|
Performance
| High Speed Cruise |
|
| Mach |
0.83 |
| MPH |
560 |
| KTAS |
486 |
| Km/H |
901 |
| Long Range Cruise |
2,875 sm (2500 nm) 4,626 km |
| Mach |
0.76 |
| MPH |
502 |
| KTAS |
436 |
| Km/H |
807 |
| Stall Speed |
91 kcas |
FAA Take-Off Balanced
Field Length GW |
3,939 ft (1,200 m) |
Weights
| Max. Ramp Wt. |
14,050 lbs (6,373 kg) |
| Max. Take-Off Wt. |
13,950 lbs (6,327 kg) |
| Max. Landing Wt. |
12,750 lbs (5,783 kg) |
| Max. Zero Fuel Wt. |
10,500 lbs (4,773 kg) |
| Empty Wt. Equipped |
8,400 lbs (3,818 kg) |
| Max. Fuel Quantity |
713 gals/4,850 lbs (2797 I) |
| Max. Baggage Compartment Wt. |
500 lbs (226 kg) |
Seating
| Configuration |
Seven seats, Pilot + 6 PAX |
Design Data
| Pressurization |
12.0 psi max differential |
| Max. Certified Altitude |
49,000 ft |
| Cabin Altitude is Sea Level Up To |
41,000 ft |
| Mmo Above 29,500 ft |
Mach 0.83 |
| Vmo Up To 29,500 ft |
320 kcas (593 km/h) |
| Vref |
105 KCAS |
| Speed Brake Operation |
No Limit |
|
|
Engines
| Models |
(2) FJ44-2A Williams Rolls |
| Take-Off Thrust |
4,600 lbs total (2,300 lbs ea) |
Aircraft Characteristics
| Overall Length |
46.80 ft (14.26 m) |
| Overall Height |
14.19 ft (4.33 m) |
| Wing |
| Span |
42.33 ft (12.90 m) |
| Sweep (@ 1/4 Chord) |
30.1° |
| Dihedral |
2.3° |
| Area |
190.69 sq ft (17.71 sq m) |
| Aspect Ratio |
9.40 |
| Mean Aerodynamic Chord (MAC) |
5.12 ft (1.56 m) |
| Horizontal Tail |
| Span |
14.56 ft (4.44 m) |
| Sweep (@ 1/4 Chord) |
33° |
| Dihedral |
0° |
| Area |
36.72 sq ft (3.41 sq m) |
| Aspect Ratio |
5.77 |
| MAC |
2.72 ft (0.83 m) |
| Vertical Tail |
| Span |
7.21 ft (2.20 m) |
| Sweep (@ 1/4 Chord) |
55.5° |
| Area |
46.80 sq ft (4.35 sq m) |
| Aspect Ratio |
1.11 |
| MAC |
7.10 ft (2.17 m) |
| Ventral Fin |
| Total Area |
11.56 sq ft (1.07 sq m) |
| Ventral Rudder Area |
1.95 sq ft (0.18 sq m) |
| Landing Gear |
| Width between Main Gear |
6.85 ft (2.09 m) |
| Wheelbase |
18.84 ft (5.74 m) |
| Tire Size |
16 in x 4.4 in |
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