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Steerable telescopic nose strut (steering horn).
- Heat-treated tapered leaf-spring main landing gear.
- Wheels with hydroconic brakes.
- Main landing gear tyres 8.00/6” 6Ply.
- Streamlined alloy-steel wing struts.
- Alloy-steel exhaust system.
- Engine cowling.
- Powerplant complete with fluids.
- G.T. wooden two-blade propeller with spinner or, by request,
three-bladed IDROVARIO variable pitch propeller.
FUSELAGE AND WINGS
The fuselage is comprised of a welded tubular alloy-steel
cockpit structure and riveted aluminium alloy tail cone.
The wings and horizontal & vertical stabilizers are
riveted aluminium alloy. The slats are in carbon fiber.
All movable surfaces: ailerons, flaps, rudder and elevator
are aluminium alloy covered with 90gr/m2
DacronTM fabric.
The windshield, door windows and cockpit roof are 2 mm transparent
polycarbonate. The cockpit doors are of square aluminium
alloy tubing. The wingtips and stabilizer tips are composite.
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