The LoCamp is intended to resemble a 1930s style light aircraft. It features a cantilever
low-wing, a two-seats-in-
tandem open cockpit with
polycarbonate windscreens, fixed
conventional landing gear and a single engine in
tractor configuration. The aircraft
fuselage is made from welded steel tubing, with the wing built from wood or optionally
aluminium sheet and its flying surfaces covered in
doped aircraft fabric. Its span wing employs a
NACA 4416 airfoil, has an area of and mounts
flaps. The standard engine available is the
Rotec R2800 four-stroke radial engine, although the
Walter Mikron MIIIC was under evaluation by the manufacturer. In 2015 the manufacturer was considering producing a fully assembled
special light-sport aircraft version. ==Variants==