|The S.A.I. produces the aircraft ultralight version (ULM) G 97 Spotter and G 97 V Spotter certified on the basis of V.EL regulation of ENAC - RAI.|
|Characteristics of the G97 Spotter - ULM version.|
Maximum visibility like an helicopter. Ease of maintenance and disassembly, low cost, little sensitive to air turbulence, high
internal comfort, large baggage comportment..
Un-braced high wing, VG1-13H high lift airfoil designed for the G97, constant chord, dihedral 1°, incidence 2°.30’, no twist, wing detachable
for storage and transportation, integral leading edge fuel tank (2x35 litres).
Large transparent nose section with two large transparent doors, rear nacelle for engine installation behind the wing (pusher propeller).
Full dual controls and one central throttle, differential Frise ailerons, stabilator tailplane with anti-balance/trim tab, electrically actuated trim tab and slotted flaps covering 71% of wing span.
All-metal basic structure of aeronautical aluminium alloy except tailplane and rudder, Dacron covered,and wing-fuselage fairing, wing and vertical fin tips, engine nacelle and tail cone which are of Fiberglas.
Fixed tricycle, hydraulic disk brakes, nose wheel with rubber shock-absorber.Main gear in one spring of carton-Fiberglas, mounted under the fuselage structure with four bolts for easy disassembly.
One 80 hp Rotax 912 (*), four-cylinder four-stroke liquid/air cooled engine.
Propeller of maximum diameter of 172 cm .
Basic version: Tonini propeller 166cm/145cm diameter to pitch ratio.
(*) Rotax 912 of 100 hp is foreseen.
Characteristics of the G97
V Spotter - Certified