SPECIFICATIONS
COMMUTER CATEGORY CERTIFICATION

Performance

High Speed Cruise

         Mach

0.83

         MPH

560

         KTAS

486

         Km/H

900

Long Range Cruise

2500 nm (4,626 km)

         Mach

0.78

         MPH

514

         KTAS

447

         Km/H

828

Stall Speed

91 kcas

FAA Take-Off Balanced Field Length GW

3,939 ft (1200 m)

FAA Landing Distance

2,555 ft (779 m)


Seating

Seven Seats, Pilot plus six passengers


Engines

         Type

2 x FJ44-2A

         Take-Off Thrust

4,600 lbs total (2,300 lbs each)


Design Data

         Pressurization

12.0 psi

         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


Weights

         Max. Ramp Wt.

14,050 lbs (6373 kg)

         Max. Take-Off Wt.

13,950 lbs (6327 kg)

         Max. Landing Wt.

12,725 lbs (5772 kg)

         Max. Zero Fuel Wt.

10,500 lbs (4763 kg)

         Empty Wt. Equipped

8,450 lbs (3833 kg)

         Max. Fuel Quantity

4,850 lbs (2199 I)

         Max. Baggage Compartment Wt.

500 lbs (227 kg)


Internal Dimensions

         Length

17 ft 7 in (5,36 m)

         Cabin Length

12ft 6in (3,81 m)

         Cabin Width

4 ft 10 in (1,47 m)

         Cabin Height

4 ft 4 in (1,32 m)

         Cabin Volume

190.6 cu ft (5.9 m³)

         Cabin Door Width

32 in (0.81 m)

Preliminary Specifications. Subject to Change