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Aviasud Industries AE-209 Albatross

Micronef ULM Albatros

 

ae209

 

Aviasud Engineering from Fréjus, France developed a 2-seat highwing ULM-aeroplane with push-propeller. Production of the AE-209 Albatros started in 1992, and the Albatros was available with the 2-stroke Rotax 582 or the 4-stroke Rotax 912 engine. The Albatros classique is equipped with a tail wheel; the Albatros tricycle is equipped with a nose wheel or tail wheel. The wings can be folded, which reduces the needed parking space in the hangar.

 

ae209-2
 
After Aviasud went defunct, Micronef ULM had the Albatros built under contract in Poland.
 
Micro-Alb503
Micronef ULM Albatros 503

 

Seats: 2
Stall: 35 kt / 40 mph / 64 kmh
Cruise: 67 kt / 78 mph / 125 kmh
VNE: 100 kt / 115 mph / 185 kmh
Empty Weight: 230 kg / 507 lbs
MTOW Weight: 450 kg / 992 lbs
Climb Ratio: 825 ft/min / 4 m/s
Glide Ratio: 9/1
Take-off distance (50ft obstacle): 820 ft / 250 m
Landing distance (50ft obstacle): 920 ft / 280 m

 
Micronef ULM Albatros 503
Engine: Rotax 503, 52 hp
Wing span: 9.7 m
Wing area: 13.9 sq.m
MAUW: 450 kg
Empty weight: 213 kg
Fuel capacity: 60 lt
Max speed: 155 kph
Cruise speed: 130 kph
Minimum speed: 64 kph
Climb rate: 3.35 m/s
Certification: VZ
Seats: 2
Fuel consumption: 15 lt/hr
Price (1998): 220 221 Fttc

 

 

 

 

 


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