Magnus
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Two-seat High Performance Light Aircraft
for all reasons and seasons
- aircraft, high performance, cruising, training, glidingWing spans:
Magnus 13.35 m (43 ft 9 1/2 in)
Mingus 10.60 m (34 ft 9 3/4 in)
Maxus 17 m (55 ft 9 1/2 in)
Magnus Performance and Airspeeds
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Vso
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Stall speed without flaps, 450 kg MTOM, IAS |
67 km/h / 36 kts |
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Vs1
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Stall speed with flaps, + 15°, 450 kg MTOM, IAS |
63 km/h / 34 kts |
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Vcr
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Crouse speed, 75 % power, IAS |
250 km/h / 135 kts
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Vcr econo |
Cruise speed, econo power, IAS |
200 km/h / 108 kts
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Vno
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LTF UL standard, max. permitted cruising speed, green arc, IAS |
270 km/h / 146 kts
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Vne
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Never exceed speed, IAS |
305 km/h / 165 kts
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Va
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Maneuvering speed, IAS |
168 km/h / 91 kts |
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Vfe
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Max. speed with flaps down, IAS |
140 km/h / 76 kts |
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Take-off distance ground roll, 450 kg MTOM, dry grass |
90 m / 295 ft
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Take-off distance, over 15 m obstacle, 450 kg MTOM, 15 deg flaps |
178 m / 584 ft
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Max range with 75 l, 75% power, 450 kg, 30 min. reserve |
1150 km / 620 nm
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Best rate of climb at sea level, max. power, 450 kg MTOM |
8.8 m/s / 17 kts |
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Glide ratio, three wheel, fixed, fairings, prop vario 90° |
1 : 27 at 108 km/h
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Glide ratio, three wheel, retractable, prop vario 90° |
1 : 30 at 108 km/h
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Magnus Specification, Dimensions, Weights and Load factors
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Wing span |
13,35 m / 43 ft 10 in
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Overall length |
6.63 m / 21 ft 9 in
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Overall height |
2.17 m / 7 ft 1 in
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Max. cabin width |
1258 mm / 4 ft 1 in
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Wing area |
11.7 sq m / 125.9 sq ft
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Aspect ratio, aerodyn., winglets |
15.8
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Aerofoil
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Orlz 166, Alestip 4
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Positive flaps |
+ 9 deg., + 15 deg.
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Negative flaps |
- 4 deg.
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Centre of gravity |
27 % – 38 %
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Empty weight including basic equipment, without BRS, Europe |
264 kg / 582 lbs
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Maximum take off weight, Germany, France, BRS installed |
472,5 kg
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Maximum take off weight, Italy, Belgium, Slovenia, no BRS |
450 kg / 992 lbs
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Maximum take off weight, designed |
600 kg / 1320 lbs
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Useful load, Europe |
186 kg / 410 lbs
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Useful load, BRS installed, 292 kg empty weight, 600 kg MTOM |
308 kg / 679 lbs
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Minimum single pilot weight |
65 kg / 143 lbs
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Wing loading |
38.5 – 51.3 kg / sq m (7.9 – 10.5 lbs / sq ft)
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Max. service ceiling, 450 kg |
9000 m / 29530 ft
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Useful fuel capacity, each wing half, 40 + 40 l volume |
75 l / 19.8 U.S. gal (2 x 37,5 l) |
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Fuel grades, UL260i, 95 HP |
unleaded mogas / AVGAS (min.95 octane RON) |
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Limiting maneuvering load factor, at 472.5 kg MTOM |
+ 5.3 / - 2,65 g
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Tested break load, with 450 kg take-off weight |
+ 9.9 g
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Tested break load, with 472.5 kg take-off weight |
+ 9.4 g
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Tested break load, with 600 kg take-off weight |
+ 7.4 g
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