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S-33 Independence  
Initial Operational Capability (IOC):
Total Production: ?
Unitary Cost: USD$3.9 million
Origin: United States of America
Corporations: Spectrum Aeronautical
Parent System: S-33 Independence
Initial Operational Capability (IOC):
Total Production: ?
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Description: The Spectrum Aeronautical S-33 Independence is a six-to-eight passengers, twin-engine business jet capable of traveling ranges of 2,000 nautical miles. Powered by two Williams International FJ33-4A turbofan engines, each rated at 1,750-lb of thrust, can achieve a top speed of 425 knots.

S-33 Independence Specifications

Crew: 1
Number of Engines: 2
Passengers: 8
Dimensions
Cabin Height: 5 foot (60 inch)
Cabin Length: 18 foot (216 inch)
Cabin Width: 5 foot (60 inch)
Height: 10.8 foot (130 inch)
Length: 46 foot (551 inch)
Wingspan: 43 foot (13.2 meter)
Performance
Ceiling: 45,000 foot (13,716 meter)
Landing Run Distance: 3,000 foot (914 meter)
Max Range: 2,000 nautical mile (2,302 mile)
Take Off Run Distance: 3,000 foot (914 meter)
Speed
Stall Speed: 90 KTAS (104 mph)
Top Speed at High Altitude: 425 knot (787 kph)
Time
Time Between Overhaul: 3,500 hour
Volume
Baggage Capacity: 70 cu ft (1.98 metric ton)
Weight
Empty Weight: 3,580 pound (1,624 kilogram)
Fuel Load: 2,730 pound (1,238 kilogram)
Max Landing Weight: 6,818 pound (3,093 kilogram)
Max Ramp Weight: 7,535 pound (3,418 kilogram)
Max Takeoff Thrust: 3,500 pound
Max Takeoff Weight: 7,500 pound (3.40 ton)
Max Zero Fuel Weight: 6,150 pound (2,790 kilogram)
Operational Weight: 4,050 pound (1,837 kilogram)
Payload: 955 pound (433 kilogram)
Useful Load: 3,685 pound (1,672 kilogram)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

Operators & Related Equipment


OperatorsItems

Grand Total ??
Propulsion Systems
FJ33-4Ax2
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