G1 - STOL




The G1    Francais    English    Espaņol    Italiano    Deutsch

Falling within the categories UL (Ultra Light) and STOL (Shorts Take Off and Landing), with 2 places, 275 Kg empty but very powerful with a Rotax engine of 80 or 100 hp.

Blueprint, click to enlarge

Blueprint, click to enlarge
Dimensions
Reference weight empty 275 kg
Wingspan 9.91 m
Length 6.73 m
Height 2.34 m
Cabin width 1.22 m
Wing area 14.80 mē
Load factor +4/-3g

Equipped with :
Rotax 912 80 hp or 912S 100 hp engine
IVOPROP or Duc Swirl three-bladed propeller,
1.70 m diameter, pitch adjustable on ground
Common control discs brakes
Parking brakes with blockable handle
Filser or Becker radio and transponder
Garmin 295 GPS optionally
Door ventilators
Performances
with engine of
Cruise speed*
Economy cruise speed*
Climb rate to 1000 ft
VNE
Stall speed
Taxiing at take off
Taxiing at landing
Time to 15 meters*
Range
* Depending on the propeller type


80 hp
165 kmh
145 kmh
      1500 ft/min
      210 kmh
      ‹ 50 kmh
      20 m / 60 m
      30 m / 60 m
      50 m / 60 m
      600 / 900 Km

100 hp
172 kmh
150 kmh

Dashboard
Airspeed indicator, altimeter, Med 80 (all engine parameters
with alarm), turn and slip indicator, compass, electrical fuel gauge.


    Fuselage, click to enlarge Aluminium (2024 T3 Alclad) anodised airframe and rigid cabin (just like formula 1 cars) in argon welded steel square tubes 25 CR MO4. Flaps, ailerons and tail-fin are Dacron-lined. The electrical flaps are equipped with trim. This plane is very stable and easy to fly.

Detailed description of G1 STOL
AIRFRAME : ready mounted, entirely metallic with the cabin in welded 25 CRMO4 steel square tubes
WINGS : entirely metallic with wing-tips and cabin-join in polyester (in epox since April, 2008).
STAYS : welded, in chrome molybdenum steel, epox painted.
WING TIPS : aluminium structure lined with thermoplastic DACRON.
ELECTRICAL FLAPS : aluminium structure lined with thermoplastic DACRON.
TAIL-FIN : Full aluminium structure lined with thermoplastic DACRON.
DEPTH : Full aluminium structure.
BELTS : 3 points aviation type.
BASIC INSTRUMENTATION : see details above.
THROTTLE : located to the left of the pilot and the passenger.
CONTROLS : twin rudder pedals, twin control columns, twin throttle controls.
ATTACHMENTS and ENGINE : see details above.
FUELING : with tanks inside the wings, by gravity or by mechanical pump.
BRAKES : hydraulic disc brakes with central lever and parking brake.
MAIN LANDING-GEAR : 2 aluminium half blades.
NOSE LANDING-GEAR : telescopic, fastened on motor mount.
WHEELS : tyres and inner tubes : nose gear 13*5.00/6' - main gear 15*6.00/6'.
DOORS : closings with locks and 2 pneumatic jacks.
Doors, windshield and roof are in LEXAN.