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 Collection: National Advisory Committee for Aeronautics Collection
Vojenska-Smolik S.16 airplane : all-metal long-distance observation bi-plane

Vojenska-Smolik S.16 airplane : all-metal long-distance observation bi-plane

Date: March 1, 1927
Creator: unknown
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The Fairchild "all-purpose" cabin monoplane

The Fairchild "all-purpose" cabin monoplane

Date: October 1, 1927
Creator: unknown
Description: The Fairchild "all-purpose" is a 4 seater with a large luggage compartment, good visibility, and can be configured for surveying work. It is rated at 200 HP. at 1800 R.P.M., but can deliver over 220 HP.
Contributing Partner: UNT Libraries Government Documents Department
Preliminary report on the problem of the atmosphere in relation to aeronautics

Preliminary report on the problem of the atmosphere in relation to aeronautics

Date: January 1, 1917
Creator: Marvin, Charles F
Description: A report to the Weather Bureau, Washington DC, from the chairman of the Subcommittee on the Atmosphere in Relation to Aeronautics describing the activities accomplished and the proposal of work to be undertaken by the subcommittee.
Contributing Partner: UNT Libraries Government Documents Department
The Fokker "Trimotor F VII" commercial transport monoplane

The Fokker "Trimotor F VII" commercial transport monoplane

Date: June 1, 1928
Creator: unknown
Description: Directly developed from the single engined type F VII ten passenger monoplanes, The Fokker Trimotor closely follows the commercial aircraft that preceded it. It has three Wright Whirlwind air-cooled engines, rated at 200 HP each.
Contributing Partner: UNT Libraries Government Documents Department
Savoia seaplane S.55 : military or commercial

Savoia seaplane S.55 : military or commercial

Date: March 1, 1927
Creator: unknown
Description: The S.55 is a two engine twin hull seaplane built by Societa Idrovolanti Alta Italia (Seaplane Company of Upper Italy). The S.55 (Santa Maria) is to be used for an around the world flight In 1927. It will have a useful load of 7,500 lbs. and a cruising speed of 100 MPH.
Contributing Partner: UNT Libraries Government Documents Department
Wibault two-seat monoplane 8C2 : an all-metal pursuit and observation airplane

Wibault two-seat monoplane 8C2 : an all-metal pursuit and observation airplane

Date: June 1, 1926
Creator: Serryer, J
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.
Contributing Partner: UNT Libraries Government Documents Department
The Boulton and Paul "Bugle" airplane : day bomber

The Boulton and Paul "Bugle" airplane : day bomber

Date: December 1, 1926
Creator: unknown
Description: The Bugle is a twin engine tractor biplane. It features two Jupiter engines and oleo-pneumatic landing gear. Its maximum speed is 120 MPH.
Contributing Partner: UNT Libraries Government Documents Department
The Fokker "Universal" commercial airplane

The Fokker "Universal" commercial airplane

Date: May 1, 1928
Creator: unknown
Description: Equipped with a Wright Whirlwind 200-230 H.P. Engine, the Universal can be configured with floats or wheels and seats 4-6 passengers.
Contributing Partner: UNT Libraries Government Documents Department
Bleriot combat monoplane 127 (French)

Bleriot combat monoplane 127 (French)

Date: November 1, 1928
Creator: unknown
Description: The 127 is a cantilever monoplane without external bracing. It is designed to accompany and protect bombardment and observation aircraft.
Contributing Partner: UNT Libraries Government Documents Department
The Handley Page "Hamlet"

The Handley Page "Hamlet"

Date: November 1, 1926
Creator: unknown
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, designed to carry a pilot and four passengers.
Contributing Partner: UNT Libraries Government Documents Department