' - Two-Seat Training Airplane, The 'Grebe II,' Single-Seat Fighter

Description: Circular presenting a description of two airplanes created by the Gloucestershire Aircraft Company, the "Grouse II" and the "Grebe II". A description of the design and flight characteristics as well as the blueprints and photographs of the aircraft are provided.
Date: June 1926
Partner: UNT Libraries Government Documents Department
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Wibault Two-Seat Monoplane 8C2: An All-Metal Pursuit and Observation Airplane

Description: Michel Wibault's two seat monoplane 8C2, is similar to the Parasol pursuit monoplane which preceded it. It has no perishable parts in its structure and needs no special storage or coverings. The sample aeroplane uses a 500 HP Hispano-Suiza engine but can accept a 400-600HP engine from a variety of manufacturers with little difficulty. It uses a two blade tractor propeller.
Date: June 1926
Creator: Serryer, J.
Partner: UNT Libraries Government Documents Department
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The New De Havilland Commercial Airplane: The D.H. 66 With Three Bristol "Jupiter" Engines

Description: 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
Partner: UNT Libraries Government Documents Department
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Farman Monoplane F.170: Commercial Airplane with One 500 HP. Farman Engine

Description: The F.170's engine has won world endurance tests in 1924 and in 1925. It has a semi-thick wing, rigidly braced by oblique struts. This wing is embedded in the top of the fuselage and measures 16.1 by 3.6 meters. The F.170 has a passenger compartment seating eight.
Date: August 1926
Creator: Serryer, J.
Partner: UNT Libraries Government Documents Department
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Heinkel Airplane H.D. 39 for Carrying Newspapers

Description: Circular presenting a description of the Heinkel Airplane H.D. 39, which is a postal airplane that can be used to carry newspapers. Details regarding the design, controls, equipment arrangement, fuel, and flying characteristics are provided.
Date: August 1926
Partner: UNT Libraries Government Documents Department
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Albatros Commercial Airplane L 73

Description: The Albatros was a two engine commercial biplane carrying 2 pilots, eight passengers, and 160 KG of baggage. The framework is metal, the wings having plywood and fabric over the steel tubing. The L 73 was the first 2 engine biplane to be made in Germany.
Date: September 1926
Creator: Rühl, Karl & Wiederhold, Hasso
Partner: UNT Libraries Government Documents Department
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The Farman Commercial Airplane "Jabiru"

Description: Circular presenting a description of the Farman Jabiru F 3X, which was designed to satisfy the requirements of the aerial-navigation companies. Details regarding the power, wing, fuselage, landing gear, construction, engines, fuel tanks, characteristics, performance, drawings, and photographs are provided.
Date: September 1926
Partner: UNT Libraries Government Documents Department
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The Avro "Avian" Airplane: 65 HP. Armstrong-Siddeley "Genet" Engine

Description: The Avro Avian, designed by Mr. Chadwick of A.V. Roe & Co., Ltd. has a very low structural weight (estimated at 750 lbs. empty) but with sufficient structural integrity to be eligible of an "Aerobatics" certificate from the British Air Ministry. It can be configured as a monoplane, or a biplane with seaplane floats. It is designed for economical production.
Date: October 1926
Partner: UNT Libraries Government Documents Department
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The Bristol "Badminton" Airplane

Description: The Bristol Badminton, Type 99 airplane has a radial aircooled engine (a Bristol Jupiter 9 cylinder 450 HP.) and three fuel tanks. It is a single seat biplane weighing 1,840 lbs. empty and 2,460 lbs. loaded. A description of the design, components, photographs, and drawings are provided.
Date: October 1926
Partner: UNT Libraries Government Documents Department
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The De Havilland "Moth"

Description: Officially designated D.H. 60, De Havilland's Moth is a small, simply made, 770 lb. aircraft. It has had it's fittings reduced in number to assist in this, seats 2 (including pilot) and uses a Cirrus 60 HP. engine.
Date: October 1926
Partner: UNT Libraries Government Documents Department
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The A.N.E.C. IV "Missel Thrush" light airplane

Description: A product of the Air Navigation Engineering Co., the Missel Thrush is a light airplane suitable for private ownership. It is a two seat tractor fuselage biplane with single I interplane struts designed by J. Bewsher.
Date: November 1926
Creator: United States. National Advisory Committee for Aeronautics.
Partner: UNT Libraries Government Documents Department
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Avia Pursuit Airplane B.H. 21

Description: Built by the 'Czecho-Slovakian' aircraft factory, AVIA, the B.H. 21, has a top speed of 250 MPH, and carries 120 kg of gasoline and 20 kg of oil, giving it a radius of action of 600-650 km. It is equipped with a Hispano-Suiza engine capable of 300 HP. Details of the design, structure, wings, stabilizer, fuselage, controls, fuel tanks, landing gear, tail, characteristics, performances, drawings, and photographs are provided.
Date: November 1926
Creator: Serryer, J.
Partner: UNT Libraries Government Documents Department
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The Handley Page "Hamlet"

Description: The Hamlet is a three engine high wing monoplane of comparatively small size, fitted with three Bristol Lucifer series IV engines of 130 HP. each, and designed to carry a pilot and four passengers. Details of the layout, wings, slot and flap gear, fuselage, characteristics, performance, and drawings are provided.
Date: November 1926
Partner: UNT Libraries Government Documents Department
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Albert TE-1 Training Airplane

Description: The TE-1 is designed for the economical training of pilots and is a single seat parasol cantilever monoplane. It is nearly entirely made of wood, using a 40 HP. air-cooled Salmson A.D. 9 engine, and weighs 255 kg empty.
Date: December 1926
Partner: UNT Libraries Government Documents Department
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