Performance Database
 |
|
Conquest I |
|
Engines |
|
| Make | Prat & Whitney |
| Model | PT6A-112 / PT6A-135A |
| HP/Thrust lbs per engine | 450 SHP |
| TBO (hours) | 3.500 |
Fuselage Dimension |
|
| Length (ft) | 35.80 |
| Height (ft) | 12.60 |
| Wing Span (ft) | 44.10 |
| Passengers | 2+6 |
| Pressurization (psi) | 5.0 |
Weights (lbs) |
|
| Max Ramp | 8.675 |
| Max Takeoff | 8.600 |
| Zero Fuel | 7.000 |
| Basic Operating | 5.350 |
| Max Landing | 8.000 |
Fuel Capacity |
|
| Standard lbs/gal | 2.450 / 366 |
Takeoff Performance (BFL) |
|
| SL ISA BFL (ft) | 2.490 |
| 5000 +20C BFL (ft) | 3.500 |
Landing Performance (ft) |
|
| FAA Field Length | 2.150 |
Range (NM) |
|
| Max Range | 1.248 |
Climb (SL ISA MTOW) |
|
| Normal (fpm) | 1.860 |
| Engine Out (fpm) | 357 |
Speeds (Knots) |
|
| Vso (Landing) | 84 |
| Normal Cruise TAS | 264 |
| Vmo (Max Operating) IAS | 230 |
Ceiling (ft) |
|
| Certified Ceiling | 30.000 |
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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