A control lever assembly for controlling an aircraft system. The lever includes: a housing having an outer side and an aperture defined by a rim; and a control lever extending through the aperture and movable in the aperture; the control lever having an outer cover member arranged to slide over the outer side of the housing and cover the rim throughout the range of movement of the control lever.
Control lever assembly for controlling an aircraft system
30.07.2024
Patent
Elektronische Ressource
Englisch
Control lever assembly for controlling aircraft system
Europäisches Patentamt | 2023
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Europäisches Patentamt | 2023
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Europäisches Patentamt | 2023
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