| Attribute | Focke-Wulf Ta 152 × | Pilatus PC-9 M × |
|---|---|---|
| General | ||
| Manufacturer | Focke-Wulf | Pilatus Aircraft |
| Model | Focke-Wulf Ta 152 | Pilatus PC-9 M |
| Country | Germany | Switzerland |
| Manufactured from (year) | 1944 | 1984 |
| Manufactured to (year) | 1945 | - |
| Type | Military Propellor Planes | Military Trainers |
| Icao | TA152 | PC9 |
| Performance | ||
| Engine | 1x Junkers Jumo 213E | 1x 1 x Pratt & Whitney PT6A-62 turboprop |
| Power, hp (hp) | 1,750 | 1,150 |
| Avionics | - | Head Up Display (HUD) and Electronic Flight Instrumentation System (EFIS) |
| Max cruise speed (km/h) | 759 | 593 |
| Approach speed (km/h) | 180 | 143 |
| Travel range (km) | 2,037 | 1,593 |
| Fuel economy (km/l) | - | 3.982 |
| Service ceiling (m) | 15,088 | 11,579 |
| Rate of climb (m/sec) | 19.81 | 19.71 |
| Take off distance (m) | - | 397 |
| Landing distance (m) | - | 687 |
| Weights | ||
| Max take off weight (kg) | 5,217 | 3,200 |
| Max payload (kg) | - | 1,050 |
| Fuel tank capacity (l) | 992 | 893 |
| Dimensions | ||
| Seats | 1 | 2 |
| Exterior length (m) | 10.82 | 10.18 |
| Tail height (m) | 4 | 3.26 |
| Fuselage diameter (m) | 1.1 | 1.1 |
| Wing span (m) | 14.5 | 10.19 |
| Wing tips | No Winglets | No Winglets |