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Eaglet's Design and Quality gives the aircraft excellent
flying capabilities combined
with comfort and safety.
These capabilities are
obtained through a combination of sophisticated design
and balanced choice of materials.
use of composite materials gives the aircraft its
aerodynamic smoothness making the Eaglet
computeraided flap design combined with small
wing span makes it possible to combine high
cruising speed and comfortably low stall speeds
for easy landings.
design speeds give you the freedom to maneuver up
to cruising speed.
User comfort is
realized with a combination of a spacious cockpit layout
and ergonomic details.
cockpit offers ample room for both pilot and
co-pilot. The feeling of space is further
improved by the excellent all around visibility.
industrial design gives the aircraft its well
balanced interior including the attractive
instrument panel and control details.
an impression of this comfort and enter the
aircraft's cockpit by clicking on the interior
picture on the right.
Comfort for the
environment is obtained by the Eaglet's quiet design. The
low external noise level will make this aircraft a
welcome guest at all airfields.
The safety level of
an aircraft can be judged on its Certification Basis.
Euro-ENAER has chosen to comply with the latest JAA
regulations to guarantee its customers the safety level
of the nineties. Damage tolerance and crashworthiness
make this aircraft safe through design.
Utility aircraft certified for the following manoeuvres:
- Lazy eight
- Steep turn
Full Composite airframe structure.
Low wing with partial laminar flow profile.
Fixed tricycle landing gear with nose wheel.
Air-cooled piston engine with fixed propeller.
Loading and Performance
Take-off weight 850 kg
Maximum landing weight 850 kg
Design Empty Weight 540 kg
Manoeuvre load factor:
VC = VA =130 kts
VD Diving speed 200 kts
VNE Never Exceed Speed 180 kts
VNO Max. structural cruising speed 130 kts
VF Flap Speed 100 Kts
Vsi Stall speed 30 deg. flaps 53 kts
Max rate of Glide (S/L) 12.5
Take-off Distance 996 ft
Service Ceiling 14.000 ft
at 75% Power 125-127 kts
Estimated fuel consumption at 75% power 25-27
7.050 m 23.13 ft
Wing span (incl. wing tips): 8.700
m 28.54 ft
Maximum Fuselage Width: 1.220
m 4.00 ft
Area(excl. wing tips):
9.85 m 106.02 ft
1.120 m 3.68 ft
2-Blade fixed pitch wooden propeller manufactured by MT.
Type: Lycoming O-320 D2A,
max take off power: 160 shp at 2700 RPM, 5minutes
max cont. Power: 145 shp at 2450 RPM
pages from the Euro-Enaer website are soley ment to inform you, about the eaglet
project as such, and functions here as billboard for Aviation Developments and our port folio.
More information about
Euro-Enaer and the
Eaglet can be obtained at
ENAER Chile or at the Delft University of Technology in
Copyright 1995 - 2009 by Euro-ENAER and ENAER Chili. All rights reserved.
Due to Euro-ENAER's bankruptcy in februari of 2002, all assets of Euro-ENAER have been purchased by ENAER
Chile or are in custody of Knuwer & Kreutsberg lawyers in Den Helder.
of February 2002 all activities have been terminated as
bankruptcy was lifted.