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Performance
High Speed Cruise  
    Mach 0.83
    MPH 560
    KTAS 486
    Km/H 901
Long Range Cruise 2,875 sm (2500 nm)
    Mach 0.76
    MPH      502
    KTAS 436
    Km/H 807
Stall Speed 91 KCAS
FAA Take-Off Balanced Field Length GW 3,939 ft (1200 m)
FAA Landing Distance 2,941 ft (896 m)
   
Seating Seven Place w/Pilot
   
Engines (2) FJ44-2A Williams Rolls
Take-Off Thrust 4,600 lbs total (2,300 lbs ea)
   
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 Speed Limit

 

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
    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
   

Preliminary specifications subject to change.
     


 
August 16, 2013

SJ30 to Be Featured In Business Jet Interiors-International
First public images of the SJ30 interior will be released.

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