Originally flown as the DR.200 which was a variant of the earlier DR.1050M1 with a strengthened wing and longer fuselage. The production version was the DR.250 Capitaine a four-seater with a 160 hp Lycoming O-320 engine and all-flying tailplane. The DR.250 first flew in 1965. The next development was a two-seat variant with a shorter fuselage the DR.220 2+2, it was powered by a 105 hp Continental O-200-A engine. The DR.221 Dauphin introduced a bigger 115 hp Lycoming O-235C engine. Then the DR.253 Regent was first flown in 1967, introducing a tricycle landing gear which was to become standard on all the following Robin designs.
Variantsedit
A DR 253 Régent with tricycle landing gear
DR.200
Prototype four-seat development of the DR.1050M1 with a Potez 105E engine, two built.[1]
DR.220 2+2
Shorter fuselage two-seat variant although it did have a small rear seat, powered by a 105hp Continental O-200-A engine, 83 built.[1]
DR.221 Dauphin
A DR.200 with four seats and powered by a 115hp Lycoming O-235C engine, 62 built.[1]
DR.250 Capitaine
A DR.200 with all-flying tailplane and powered by a 160hp Lycoming O-320-E engine, 100 built.[1]
DR.250-180
Experimental DR.250 with a 180hp Lycoming O-360-A engine, one built.[1]
DR.253 Regent
A DR.250 with enlarged fuselage and tricycle landing gear, powered by a Lycoming O-360-D2A engine, 100 built.[1]
Taylor, John W. R. (1969). Jane's All The World's Aircraft 1969–70. London: Jane's Yearbooks.
Simpson, R.W. (1991). Airlife's General Aviation. England: Airlife Publishing. ISBN1-85310-194-X.
April 10, 2024
robin, family, french, conventional, landing, gear, single, engined, light, touring, training, cabin, monoplanes, originally, produced, centre, aéronautique, company, later, changed, name, avions, pierre, robin, dauphinrole, four, seat, light, aircraftmanufact. The Robin DR 200 is a family of French conventional landing gear single engined light touring or training cabin monoplanes Originally produced by Centre Est Aeronautique the company later changed its name to Avions Pierre Robin Robin DR 200DR 221 DauphinRole Four seat light aircraftManufacturer Avions Pierre RobinFirst flight 1964 DR 200 Number built 348Variants Robin DR300 Contents 1 Development 2 Variants 3 Specifications DR 221 4 See also 5 ReferencesDevelopment editOriginally flown as the DR 200 which was a variant of the earlier DR 1050M1 with a strengthened wing and longer fuselage The production version was the DR 250 Capitaine a four seater with a 160 hp Lycoming O 320 engine and all flying tailplane The DR 250 first flew in 1965 The next development was a two seat variant with a shorter fuselage the DR 220 2 2 it was powered by a 105 hp Continental O 200 A engine The DR 221 Dauphin introduced a bigger 115 hp Lycoming O 235C engine Then the DR 253 Regent was first flown in 1967 introducing a tricycle landing gear which was to become standard on all the following Robin designs Variants edit nbsp A DR 253 Regent with tricycle landing gearDR 200 Prototype four seat development of the DR 1050M1 with a Potez 105E engine two built 1 DR 220 2 2 Shorter fuselage two seat variant although it did have a small rear seat powered by a 105hp Continental O 200 A engine 83 built 1 DR 221 Dauphin A DR 200 with four seats and powered by a 115hp Lycoming O 235C engine 62 built 1 DR 250 Capitaine A DR 200 with all flying tailplane and powered by a 160hp Lycoming O 320 E engine 100 built 1 DR 250 180 Experimental DR 250 with a 180hp Lycoming O 360 A engine one built 1 DR 253 Regent A DR 250 with enlarged fuselage and tricycle landing gear powered by a Lycoming O 360 D2A engine 100 built 1 Specifications DR 221 editData from Jane s 2 General characteristicsCrew 2 Length 7 00 m 23 ft 0 in Wingspan 8 72 m 28 ft 7 in Height 1 85 m 6 ft 1 in Wing area 13 60 m2 146 4 sq ft Empty weight 475 kg 1 047 lb equipped Max takeoff weight 840 kg 1 852 lb Powerplant 1 Lycoming O 235 C2A flat four piston engine 86 kW 115 hp Propellers 2 bladed EVRA 1 80 m 5 ft 11 in diameter wooden fixed pitch propellerPerformance Maximum speed 235 km h 146 mph 127 kn at sea level Cruise speed 220 km h 140 mph 120 kn at 2 750 m 9 000 ft 75 power Stall speed 80 km h 50 mph 43 kn Never exceed speed 290 km h 180 mph 160 kn Range 910 km 570 mi 490 nmi Service ceiling 3 900 m 12 800 ft Rate of climb 3 3 m s 650 ft min See also edit nbsp Aviation portalRelated development Robin DR300 Robin DR400References edit nbsp Wikimedia Commons has media related to Robin DR200 Notes a b c d e f Simpson 1991 pp 267 270 Taylor 1969 p 66 BibliographyThe Illustrated Encyclopedia of Aircraft Part Work 1982 1985 Orbis Publishing Taylor John W R 1969 Jane s All The World s Aircraft 1969 70 London Jane s Yearbooks Simpson R W 1991 Airlife s General Aviation England Airlife Publishing ISBN 1 85310 194 X Retrieved from https en wikipedia org w index php title Robin DR 200 amp oldid 1013423884, wikipedia, wiki, book, books, library,
