Performance Database
 |
|
LEAR 60 |
|
Engines |
|
| Make | Pratt & Whitney |
| Model | PW 305A |
| HP/Thrust lbs per engine | 4.600 |
| TBO (hours) | 5.000 |
Fuselage Dimension |
|
| Length (ft) | 58.70 |
| Height (ft) | 14.70 |
| Wing Span (ft) | 43.80 |
| Passengers | 8 |
| Pressurization (psi) | 9.4 |
Weights (lbs) |
|
| Max Ramp | 23.750 |
| Max Takeoff | 23.500 |
| Zero Fuel | 17.000 |
| Basic Operating | 14.700 |
| Max Landing | 19.500 |
Fuel Capacity |
|
| Standard lbs/gal | 7.910 / 1.180 |
Takeoff Performance (BFL) |
|
| SL ISA BFL (ft) | 5.360 |
| 5000 +20C BFL (ft) | 8.520 |
Landing Performance (ft) |
|
| FAA Field Length | 3.420 |
Range (NM) |
|
| Max Range | 2.428 |
Climb (SL ISA MTOW) |
|
| Normal (fpm) | 4.500 |
| Engine Out (fpm) | 1.340 |
Speeds (Knots) |
|
| Vso (Landing) | 107 |
| Normal Cruise TAS | 453 |
| Vmo (Max Operating) IAS | 340 |
Ceiling (ft) |
|
| Certified Ceiling | 51.000 |
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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