Performance Database
 |
|
King Air 350 |
|
Engines |
|
| Make | Pratt & Whitney |
| Model | PT6A-60A |
| HP/Thrust lbs per engine | 1.050 SHP |
| TBO (hours) | 3.600 |
Fuselage Dimension |
|
| Length (ft) | 46.70 |
| Height (ft) | 15.00 |
| Wing Span (ft) | 57.90 |
| Passengers | 2+9 |
| Pressurization (psi) | 6.6 |
Weights (lbs) |
|
| Max Ramp | 15.100 |
| Max Takeoff | 15.000 |
| Zero Fuel | 12.500 |
| Basic Operating | 9.640 |
| Max Landing | 15.000 |
Fuel Capacity |
|
| Standard lbs/gal | 3.610 / 539 |
Takeoff Performance (BFL) |
|
| SL ISA BFL (ft) | 3.300 |
| 5000 +20C BFL (ft) | 5.376 |
Landing Performance (ft) |
|
| FAA Field Length | 2.508 |
Range (NM) |
|
| Max Range | 1.966 |
Climb (SL ISA MTOW) |
|
| Normal (fpm) | 2.979 |
| Engine Out (fpm) | 912 |
Speeds (Knots) |
|
| Vso (Landing) | 81 |
| Normal Cruise TAS | 311 |
| Vmo (Max Operating) IAS | 263 |
Ceiling (ft) |
|
| Certified Ceiling | 35.000 |
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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