The invention relates, in particular, to an aircraft for flight training, the aircraft comprising, in particular, a fuselage (1) which extends along a longitudinal axis (D) of the aircraft, the fuselage (1) comprising a front end forming an aircraft nose (8) and a rear end, the aircraft (1) comprising a cockpit (2), a wing (3), a landing gear (4), at least one turboprop engine (5) and a tail (6). The aircraft further comprises two canard wings (7) attached to the fuselage (1) in the front part of the aircraft, on either side of the nose (8). The tail (6) comprises two elements (60) forming a V, symmetric about the longitudinal axis (D) of the aircraft, and the turboprop engine (5) is located above the fuselage (1) upstream from the tail (6) and in a plane of symmetry comprising the longitudinal axis (D) of the aircraft, between the two elements (60) forming a V of the tail (6).


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    Titel :

    AVION POUR LA FORMATION AU PILOTAGE


    Weitere Titelangaben:

    AIRCRAFT FOR FLIGHT TRAINING
    FLUGZEUG FÜR FLUGTRAINING


    Beteiligte:

    Erscheinungsdatum :

    16.04.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G09B Unterrichts- oder Vorführungsgeräte , EDUCATIONAL OR DEMONSTRATION APPLIANCES



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