Pilatus Porter PC-6 H4
Our Pilatus PC 6-H4 is the optimal aircraft for our diverse missions. With its unique Short Take-Off and Landing (STOL) capabilities, the Pilatus can serve remote areas with very short airstrips. The Pilatus provides dependable performance at high altitudes, responsive maneuverability for flights over rugged terrain, and all-weather reliability for extreme weather conditions.
| SPECIFICATIONS | ||
|---|---|---|
| Speeds at max gross wt | 1,444 ft | 440 m |
| Landing distance over 50 ft (15 m) obstacle (STOL) | 1,033 ft | 315 m |
| Rate of climb (MTOW) | 1,010 ft/min | 5.13 m/sec |
| Max. cruise speed | 125 KTAS | 232 km/h |
| Max. range at 10,000 ft | 500 nm | 926 km |
| – with underwing tanks | 870 nm | 1611 km |
| Max. operating altitude | 25,000 ft | 7620 m |
| Stall speed | ||
| – flaps up (Vs) | 58 KEAS kt | 107 km/h |
| – full flaps set (VSO) | 52 KEAS kt | 96 km/h |
| Basic empty weight* | approx 2,756 – 3,086 lb | 1,250 – 1,400 kg |
| Max. take-off weight | 6,173 lb | 2,800 kg |
| Max. landing weight | 5,863 lb | 2,660 kg |
| Max. payload* | up to approx. 2,646 lb | 1,200 kg |
| Payload with max. fuel* | up to approx. 2,381 lb | 1,080 kg |
| *depending on configuration and fuel | ||
| Wing span | 52.07 ft | 15.87 m |
| Wing area | 324.54 ft2 | 30.15 m2 |
| Overall length | 35.76 ft | 10.90 m |
| Height | 10.50 ft | 3.20 m |
| Track | 9.84 ft | 3.00 m |