Anderson EA-1 Kingfisher             

Earl Anderson, a Boeing 747 Captain, spent nine years developing the EA-1 Kingfisher at a cost of $5,500, and first flew it on 24 April 1969. At that time, it used a 100-hp Continental 0-200, similar to the Volmer VJ-22 Sportsman, which served as a design inspiration. Later, Anderson switched to a 115-hp Lycoming 0-235-C1, and by January 1975 had logged more than 600 hours on the amphibian. Seating two people side-by-side in an enclosed cabin, the Kingfisher uses standard Piper J-3 Cub wings, with tip floats of mahogany and plywood covered with fiberglass. The fuselage also is wooden, the framework covered with plywood and fiberglass. The landing gear is retractable.

200 sets of plans had been sold by 1978.

Gallery

Engine: 100 hp Continental O-200
Prop: 2 blade fixed pitch, wood
Max speed: 96 mph
Cruise speed: 85 mph
Range: 322 miles
Empty weight: 1032 lb
MTOW: 1540 lb
Wingspan: 36 ft 2 in
Length: 23 ft 6 in
Wing area: 178.5 sq.ft

Engine: Lycoming O-235, 115 hp.
Span 37 ft l in.
Wing Area 185 sq.ft.
Height 8 ft 4 in.
Length 23 ft 7 in.
Gross Weight 1600 lb.
Empty Weight 1092 lb.
Fuel 20-26 USgal.
Vmax 113 mph.
Cruise 90 mph.
Climb 650 fpm.
Stall 42 mph.
Ceiling 13,500 ft
Range 330 sm.
Seats 2.
Landing gear:
Retractable tail wheel.

Engine: Continental O-200A, 100 hp.
Span 37 ft l in.
Wing Area 185 sq.ft.
Height 8 ft 4 in.
Length 23 ft 7 in.
Gross Weight 1600 lb.
Weight empty: 1050 lbs.
Fuel cap: 20 USG.
Speed max: 95 mph.
Cruise: 85 mph.
Range: 280 sm.
Stall: 42 mph.
ROC: 700 fpm.
Take-off dist: 1000 ft (land), 2000 ft (water).
Seats 2.
Landing gear: Retractable tail wheel.

Anders Kiev / Russian Empire Airship Kiev

Russian non-rigid dirigible “Kiev” «Киев» was designed and constructed by Fedor Ferdinandovich Anders [Федор Фердинандович АНДЕРС].

The first flight is given as August 6, 1911 in the city of Kiev. It is claimed that the non-rigid “Kiev” was the first Russian dirigible built with private funds that carried passengers commercially.

Engine: 1 x 50 hp
Envelope: 1000 cu.m
Length: 35.5 m
Diameter: 7 m

Andreasson BA-6

Designed by Björn Andreasson and first flown in 1955, the BA-5 single-seat aerobatic sports monoplane was developed primarily for amateur construction.

The BA-6 is of all-wood construction and, with the exception of the fabric-covered control surfaces, has plywood covering. Fully aerobatic, The BA-6 has a Cessna-type spring-steel cantilever landing gear. Landing flaps are fitted.

SE-BXX and SE-BXY

The first two built were fitted with Continental A65 65hp engines and the airframe will take the Continental C85.

Engine: Continental A65, 65 hp
Wingspan: 23 ft
Length: 16 ft 5 in
Height: 5 ft
Max speed: 145 mph
Landing speed: 34 mph
Time to 20,000ft: 6 min
Range: 1200 mi

Andreasson BA-4 / Crosby Aviation Ltd BA-4B

Designed by Björn Andreasson as a homebuilt in 1944 as the single-seat biplane BA-4 was built at Malmo Aviation’s plant at Bulltofta, Sweden.

In 1966 it was designated as the BA-4B c/n 1 registered SE-XBS and was powered by a Continental O-200-A.

The rights to the design were sold to Peter J.C. Phillips who formed Crosby Aviation Ltd to market kits and plans of the BA-4B. The prototype was imported to the UK in 1968 as G-AWPZ.

Andreasson BA-4B

Three aircraft were laid down for initial sales at Knutsford, Cheshire, UK, and all were completed, including G-AYFU, V and W.

Crosby Aviation built G-AYFV

Crosby Aviation offered two versions: the BA-4B with a Rolls-Royce/Continental O-200-A; and the Super BA-4B with a Rolls-Royce/Continental O-240-A.

Gallery

BA-4B
Engine: Rolls-Royce/Continental O-200-A
Wingspan: 18.06 ft
Length: 15.04 ft
Empty Weight: 330 kg / 728 lbs
MTOW Weight: 450 kg / 992 lbs
Stall: 52 kt / 60 mph / 96 kmh
Cruise: 113 kt / 130 mph / 210 kmh
VNE: 130 kt / 149 mph / 240 kmh
Take-off distance (50ft obstacle): 890 ft / 270 m
Landing distance (50ft obstacle): 1530 ft / 465 m

Super BA-4B
Engine: Rolls-Royce/Continental O-240-A
Wingspan: 18.06 ft
Length: 15.06 ft

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

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

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

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