Aero Boero Series 95

AERO BOERO 95
Four versions of the Aero Boero 95 have been announced, as follows:
Aero Boero 95 Standard. Initial production version, with 95 hp Continental C90 engine, to which details below apply.
Aero Boero 95A De Lujo. Production version with 100 hp Continental O-200-A engine.
Aero Boero 95A Fumigador. Agricultural version with 100 hp O-200-A engine and dusting or spraying equipment, including a chemical tank of 55 Imp gallons (250 litres) capacity. In production.
Aero Boero 95B. With 150 hp engine. Construction begun in 1953.
A second series of ten Aero Boero 95/95A aircraft was under construction in mid-1965. Plans exist for production under licence in Peru and Uruguay.
Type: Three-seat light aircraft.
Wings: Braced high-wing monoplane. Wing section NACA 23012. Aspect ratio 6-5. Constant chord of 5 ft 3.5 in (1-61 m). Dihedral 1° 45'. Incidence 3° at root, 1° at tip. Light alloy structure, fabric-covered. Two separate streamlined bracing struts each side. Fabric-covered light alloy ailerons and flaps.
Fuselage: Welded steel-tube structure, fabric-covered.
Tail Unit: Wire-braced welded steel-tube structure, fabric-covered.
Landing Gear: Non-retractable tail-wheel type. Shock-absorption by helicoidal springs inside fuselage. Main wheel tyre size 600 x 6, pressure 18 lb/sq in (1-27 kg/cm2). Hayes brakes.
Power Plant: One 95 hp Continental C90-8F four-cylinder horizontally-opposed air-cooled engine, driving a Sensenich metal two-blade fixed-pitch propeller, diameter 6 ft 2 in (1-88 m). Fuel in two tanks in wings, with total capacity of 24 Imp gallons (110 litres). Oil capacity 10 Imp gallon (4-5 litres).
Accommodation: Normal accommodation for pilot and two passengers in enclosed cabin.
Equipment: Provision for dual controls, cropdusting and spraying equipment.
Jane's All The World's Aircraft / 1965/1966 EDITION - Edited by John W. R. Taylor
Dimensions, external:
Wing span - 34 ft 2.5 in (10-42 m)
Length overall - 22 ft 7.5 in (6-90 m)
Height overall - 6 ft 10 in (2-10 m)
Wheel track - 6 ft 8.75 in (205 m)
Wheelbase - 16 ft 9 in (5-10 m)
Areas:
Wings, gross - 176-1 sq ft (16-36 m2)
Ailerons (total) - 20-45 sq ft (1-90 m2)
Flaps (total) - 17-97 sq ft (1-67 m2)
Fin - 10-76 sq ft (100 m2)
Elevators - 27-10 sq ft (2-52 m2)
Weights and Loadings:
Weight empty, equipped - 930 lb (422 kg)
Max T-O weight - 1,543 lb (700 kg)
Max wing loading - 8-60 lb/sq ft (42 kg/m2)
Max power loading - 16-22 lb/hp (7-36 kg/hp)
Performance (at max T-O weight, except where indicated):
Max level speed - 127 mph (205 kmh)
Max cruising speed - 106 mph (170 kmh)
Econ cruising speed - 100 mph (160 kmh)
Stalling speed, flaps down - 30 mph (48 kmh)
Rate of climb at S/L - 1,000 ft (300 m) min
Service ceiling - 17,000 ft (5,200 m)
T-O run, full load - 380 ft (115 m)
T-O run, two persons - 250 ft (75 m)
T-O to 50 ft (15 m), two persons - 500 ft (150 m)
Landing from 50 ft (15 m), two persons - 500 ft (150 m)
Landing run, two persons, heavy braking - 150 ft (45 m)
Range with max fuel - 600 miles (960 km)
Jane's All The World's Aircraft / 1965/1966 EDITION - Edited by John W. R. Taylor
AERO BOERO - AERO TALLERES BOERO SRL
Head Office: Boulevard H. Irigoyen 505, Morteros, Cordoba
This company is producing a three-seat allmetal light monoplane, known as the Aero Boero 95, of which a prototype flew for the first time on March 12, 1959.
Also nearing completion in mid-1965 was the prototype of a larger, four-seat aircraft known as the Aero Boero 180. In the design study stage is a four/six-seat light executive transport known as the Aero Boero Turbo, powered by two unspecified Turbomeca gas-turbine engines.