| First flown on 12 August 1965, the Aero Subaru is a four-seat light monoplane, produced in three versions with 119-134kW Lycoming engines. Between 1968 and 1985 a total of 274 were completed.
CREW | 1 |
PASSENGERS | 3 |
ENGINE | 1 x Lyc. O-360, 132kW |
WEIGHTS |
Take-off weight | 1060 kg | 2337 lb |
Empty weight | 620 kg | 1367 lb |
DIMENSIONS |
Wingspan | 9.4 m | 31 ft 10 in |
Length | 8.0 m | 26 ft 3 in |
Height | 2.6 m | 9 ft 6 in |
Wing area | 14.0 m2 | 150.69 sq ft |
PERFORMANCE |
Max. speed | 225 km/h | 140 mph |
Cruise speed | 211 km/h | 131 mph |
Ceiling | 4724 m | 15500 ft |
Range w/max.fuel | 1295 km | 805 miles |
horst, e-mail, 28.01.2014 14:47 Is there any chance to get a plot of the airfoil (U615M), since I am planning to build a RC Model and would like to use the original airfoil. I cant find anything in the internet. reply | sven, 23.03.2012 18:36 Proper canopy? You like the ones that restrict your view ? As for the fuji, corrosion problems have grounded many. A bit of a barge if I remember it correctly. reply | Hiroyuki Takeuchi, e-mail, 23.03.2012 11:54 The airfoil is a Fuji original called U615M. This is an laminar flow type. It is also interesting that the horizontal tail has a negative camber, like a Clark Y turned upside down. reply | Recordo, e-mail, 21.02.2010 17:37 What the Grumman Tiger would have looked like with a proper canopy. Which airfoil is a good question. reply |
| mark, e-mail, 28.03.2008 19:37 yes i have one question: What kind type profile was used to build the wing? I mean NACA profile for exeple: NACA 23018 If someone know ,please send me this information to my email> Thank you reply |
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