
            
                              
                              
                              Robin began development of the R 3000 in the late 
                              1970s as part of a model range modernisation 
                              drive. Robin originally proposed offering a wide 
                              range of R 3000 models, although only a few have 
                              seen production. Models that were proposed but 
                              never saw the light of day include the R 3180S 
                              with a turbocharged engine and retractable 
                              undercarriage; the fixed gear, but turbocharged R 
                              3180T; the R 3180GT1 and R 3180GT2 with a larger 
                              cabin (the GT1 would have been turbocharged, the 
                              GT2 turbocharged with retractable gear); and the R 
                              3140T with a solid cabin roof.
      
                              
                              A 1981 agreement saw 
                              Aerospatiale, GA manufacturer Socata's parent, 
                              become responsible for R 3000 marketing between 
                              1983 and 1987, which meant that Robin concentrated 
                              on lower power models so as to not compete with 
                              Socata's TB range (described separately), and 
                              plans for the higher performance models were 
                              dropped. 
      
                              
                              The metal construction R 3000 features a Jodel based wing and forward sliding cockpit 
                              canopy and an aerodynamically efficient airframe, 
                              and is distinguishable by its T-tail. The first R 
                              3000 model to fly was the R 3140, its first flight 
                              occurred on December 8 1980, a second prototype 
                              flew in June 1981 and introduced the definitive 
                              tapered wings. Production aircraft have been 
                              delivered since 1985. 
      
                              
                              The R 3140, now the R 
                              3000/140, has been joined in production by the two 
                              seat 87kW (116hp) O235 powered R 3000/100; the 
                              three seat R 3120; R 3000/120 (R3120); four seat 
                              105kW (140hp) powered R 3000/140; and the 135kW 
                              (180hp) R 3000/180R glider tug. Current production 
                              is of the R 3000/140 and R 3000/160, a development 
                              of the R 3000/120 (which went of production in 
                              1988). 
                              
                              
                              Powerplants
                              
                              
                              R 3000/100 - One 87kW (116hp) Lycoming O235 flat 
                              four piston engine driving a two blade fixed pitch 
                              propeller. R 3000/160 - One 135kW (180hp) Textron 
                              Lycoming O320D2A flat four. 
                              
                              
                              Performance
                              
                              
                              R 3000/100 - Max speed 230km/h (124kt), 
                              max cruising speed 210km/h (113kt), 
                              normal cruising speed 200km/h (108kt). 
                              Initial rate of climb 590ft/min. 
                              Service ceiling 13,000ft. 
                              Range with standard fuel and no reserves 1120km 
                              (605nm), with optional fuel 1420km (767nm). 
                              
                              
                              R 3000/160 - Max speed 270km/h (146kt), 
                              max cruising speed 255km/h (138kt), 
                              economical cruising speed at 65% power 238km/h 
                              (128kt). 
                              Initial rate of climb 875ft/min. 
                              Service ceiling 15,000ft. 
                              Range with standard fuel at 75% power cruising 
                              speed 1490km (804nm), at 65% power cruising speed 
                              1610km (868nm). 
                              
                              
                              Dimensions
                              
                              
                              Wing span 9.81m (32ft 2in), 
                              length 7.51m (24ft 8in), 
                              height 2.66m (8ft 9in). 
                              Wing area 14.5m2 (155.8sq ft). 
                              
                              
                              Capacity
                              
                              
                              Seating for two in R 3000/100, three in R 3000/120 
                              and four in R 2000/140 and R 3000/160. 
                              
                              
                              Production
                              
                              
                              Approximately 75 examples of the two versions of 
                              the R 3000 had been delivered.