Aquila A 210

Airplanes

Length

7.3 m

Flat Wing Span

10.3 m

Height

2.3 m

Flat Wing Area

10.5 m²

Cruise Speed

191 km/h

Max Speed

241 km/h

Max Ceiling

4420 m

Number of Engines

Aircraft Engine

First Flight

2000-03-05

Number Built

222

Maximum Take-Off Weight

0.75 t (paragliders: kg)

Maximum Range

1148 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Aquila A 210	0.75	1148

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Aquila A 211		7.4	10.3		Compare
Aero Boero AB-115		7.273	10.72	2	Compare
Aviamilano Scricciolo	Continental O-200	7.03	10.24		Compare
Arado Ar 79		7.6	10		Compare
Beneš-Mráz Be-56 Beta-Major	Walter Major	7.55	10.66		Compare
Beechcraft Skipper	Lycoming O-235	7.32	9.14		Compare

All data (26 fields)

Name: Aquila A 210
Manufacturer: Aquila Aviation by Excellence
Description: The Aquila A 210 is a two-seat reinforced plastic light aircraft produced in Germany from 2002.
ICAO Code: A210
First Flight: 2000-03-05
Designer: Aquila Aviation by Excellence
Length (m): 7.3
Height (m): 2.3
Max Speed (km/h): 241
Cruise Speed (km/h): 191
Min Speed (km/h): 80
Max Ceiling (m): 4420
Rate of Climb (m/s): 3.82
Capacity Description: 2
Endurance (h): 6
National Origin: Germany
Number Built: 222
Powerplant Description: 1 × Rotax 912 S3 flat four air and water cooled piston, 74 kW (99 hp) each
Primary Users: Cameroon Air Force
Status: In production
Wikipedia Article (URL): en.wikipedia.org/wiki/Aquila_A_210
Flat Wing Span (m): 10.3
Flat Wing Area (m²): 10.5
Wake Category: L
Aircraft Engine: Rotax 912
Number of Engines: 1