| DIMENSIONS . . . . . . . . | . . . . . . . . . . . . . . . . | WITH WINGS FOLDED | . . . . . . . . . . . . . . |
Wingspan o.a. |
9,75 m |
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Length o.a. |
6,45 m |
Length o.a. |
6,20 m |
Height o.a. |
2,45 m |
Height o.a. |
1,80 m |
Cabin with |
1,18 m |
Width o.a. |
2,46 m |
Wheelbase |
2,00 m |
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Wing surface area |
12,5 mē |
||
| Extension haul | 6,6 m |
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| Diedro haul | 1,5° |
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| Weight to void | 285 kg |
||
| Maximum weight | 450 kg |
||
| Load haul | 36,14 kg/mq |
| POWER UNIT . . . . . . . . . | ROTAX 912 ( 80 HP ) . . . . | ROTAX 914 Turbo ( 115 HP ) . |
| PERFORMANCE . . . . . . . . . | ROTAX 912 . . . . . . . . . . . . . | ROTAX 914 T . . . . . . . . |
Maximun speed |
175 Km/h |
195 Km/h |
Cruising speed 75 % |
150 Km/h |
175 Km/h |
Stall speed ( without flaps ) |
50 Km/h |
50 Km/h |
| Stall speed ( with flaps ) | 40 Km/h |
40 Km/h |
Climb rate |
6 m/sec |
10 m/sec |
Take-off run fully loaded |
40 m |
30 m |
Take-off run with 1 person |
30 m |
20 m |
Landing run |
30 m |
30 m |
Max. ceiling |
5000 m |
7000 m |
| Autonomy to the maximum weight in cruise 75% (5000 Rpm) | 820 km |
750 km |
| Autonomy to the maximum weight in cruise 55% (4300 Rpm) | 910 km |
1100 km |
| Space of landing with 1 person | 30 mt |
30 mt |
| Space of maximum landing | 40 mt |
40 mt |
Ability reservoir fuel |
87 L |
87 L |
| WEIGHT . . . . . . . . . . . . . . . . . . . . . | . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . | . . . . . . . . . . . . . . . . . . . . . . . . . . . . . |
Max. take-off weight |
450 Kg |
450 Kg |
Dea S.r.l. via Nazionale, 19 - 24060 Rogno (Bg) ITALY
Tel. ++39 35 . . 967347 - Fax ++39 35 . . 967544
