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  2. Langley Aerodrome - Wikipedia

    en.wikipedia.org/wiki/Langley_Aerodrome

    The Aerodrome had a primitive control system that included a cruciform tail and a centrally-mounted rudder. [3] Langley again used a houseboat catapult for launch. He chose his chief engineer, Charles M. Manly, to ride the aircraft and operate the controls as best he might. On the first flight attempt, October 7, 1903, the craft failed to fly ...

  3. Cruciform tail - Wikipedia

    en.wikipedia.org/wiki/Cruciform_tail

    The cruciform tail is an aircraft empennage configuration which, when viewed from the aircraft's front or rear, looks much like a cross. The usual arrangement is to have the horizontal stabilizer intersect the vertical tail somewhere near the middle, and above the top of the fuselage .

  4. Category:Cruciform tail aircraft - Wikipedia

    en.wikipedia.org/wiki/Category:Cruciform_tail...

    This page was last edited on 2 December 2016, at 17:32 (UTC).; Text is available under the Creative Commons Attribution-ShareAlike 4.0 License; additional terms may apply.

  5. Aerion AS2 - Wikipedia

    en.wikipedia.org/wiki/Aerion_AS2

    The fuselage has pronounced area ruling at its mid-section, and the cruciform horizontal stabilizer allows for a shorter airplane, down from 180 to 145 ft (55 to 44 m). [23] The design is lighter with a 139,000 lb (63 t) gross weight, allowing a payload of 8,000 lb (3.6 t) and 70,000 lb (32 t) of fuel, used to trim weight and balance during the ...

  6. List of aircraft structural failures - Wikipedia

    en.wikipedia.org/wiki/List_of_aircraft...

    Faulty repair after same plane suffered a tailstrike: the rear bulkhead failed which caused the tail fin to fall off and rupture all four hydraulic systems. The crash remains the deadliest single-aircraft accident in aviation history. 1987-11-28 South African Airways Flight 295: Indian Ocean, 134 nautical miles (248 km) north-east of Mauritius,

  7. de Havilland Canada DHC-3 Otter - Wikipedia

    en.wikipedia.org/wiki/De_Havilland_Canada_DHC-3...

    The de Havilland Canada DHC-3 Otter is a single-engined, high-wing, propeller-driven, short take-off and landing aircraft developed by de Havilland Canada.It was conceived to be capable of performing the same roles as the earlier and highly successful Beaver, including as a bush plane, but is overall a larger aircraft.

  8. Empennage - Wikipedia

    en.wikipedia.org/wiki/Empennage

    The empennage of an Atlas Air Boeing 747-200. The empennage (/ ˌ ɑː m p ɪ ˈ n ɑː ʒ / or / ˈ ɛ m p ɪ n ɪ dʒ /), also known as the tail or tail assembly, is a structure at the rear of an aircraft that provides stability during flight, in a way similar to the feathers on an arrow.

  9. Santos-Dumont Demoiselle - Wikipedia

    en.wikipedia.org/wiki/Santos-Dumont_Demoiselle

    The first aircraft of the type was the Santos-Dumont No. 19, which was built in 1907 to attempt to win the Grand Prix d'Aviation offered for a one kilometre closed-circuit flight. Powered by a 15 kW (20 hp) air-cooled Dutheil & Chalmers flat-twin engine mounted on the leading edge of the wing, it had a wingspan of 5.1 m.