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Robin Dauphin
2004 spec aircraft performance and specifications
The Robin Dauphins are renowned for their
excellent handling characteristics, ruggedness and
low operating costs. They are powered by a
reliable Lycoming 4-cylinder engine, with 120 hp
or 160 hp or the new JetA1 Centurion 1.7. Their
versatility makes them great favourites with
aero-clubs and flying-schools where they are
operated for basic training, navigation
instruction and instrument flying, or as
3-/4-seat, low cost, general purpose airplanes.
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Robin 120 |
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Robin 135 CDI
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Robin140 |
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2+2 |
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2+2 |
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4 |
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Engine |
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Lyco O-235,118hp |
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Centurion 1.7
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Lyco O-320, 160hp |
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Hélice Propeller |
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Sensenich fixed
pitch |
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MT var. pitch
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Sensenich fixed
pitch |
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Gross weight |
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1984 lb
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2159 lb |
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2204 lb
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Useful load |
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772 lb |
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774 lb |
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926 lb |
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Wing span |
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28 ft 7 in
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28 ft 7 in |
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28 ft 7 in
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Fuel capacity,
std |
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29 US Gal
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29 US Gal
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29 US Gal |
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Max.cruise, at
75% power, best altitude |
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116 knt |
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126 knt |
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128 knt
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Max. range, at
65% power, best altitude |
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915 km |
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1200 km
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828 km |
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Max. range, at
65% power with optional 50 l tank,
best altitude |
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1800 km |
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1195 km |
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Climbing speed,
sea level, at MTOW |
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590 ft/min
3 m/s |
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670 ft/min
3.35 m/s |
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870 ft/min
4.4 m/s |
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Take-off
distance, over 50 ft obstacle |
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1755 ft
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1443 ft
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1591 ft
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Landing
distance, over 50 ft obstacle
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1510 ft
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1541 ft
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1541 ft |
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