Performance Database
 |
|
Cheyenne 400 |
|
Engines |
|
| Make | Garrett |
| Model | TPE-331-14-801 |
| HP/Thrust lbs per engine | 1.000 SHP |
| TBO (hours) | 3.000 |
Fuselage Dimension |
|
| Length (ft) | 43.40 |
| Height (ft) | 16.50 |
| Wing Span (ft) | 47.70 |
| Passengers | 2+6 |
| Pressurization (psi) | 7.5 |
Weights (lbs) |
|
| Max Ramp | 12.135 |
| Max Takeoff | 12.050 |
| Zero Fuel | 10.000 |
| Basic Operating | 7.965 |
| Max Landing | 11.100 |
Fuel Capacity |
|
| Standard lbs/gal | 3,832 / 572 |
Takeoff Performance (BFL) |
|
| SL ISA BFL (ft) | 2.325 |
| 5000 +20C BFL (ft) | 3.455 |
Landing Performance (ft) |
|
| FAA Field Length | 2.317 |
Range (NM) |
|
| Max Range | 1.430 |
Climb (SL ISA MTOW) |
|
| Normal (fpm) | 3.242 |
| Engine Out (fpm) | 997 |
Speeds (Knots) |
|
| Vso (Landing) | 84 |
| Normal Cruise TAS | 334 |
| Vmo (Max Operating) IAS | 244 |
Ceiling (ft) |
|
| Certified Ceiling | 41.000 |
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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