| Manufacturer |
Arsenal de l'Aéronautique |
Aquila Aviation by Excellence |
| Description |
The Arsenal-Delanne 10 was an experimental fighter aircraft of French origin. |
The Aquila A 210 is a two-seat reinforced plastic light aircraft produced in Germany from 2002. |
| ICAO Code |
|
A210 |
| First Flight |
1941-10-01 |
2000-03-05 |
| Entry Into service |
1940-01-01 |
|
| Designer |
Maurice Delanne |
Aquila Aviation by Excellence |
| Length (m) |
7.3152 |
7.3 |
| Height (m) |
2.7432 |
2.3 |
| Cockpit Crew |
2 |
|
| Max Speed (km/h) |
550.3956 |
241 |
| Cruise Speed (km/h) |
|
191 |
| Min Speed (km/h) |
|
80 |
| Max Ceiling (m) |
10000.49 |
4420 |
| Rate of Climb (m/s) |
|
3.82 |
| Armament |
(proposed); 1 × fixed forward firing 20 mm cannon and 2 × wing mounted 7.5 mm MAC 1934 machine guns; 2 × flexibly mounted 7.5 mm machine guns in rear cockpit |
|
| Capacity Description |
|
2 |
| Endurance (h) |
1.5 |
6 |
| National Origin |
|
Germany |
| Number Built |
1 |
222 |
| Powerplant Description |
1 × Hispano-Suiza 12Ycrs liquid-cooled v12 engine, 641 kW (860 hp) each |
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/Arsenal-Delanne_10 |
en.wikipedia.org/wiki/Aquila_A_210 |
| Flat Wing Span (m) |
10.0584 |
10.3 |
| Flat Wing Area (m²) |
22.5011 |
10.5 |
| Wake Category |
|
L |
| Aircraft Engine |
|
Rotax 912 |
| Number of Engines |
1 |
1 |