| Aéro Services Guépard | |
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HW100 - 45000
UAW55 - 105000 RRW100 - 175000 PKRR - 7500 |
Aéro Services Guépard Guépy Guépy Role - Microlight cabin monoplane National origin - France Manufacturer - Aéro Services Guépard The Aéro Services Guépard Guépy is a French two-seat microlight cabin monoplane designed and built by Aéro Services Guépard to meet the FAI Microlight standard, it is also sold as a kit of parts for amateur construction. The Guépy is a smaller variant of the Guépard 912 and is a cabin monoplane with a braced high-mounted wing, it has a fixed tricycle landing gear and an enclosed cabin for two sitting in side-by-side configuration. The Guépy is built from welded steel tube with tubular wing spars and aluminium ribs, the Club variant has a fabric covered wing. Although capable of using a range of engines a 80 hp (60 kW) Jabiru 2200 four-stroke or a 64 hp (48 kW) Rotax 582 two-stroke powerplant is normally used. Specifications (Guépy Super) Data from World Directory of Leisure Aviation 2005/2006 and 2015/16 General characteristics Crew: one Capacity: oner passenger Wingspan: 9.7 m (31 ft 10 in) Wing area: 14 m2 (150 sq ft) Empty weight: 240 kg (529 lb) Max takeoff weight: 472.5 kg (1,042 lb) Fuel capacity: 50 litres (11 imp gal; 13 US gal) Powerplant: 1 × Jabiru 2200 , 60 kW (80 hp) Performance Maximum speed: 200 km/h (120 mph, 110 kn) Cruise speed: 170 km/h (110 mph, 92 kn) Stall speed: 60 km/h (37 mph, 32 kn) Rate of climb: 4 m/s (790 ft/min) Aéro Services Guépard Guépard 912 Guépard 912 Role - Microlight cabin monoplane National origin - France Manufacturer - Aéro Services Guépard The Aéro Services Guépard Guépard 912 (English: Cheetah) is a French two-seat microlight cabin monoplane designed and built by Aéro Services Guépard to meet the FAI Microlight standard, it is also sold as a kit of parts for amateur construction. The Guépard 912 is a cabin monoplane with a braced high-mounted wing, it has a fixed tricycle landing gear and an enclosed cabin for two sitting in side-by-side configuration. The Guépard is built from welded steel tube with aircraft fabric covering but is also available with a riveted steel covering. Although capable of using a range of engines with power outputs from 65 to 100 hp (48 to 75 kW) the 80 hp (60 kW) Rotax 912 or the 100 hp (75 kW) Rotax 912S are normally used. Specifications Data from World Directory of Leisure Aviation 2005/2006 and 2015/16 General characteristics Crew: one Capacity: one passenger Wingspan: 9.6 m (31 ft 6 in) Wing area: 14.60 m2 (157.2 sq ft) Empty weight: 282 kg (622 lb) Max takeoff weight: 472.5 kg (1,042 lb) Fuel capacity: 65 litres (14 imp gal; 17 US gal) Powerplant: 1 × Rotax 912S , 75 kW (100 hp) Propellers: 2-bladed composite Performance Maximum speed: 190 km/h (120 mph, 100 kn) Cruise speed: 170 km/h (110 mph, 92 kn) Stall speed: 45 km/h (28 mph, 24 kn) Rate of climb: 5 m/s (980 ft/min) Aéro Services Guépard Guêpe Guêpe Role - Ultralight aircraft National origin - France Manufacturer - Aéro Services Guépard Status - In production The Aéro Services Guépard Guêpe (sometimes just called La Guêpe; English: Wasp) is a French ultralight aircraft, designed and produced by Aéro Services Guépard. The aircraft is supplied fully assembled. Design and development The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a V-strut-braced high-wing, a two seats in tandem open cockpit, conventional landing gear and a single engine in pusher configuration. The aircraft is made from bolted-together aluminum tubing, with a single tube serving as the keel tube. A small cockpit fairing and windshield are optional. Its 8.6 m (28.2 ft) span wing has an aluminium structure with its flying surfaces covered in doped aircraft fabric. Standard engines available are the 64 hp (48 kW) Rotax 582 two-stroke and the 60 hp (45 kW) HKS 700E four-stroke powerplant. Specifications (Guêpe) Data from Bayerl General characteristics Crew: one Capacity: one passenger Wingspan: 8.6 m (28 ft 3 in) Wing area: 12 m2 (130 sq ft) Empty weight: 190 kg (419 lb) Fuel capacity: 60 litres (13 imp gal; 16 US gal) Powerplant: 1 × Rotax 582 four cylinder, liquid-cooled, two stroke, 48 kW (64 hp) Propellers: 2-bladed ground adjustable Performance Maximum speed: 160 km/h (99 mph, 86 kn) Cruise speed: 130 km/h (81 mph, 70 kn) Stall speed: 45 km/h (28 mph, 24 kn) Rate of climb: 2.5 m/s (490 ft/min) Aéro Services Guépard Super Guépard Super Guépard Role - Ultralight aircraft National origin - France Manufacturer - Aéro Services Guépard Status - In production (2016) The Aéro Services Guépard Super Guépard SG 12 (English: Super Cheetah) is a French ultralight aircraft that was designed and produced by Aéro Services Guépard by of Villefranche-de-Rouergue. The aircraft is supplied as a complete ready-to-fly-aircraft. Design and development The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a cantilever single-strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cabin with doors, fixed tricycle landing gear and a single engine in tractor configuration. The aircraft is made from welded steel tubing with its wings made from aluminum sheet. Its 8.5 m (27.9 ft) span wing has an area of 12.75 m2 (137.2 sq ft) and flaps. The standard engine used is the 100 hp (75 kW) Rotax 912ULS four-stroke powerplant. Operational history Reviewer Marino Boric described the design of the welded steel tube fuselage in a 2015 review as assuring "good protection for the crew". Specifications (Super Guépard SG 12) Data from Tacke General characteristics Crew: one Capacity: one passenger Wingspan: 8.5 m (27 ft 11 in) Wing area: 12.75 m2 (137.2 sq ft) Empty weight: 274 kg (604 lb) Gross weight: 450 kg (992 lb) Fuel capacity: 60 litres (13 imp gal; 16 US gal) Powerplant: 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft engine, 75 kW (101 hp) Performance Maximum speed: 198 km/h (123 mph, 107 kn) Stall speed: 62 km/h (39 mph, 33 kn) Rate of climb: 5.8 m/s (1,140 ft/min) Wing loading: 35.3 kg/m2 (7.2 lb/sq ft) |