U-27A / C-16
| Specifications | |
|---|---|
| Length | 37.6 ft / 11.5 m |
| Span | 52.1 ft / 15.9 m |
| Height | 14.8 ft / 4.5 m |
| Maximum Weights |
Ramp 8,035 lbs / 3,645 kg Takeoff 8,000 lbs / 3,629 kg Landing 7,000 lbs / 3,538 kg Standard Empty Weight 3,973 lbs / 1,802 kg Maximum Useful Load 4,062 lbs / 1,842 kg |
| Engine | PT6A-114A 675 shp |
| Propeller | 3-Bladed, Constant Speed, Full Feathering, Reversible |
| Fuel Capacity | 335 gals / 2,248 lbs |
| Max Seating | 11 [FAR 23] / 14 Other |
| Certified Ceiling | 25,000 ft / 7,620 m |
| Cruise Speed | 186 kts / 344 km/hr (@ 10,000 ft) |
| Range | 932 nm / 1,726 km (@ 10,000 ft) nm/km
Includes takeoff, climb, cruise, descent and 45-min.reserve at max.cruise power |
| S.I. Rate of Climb | 1,234 fpm / 376 mpm |
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