Performance Database
 |
|
Cheyenne II |
|
Engines |
|
| Make | Pratt & Whitney |
| Model | PT6A-28 / PT6A-34 / PT6A-135 / PT6A-135A |
| HP/Thrust lbs per engine | 620 SHP |
| TBO (hours) | 3.500 |
Fuselage Dimension |
|
| Length (ft) | 34.70 |
| Height (ft) | 12.80 |
| Wing Span (ft) | 42.70 |
| Passengers | 2+6 |
| Pressurization (psi) | 5.5 |
Weights (lbs) |
|
| Max Ramp | 9.050 |
| Max Takeoff | 9.000 |
| Zero Fuel | 7.200 |
| Basic Operating | 5.418 |
| Max Landing | 9.000 |
Fuel Capacity |
|
| Standard lbs/gal | 2.560 / 382 |
Takeoff Performance (BFL) |
|
| SL ISA BFL (ft) | 1.980 |
| 5000 +20C BFL (ft) | 2.650 |
Landing Performance (ft) |
|
| FAA Field Length | 2.480 |
Range (NM) |
|
| Max Range | 1.380 |
Climb (SL ISA MTOW) |
|
| Normal (fpm) | 2.710 |
| Engine Out (fpm) | 660 |
Speeds (Knots) |
|
| Vso (Landing) | 75 |
| Normal Cruise TAS | 255 |
| Vmo (Max Operating) IAS | 246 |
Ceiling (ft) |
|
| Certified Ceiling | 31.600 |
Specifications are provided as introductory information only and
are subject to verification by the buyer during a prepurchase inspection
of the aircraft. The aircraft is offered subject to prior sale,
price changes and/or removal from the market without notice.
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