| Weights |
 |
| Max. Ramp Wt. |
14,050 lbs (6373 kgs) |
|
| Max. Take-Off Wt. |
13,950 lbs (6327 kgs) |
|
| Max. Landing Wt. |
12,725 lbs (5772 kgs) |
|
| Max. Zero Fuel Wt. |
10,500 lbs (4763 kgs) |
|
| Basic Operating Wt. |
8,650 lbs (3923 kgs) |
|
| Max. Fuel Quantity |
4,850 lbs (2199 kgs) |
|
| Max. Baggage Compartment Wt. |
500 lbs (227 kgs) |
|
| |
|
| 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 |
|
| Mean Aerodynamic Chord (MAC) |
2.72 ft (0.83 m) |
|
| Vertical Tail: Span |
7.21 ft (2.20 m) |
|
| Sweep (@ 1/4 Chord) |
55.5° |
|
| Dihedral |
46.80 sq ft (4.35 sq m) |
|
| Area |
11.56 sq ft (1.07 sq m) |
|
| Aspect Ratio |
1.11 |
|
| Mean Aerodynamic Chord (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 |
| |
|
