Beechcraft King Air A100 (ICAO BE10)
Prepared 16 October 2026.
Geometry source: Raytheon Aircraft Engineering, A100 Supplemental Operational Data page 9-4, drawing A100-607-3; reproduced in NTSB Aircraft Performance attachment 4, PDF page 2.
https://data.ntsb.gov/Docket/Document/docBLOB?FileExtension=.PDF&FileName=Aircraft+Performance+13+-+Attachment+4+to+Airplane+Performance+Study-Master.PDF&ID=40178980
The manufacturer top view determines fuselage, wing, nacelle, propeller and conventional horizontal-tail geometry. Hand-traced smooth native SVG curves, with the cleaner left half mirrored about the fuselage centreline to remove fax skew. Uniform scale preserves reference proportions; no winglets or T-tail. Cockpit and restrained nacelle/control-surface detail are transparent cuts. Outline checked against an overlay of the reference.
Decorative identification artwork, not an engineering drawing.
