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PC-7
Mk.II (M) TURBO TRAINER |
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Training aircraft | ||
Specification: | ||
Year deployed
Wing span, m Length, m Height, m Wings area, m2 Weight, kg - empty aircraft - normal take-off - maximum take-off Fuel, l - Internal - AFT Engine Power, hp Maximum speed, km/h Cruising speed, km/h Range, km Combat range, km Endurance, h.min Rate of climb, m/min Service ceiling, m Maximum overload Crew Useful load: |
- 1978 - 10.19 - 10.13 - 3.26 - 16.29 - 1670 - 1910 - 2710 - 518 - 2 У 245 (2 У 155) - 1 TE Pratt & Whitney Canada PT6A-25C - 1 У 700 - 555 - 465 - 1935 - 1407 - 4.40 - 865 - 9150 - 7 - 2 1040 kg in 6 hardpoints |