Fuselage and wings
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The fuselage consists of a lattice of chrome-molybdenum steel tubes connected to the light alloy tail beam. Light alloy right and left half-wings, light alloy stabilizer and rudder. The moving parts: ailerons, flaps, rudder and stabilizer are of |
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light alloy covered by 90 g/Mē Dacron. The transparent front and cabin roof are of 2 mm lexan. The doors are of square light alloy tubes with the transparent parts of 2 mm lexan. The wingtips and stabilizer tips are of composite material. |
Exterior
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Steel front undercarriage, telescopic suspension with dolly wheel steerable by compass. Leaf spring rear undercarriage of variable thickness harmonic steel. Wheels with hydraulic disc brakes. Faired chrome-molybdenum uprights. Wheel fairings. Exhaust pipe. Engine cowling. Engine group complete with cooling liquids. G.T. armoured wooden two-blade propeller with spinner. |
Electrical system
| 12V, 18Ah battery; Light strobe; 15A alternator integrated with the engine; Regulator; Starter motor; Services protection; Main and services switch. |
Fuel system
| Gravity feed; Two wing tanks of 2x41 l + 1 tank (recovery sump) of 5 l, total 87 l; Mechanical pump integrated in the engine; Quick drain; Electric safety pump (anti-vapour lock). |
