The EE-10
Eaglet

The PH-EAG flying over the Alps

Description

The Eaglet's combination of Chilean Design and European Quality gives you excellent flying capabilities combined with comfort and safety.

The excellent flying capabilities are obtained through a combination of design and material choice.

  • The use of composite materials gives the aircraft its aerodynamic smoothness making the Eaglet surprisingly fast.
  • Efficient computerized flap design combined with small wing span makes it possible to combine high cruising speed and comfortably low stall speeds for easy landings.
  • High 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.

  • The cockpit offers ample space to both pilot and co-pilot. The feeling of space is further improved by the excellent all around visibility.
  • Modern industrial design gives the aircraft its well balanced interior including the attractive instrument panel and control details.
  • Get 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.

Specifications

Type

JAR 23 Utility aircraft certified for the following manoeuvres:
 
-  Lazy eight, Chandelle and Steep turn

   Design features

Side-by-side, two-seat monoplane.
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.

Weights, Loading and Performance

Maximum Take-off weight 850 kg

1874 lb

Maximum landing weight 850 kg

1874 lb

Design Empty Weight 600 kg

1323 lb

 

Cruising Speed at 65% Power 125 ktas@11000 ft

Cruising Speed at 75% Power

133 ktas@8000 ft
Max. speed in level flight 139 ktas@sea lvl

Fuel consumption
at 75% power  

32 L/h
8.5 G/h
Fuel consumption
at 65% power
28 L/h
7.4 G/h

Manoeuvre load factor:

+ 4.4 g

- 2.4 g

Vc Cruise speed

140 kias
Va Manoeuvre speed 130 kias

Vne Never Exceed Speed 

180 kias

Vno Max. structural cruising speed

130 kias

Vf Flap Speed 

100 kias
Vclean Stall speed w/o flaps 61 kias

Vsi Stall speed 30 deg. flaps 

54 kias

Max rate of Glide (S/L) 

12.5
Max rate of Climb 900 ft/min

Take-off Distance (intermediate flaps, ISO conditions)

260 m
850 ft

Service Ceiling 

14.000 ft

Dimensions

Click for a larger image 
Click on pictures for detailed views

Total Length: 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
Fuel Quantity (usable): 158 L 41.5 G
Cabin Width: 1.120 m 3.68 ft

Power Plant

Propeller
2-Blade fixed pitch wooden propeller
manufactured by MT
Engine
Type: Textron Lycoming O-320 D2A
max power: 160 shp at 2700 RPM

line_2.GIF (62 bytes)



An mpg movie of the Eaglet