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).
AVION POUR LA FORMATION AU PILOTAGE
AIRCRAFT FOR FLIGHT TRAINING
FLUGZEUG FÜR FLUGTRAINING
2025-04-16
Patent
Electronic Resource
French
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