Technical Report Archive and Image Library (TRAIL) - Browse

ABOUT BROWSE FEED

Combat and bombing airplane, Amiot 120 B 3

Description: The Amiot 120 B 3 is designed as a French combat aircraft. It can accept a variety of engines, and is equipped with 2 machine guns as well as specialized bomb sights and other combat equipment.
Date: January 1, 1927
Item Type: Report
Partner: UNT Libraries Government Documents Department

The Caproni monoplanes "Ca 97" Italian

Description: The Ca 97 is constructed with wings half overhung, a large fuselage, all metal construction, and can be configured with 1 to 3 engines.
Date: October 1, 1928
Item Type: Report
Partner: UNT Libraries Government Documents Department

Liore-Olivier LeO 194 seaplane

Description: It's fuselage is made entirely of wood. It has 6 gasoline tanks each with a capacity of 255 liters. It is a single engine biplane with wings mounted above the body of the seaplane.
Date: April 1, 1927
Item Type: Report
Partner: UNT Libraries Government Documents Department

"Villiers 24" slotted-wing airplane (French)

Description: The Villiers 24 C.A.N. 2 is a night pursuit sesquiplane equipped with the 450 HP direct-drive Lorraine 12 Eb engine. It is characterized by Handley Page slotted wings.
Date: November 1, 1928
Item Type: Report
Partner: UNT Libraries Government Documents Department

The De Havilland "Tiger Moth"a low wing monoplane

Description: With a speed of 186.5 M.P.H. and an operational altitude of 20,000 feet the De Havilland Tiger Moth has caused comment as it was introduced just before the King's Cup race of 1927. It is a single seater with unusual control configuration due to the cramped cockpit area.
Date: October 1, 1927
Item Type: Report
Partner: UNT Libraries Government Documents Department

Meteore 63 commercial seaplane

Description: Societe Provencale de Constructions Aeronautiques, builder of the "Meteore 63" has constructed a three engine (biplane) seaplane which has met conditions for a seaworthy certificate of the first class.
Date: May 1, 1927
Item Type: Report
Partner: UNT Libraries Government Documents Department

Farman two-engine commercial biplane F.180 (French)

Description: The F180 was designed for reliable long distance travel in stages of 500, 1000, 1500 km, carrying loads of 2500, 2000, and 1500 kg respectively. At maximum load it can carry 20 passengers.
Date: October 1, 1929
Item Type: Report
Partner: UNT Libraries Government Documents Department

Levasseur 8 transatlantic airplane

Description: "L'Oiseau Blanc" used by Nungesser and Coli in their unsuccessful attempt to fly from Paris to New York.
Date: August 1, 1927
Item Type: Report
Partner: UNT Libraries Government Documents Department

The C.A.M.S. 54 G.R. transatlantic seaplane (French)

Description: Tested at the end of March, 1928, the C.A.M.S. 54 G.R. was built for the purpose of crossing the Atlantic from Europe by way of the azores. It has a biplane construction with wings mounted above the hull. It is powered by two new series 500 HP. geared Hispano Suiza V type engines.
Date: September 1, 1928
Creator: Ide, John Jay
Item Type: Report
Partner: UNT Libraries Government Documents Department

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 1, 1926
Item Type: Report
Partner: UNT Libraries Government Documents Department

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 1, 1926
Creator: Serryer, J
Item Type: Report
Partner: UNT Libraries Government Documents Department