Performance Database
 |
|
ASTRA G 100 (formerly Astra SPX) |
|
Engines |
|
| Model | TFE-731-40R-200G |
| HP/Thrust lbs per engine | 4.250 |
| TBO (hours) | 5.000 |
Fuselage Dimension |
|
| Length (ft) | 55.70 |
| Height (ft) | 18.20 |
| Wing Span (ft) | 54.70 |
| Passengers | 6 + 2 Crew |
| Pressurization (psi) | 8.8 |
Weights (lbs) |
|
| Max Ramp | 24.800 |
| Max Takeoff | 24.650 |
| Zero Fuel | 17.000 |
| Basic Operating | 13.700 |
| Max Landing | 20.700 |
Fuel Capacity |
|
| Standard lbs/gal | 9.365 / 1.398 |
Takeoff Performance (BFL) |
|
| SL ISA BFL (ft) | 5.395 |
| 5000 +20C BFL (ft) | 8.700 |
Landing Performance (ft) |
|
| FAA Field Length | 2.920 |
Range (NM) |
|
| Max Range | 2.949 |
Climb (SL ISA MTOW) |
|
| Normal (fpm) | 3.800 |
Speeds (Knots) |
|
| Normal Cruise TAS | 456 |
| Vmo (Max Operating) IAS | 353 |
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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