Essentially a developed Voisin 5 (the initial letters signifying ‘Voisin Ivanov’) designed in 1915. From March 1915 one year’s output of VI type was intended to total about 150, though this quantity not completed until mid-1918.
Aircraft
Anatra DS Anasal
Reconnaissance, Russia, 1916
Engine: Salmson 9 U, 148 hp
Length: 26.575 ft / 8.1 m
Wingspan: 37.467 ft / 11.42 m
Wing area: 398.268 sqft / 37.0 sqm
Max take off weight: 2566.6 lb / 1164.0 kg
Wing load: 6.36 lb/sq.ft / 31.00 kg/sq.m
Max. speed: 78 kts / 144 km/h
Service ceiling: 14108 ft / 4300 m
Endurance: 4 h
Crew: 2
Armament: 2x MG
Anatra D.I Anadis
Experimental fighter aircraft, Russia, 1916
Engine: Salmson 9U (Canton-Unné), 148 hp
Length: 25.427 ft / 7.75 m
Wingspan: 37.402 ft / 11.4 m
Wing area: 398.268 sqft / 37.0 sqm
Max take off weight: 2568.8 lb / 1165.0 kg
Weight empty: 1466.3 lb / 665.0 kg
Max. speed: 83 kts / 153 km/h
Wing load: 6.36 lb/sq.ft / 31.00 kg/sq.m
Crew: 1
No. built: 1
Anatra D Anade
The Anatra D reconnaissance aircraft of 1915 was a German Albatros derivative, with a rotary engine.
Engine: Gnome Monosoupape, 99 hp
Length: 25.262 ft / 7.7 m
Wingspan: 37.73 ft / 11.5 m
Wing area: 376.74 sqft / 35.0 sqm
Max take off weight: 1907.3 lb / 865.0 kg
Max. speed: 71 kts / 132 km/h
Service ceiling: 13123 ft / 4000 m
Wing load: 5.13 lb/sq.ft / 25.00 kg/sq.m
Endurance: 4 h
Armament: 1x MG
Anatra
Zavod A.A. (for Arturo Antonovich) Anatra was founded at Odessa in 1913. Important during First World War, with factories at Odessa and Simferopol, Ukraine, by 1917 the company was building their own designs, plus Voisins and Nieuports, to a total monthly output of 80.
The Companys activities ceased in the early 1920s.
Anahuac TA-70 Tauro
Designed in Mexico as an ag aircraft, the prototype Tauro 300 first flew on 3 December 1968. An improved Tauro 350 with more powerful radial engine (350 hp) followed into production from 1977.
Tauro 300
Engine: Jacobs R-755-A2M1, 300 hp
Wing span: 37 ft 6.5 in / 11.44 m
Length: 26 ft 11.25 in / 8.21 m
Max cabin length: 3 ft 8 in / 1.12 m
Max cabin width: 2 ft 10 in / 0.86 m
Max cabin height: 4 ft 3 in / 1.295 m
Empty weight: 1973 lb / 895 kg
MTOW: 3542 lb / 1606 kg
Max cruise SL: 78 kt / 90 mph / 145 kph
Max ROC SL: 500 fpm / 152 m/min
Service ceiling: 14,000 ft / 4250 m
Range max fuel: 202 nm / 233 mi / 375 km
Seats: 1
Hopper capacity: 230 USG / 191 Imp.G / 870 lt / 1764 lb / 700 kg
Anahuac
Fabrica de Aviones Anahuac SA, Mexico, was established in 1966 to develop agricultural aircraft suited to national requirements. The rototype Tauro 300 first flew on 3 December 1968. The improved Tauro 350 with a more powerful radial engine (350 hp) followed into production from 1977.
AMX International
Founded by Aermacchi and Aeritalia of Italy and Embraer of Brazil to develop the AMX close-air- support, interdiction and reconnaissance jet (known as A-1 in Brazil), first flown May 1984 and delivered from 1989 (192 delivered by 1998).
AMS Flight Carat A
Retractable landing gear, folding propeller, low-noise four-stroke engine, good gliding performance, suitable for trailering, one-man assembly possible, comfortable cockpit.
Stall: 43 kt / 50 mph / 80 kmh
Cruise: 108 kt / 124 mph / 200 kmh
VNE: 135 kt / 155 mph / 250 kmh
Empty Weight: 325 kg / 717 lbs
MTOW Weight: 470 kg / 1036 lbs
Climb Ratio: 700 ft/min / 3.5 m/s
Glide Ratio: 35
Take-off distance (50ft obstacle): 1400 ft / 428 m
Amphibian Airplanes of Canada Super Petrel
Engine: Rotax 912S, 100 hp
HP range: 65-100
Length: 19.3 ft
Wing span: 30.3 ft
Wing area: 196 sq.ft
Empty weight: 695 lb
Gross weight: 1320 lb
Fuel capacity: 27 USG
Cruise: 103 mph
Stall: 34 mph
Range: 580 sm
Rate of climb: 1000 fpm
Takeoff dist: 240 ft
Landing dist: 360 ft
Cockpit width: 42 in
Landing gear: retract, nose
