| THC 020 - BN2B-26 Tech Data Sheet Last revision: 22.6.2000
| PERFORMANCE | U.S. | METRIC | | Max Cruise Speed (336 mph) | | | | Certified Ceiling | | | | Max Range | | | ENGINES: Pratt & Whitney | | PT6A-42 | | | WEIGHTS | Basic operating weight (Std. BEW plus one pilot at 200 lb) | | | | Useful load | | | DIMENSIONS (External) | | Wingspan | | | | Max airplane length | | | | Max tail height | | | DIMENSIONS (Internal) CABIN | | Length | | | | Height | | | | Width | | | | | | | | | | WM Data: | | | | | | | 2* Turboprop | | | | redline rpm | | | | reverse pitch | | | | Prop | | | | | | | | | | | | | Optimal RPM | | | | Optimal Speed | | | | | | | Empty weight: | | | | Max. weight: | | | | Fuel load: | | | | | | | Vso | | | | Vs | | | | Vfe | | | | Vno | | | | Vne | | | | Mmo | | | | | | | | | | | | | |  |