Performance Database
 |
|
BEECHJET 400A |
|
Engines |
|
| Model | JT15D-5 |
| HP/Thrust lbs per engine | 2.965 |
| TBO (hours) | 3.600 |
Fuselage Dimension |
|
| Length (ft) | 48.40 |
| Height (ft) | 13.90 |
| Wing Span (ft) | 43.50 |
| Passengers | 7 + 2 Crew |
| Volume Interior (cu.ft) | 305 |
| Volume Baggage (cu.ft) | 57 |
| Pressurization (psi) | 9.1 |
Weights (lbs) |
|
| Max Ramp | 16.300 |
| Max Takeoff | 16.100 |
| Zero Fuel | 13.000 |
| Basic Operating | 10.950 |
| Max Landing | 15.700 |
Fuel Capacity |
|
| Standard lbs/gal | 4.911 / 733 |
Takeoff Performance (BFL) |
|
| SL ISA BFL (ft) | 4.169 |
| 5000 +20C BFL (ft) | 6.322 |
Landing Performance (ft) |
|
| FAA Field Length | 2.960 |
Range (NM) |
|
| Max Range | 1.249 |
| Full passengers | 1.225 |
| Two passengers (200 lbs each) | 1.450 |
Climb (SL ISA MTOW) |
|
| Normal (fpm) | 2.056 |
| Engine Out (fpm) | 305 |
Speeds (Knots) |
|
| Vso (Landing) | 87 |
| Normal Cruise TAS | 445 |
| Vmo (Max Operating) IAS | 320 |
Ceiling (ft) |
|
| Certified Ceiling | 45.000 |
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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