The invention relates to a release lever, especially for a parachute rescue system of a light aircraft, with a jet engine mounted on the fuselage, the release lever (1) comprising a handle (7) arranged in the body mounted to the fuselage structure in the aircraft (1) cabin. characterised in that the body consists of a console (4) and a rotatable lever (5), tiltable from the resting position to the operating position, rotatably mounted in the console (4), wherein the console (4) is mounted to the aircraft (2) fuselage structure, and the handle (7) is seated inside the rotatable lever (5) and protrudes beyond the rotatable lever (5), wherein the handle (7) is provided with a locking mechanism (3) which prevents pulling the handle (7) out of the rotatable lever (5) before it is tilted from the resting position to the operating position.
RELEASE LEVER FOR A PARACHUTE RESCUE SYSTEM
AUSLÖSUNGSHEBEL FÜR EIN FALLSCHIRMRETTUNGSSYSTEM
LEVIER DE DÉGAGEMENT POUR UN SYSTÈME DE PARACHUTE DE SECOURS
2020-02-12
Patent
Electronic Resource
English