| Manufacturer |
Beechcraft |
Aquila Aviation by Excellence |
| Description |
The Beechcraft Model 77 Skipper is a two-seat, fixed tricycle gear general aviation airplane, originally designed for flight training but also used for touring and personal flying. |
The Aquila A 210 is a two-seat reinforced plastic light aircraft produced in Germany from 2002. |
| ICAO Code |
|
A210 |
| First Flight |
1978-09-12 |
2000-03-05 |
| Entry Into service |
1979-01-01 |
|
| Production End |
1983-01-01 |
|
| Designer |
Beechcraft |
Aquila Aviation by Excellence |
| Type |
Light utility aircraft |
|
| Length (m) |
7.32 |
7.3 |
| Height (m) |
2.41 |
2.3 |
| Cockpit Crew |
2 |
|
| Max Speed (km/h) |
|
241 |
| Cruise Speed (km/h) |
195 |
191 |
| Min Speed (km/h) |
87 |
80 |
| Max Ceiling (m) |
3930 |
4420 |
| Rate of Climb (m/s) |
3.65 |
3.82 |
| Capacity Description |
|
2 |
| Endurance (h) |
|
6 |
| National Origin |
|
Germany |
| Number Built |
312 |
222 |
| Powerplant Description |
1 × Lycoming O-235-L2C four-cylinder, air-cooled, horizontally opposed, piston aero engine, 86 kW (115 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/Beechcraft_Skipper |
en.wikipedia.org/wiki/Aquila_A_210 |
| Flat Wing Span (m) |
9.14 |
10.3 |
| Flat Wing Area (m²) |
12.1 |
10.5 |
| Wake Category |
|
L |
| Aircraft Engine |
Lycoming O-235 |
Rotax 912 |
| Number of Engines |
1 |
1 |