A fitting to mount an engine to a wing of an aircraft. The fitting includes a body with a first end and a second end. A first pocket is positioned at the first end with the first pocket sized to receive the forward engine mount fitting. A second pocket is positioned at the second end with the second pocket sized to receive a strut of the wing of the aircraft. The body includes a first section and a second section that are connected together.
Engine Mount Fitting
27.03.2025
Patent
Elektronische Ressource
Englisch
| IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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