Aircraft resources

Spratt 103

Part 103

Bernard Geffray (designer/plans publisher via spratt103.com; French Ultralight pendular / multi-axis registrations noted on site)

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Manufacturer
Bernard Geffray (designer/plans publisher via spratt103.com; French Ultralight pendular / multi-axis registrations noted on site)
Model
Spratt 103
Category
Part 103
Seats
1
Cruise Speed
64 mph
Years Produced
1998–present
Useful Load
—
Fuel Burn
—
Production Status
In production
Type
Single-seat ultralight of pendular / free-wing type with steering-wheel control; stainless-steel tube fuselage; free autostable rigid wings collectively and differentially controlled; plans-built (kit later contemplated on Q&A); recommended ~25 hp injected 4-stroke (Honda IGX800 cited) or lighter 2-stroke options

Part 103 eligibility

Manufacturer characteristic page states the design complies with the USA Part 103, English SSDR and German regulations, and is registered in France as pendular and multi-axis Ultralight. Listed empty weight 80 to 90 kg without engine (+15 kg / 2-stroke to +45 kg / 4-stroke). Fuel tank listed maxi 25 litres (~6.6 US gal) — above the typical Part 103 5 US gal fuel limit unless a US-compliant tank is fitted; finished-aircraft compliance therefore requires attention to fuel quantity as well as weight/speed. Actual eligibility depends on the finished aircraft meeting 14 CFR Part 103 limits (not independently verified here).

This note is reference information from the listed sources. It is not a determination by Fly For Less Aviation.

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