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Robin Régent 2004 specs aircraft performance and specifications
The Robin 160 and Robin 180 are 4-seat
cross-country aircraft offering a unique
combination of
high performance, comfort and operating economy.
They have superior cruising speeds and ranges to
most of their competitors while their fixed gear
and fixed-pitch propellers make them dependable
and easy to handle. Three fuel tanks with a 190
litres total capacity and an externally accessible
luggage compartment are part of the standard.
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Robin 160 |
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Robin 180 |
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4 |
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4 |
Engine, Lycoming |
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O-320, 160 hp |
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O-360, 180 hp |
Hélice Propeller,
Sensenich |
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fixed pitch |
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fixed pitch |
Gross weight |
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2315 lb |
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2425 lb |
Useful load |
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996 lb |
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1080 lb |
Wing span |
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28 ft 7 in |
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28 ft 7 in |
Max.cruise, at 75%
power, best altitude |
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132 kt |
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140 kt |
Climbing speed,
sea level, at MTOW |
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4,25 m/s (836 ft/min) |
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4,5 m/s (885 ft/min) |
Max. range, at 65%
power, best altitude |
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813 NM |
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753 NM |
Max. range, at 65%
power with optional 50 l tank, best
altitude |
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1026 NM |
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950 NM |
Take-off distance,
over 50 ft obstacle |
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1936 ft |
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1690 ft |
Landing
distance, over 50 ft obstacle
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1788 ft |
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1739 ft |
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