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Bell 609 - Engine(s) (2) Pratt & Whitney PT6C-67A 
HP (takeoff) 1,941hp/1,448 kw ea.
Dimensions main rotor (2) 26.0 ft/7.9 m Tail rotor N/A
Height 15 ft/4.6 m Length 44.0 ft/13.4 m
Width 60.0 ft/18.3 m (proprotors turning)
Empty weight 11,300 lb/5,126 kg Gross weight 16,800 lb/7,612 kg
Useful load 5,500 lb/2,495 kg External N/A
Vne TBD Max cruise 275 kts/509 kmh
Max rate of climb 1,500 fpm/7.6 ms
HIGE TBD HOGE 5,000 ft/1,524 m
Service ceiling 25,000 ft/7,620 m OEI service ceiling 16,000 ft/4,877 m
Std fuel 365 gal/1,381 lit Aux. fuel TBD
Max range std fuel (no reserve) 700 nm/1,296 km @ Best Altitude
Range with opt fuel TBD
IFR Crew 2 Passengers 6 VIP, 9 STD, 12 High Density
Standard avionics FAA IFR Package.
Bell 609 - Engine(s) (2) Pratt & Whitney PT6C-67A HP (takeoff) 1,941hp/1,448 kw ea. Dimensions main rotor (2) 26.0 ft/7.9 m Tail rotor N/A Height 15 ft/4.6 m Length 44.0 ft/13.4 m Width 60.0 ft/18.3 m (proprotors turning) Empty weight 11,300 lb/5,126 kg Gross weight 16,800 lb/7,612 kg Useful load 5,500 lb/2,495 kg External N/A Vne TBD Max cruise 275 kts/509 kmh Max rate of climb 1,500 fpm/7.6 ms HIGE TBD HOGE 5,000 ft/1,524 m Service ceiling 25,000 ft/7,620 m OEI service ceiling 16,000 ft/4,877 m Std fuel 365 gal/1,381 lit Aux. fuel TBD Max range std fuel (no reserve) 700 nm/1,296 km @ Best Altitude Range with opt fuel TBD IFR Crew 2 Passengers 6 VIP, 9 STD, 12 High Density Standard avionics FAA IFR Package.
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