Dassault Falcon 20 (ICAO FA20)
Prepared 18 October 2026.
Geometry source: APS Aviation / Transport Canada report TP 14716E, Falcon 20 Trials to Examine Fluid Removed from Aircraft During Takeoff with Ice Pellets, Figure 2.2, printed page 8 / PDF page 26. Public author archive at RHEA Canada.
https://rheacanada.ca/wp-content/uploads/2020/11/TP-14716E-Final-Version-1.0.pdf
Manufacturer dimension cross-check:
https://www.dassault-aviation.com/en/passion/aircraft/civil-dassault-aircraft/mystere-falcon-20-200/
The report specifies 16.32 m span and 17.15 m length; Dassault lists 16.30 m and 17.15 m. The reproduced plan view has unequal longitudinal and transverse scales. The transverse axis is normalised to the report dimensions before uniform overall scaling. Smooth native SVG paths follow the fuselage, swept wings, wing fences, rear nacelles and pylons, and swept horizontal tail. Transparent cockpit glazing and restrained nacelle/control-surface cuts. Original CF700-style nacelles without research booms, military equipment or winglets. Outline checked by source overlay; overall span/length ratio checked against published dimensions. Engine conversions vary. Decorative artwork, not an engineering drawing.
