Sino Swearingen SJ30-2

The light jet built for exceptional speed and high-altitude performance

Overview

ICAO: SJ30 2007–2009 Active $8.3 million (2015)

The Sino Swearingen SJ30-2 is a light business jet developed for high cruise speed and extended range. Designed to operate at high altitudes with a pressurized cabin, it aimed to outperform competitors in its size category. The aircraft experienced a prolonged development path before entering service.

Live Fleet Activity (SJ30)

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Specifications

Units
Engine
2 × Williams International FJ44-2a
Engine type
Turbofan
Thrust
2 × 2,300 lbf · 10 kN
Avionics
Honeywell Primus Epic CDS, Primus 331 weather radar, Dual Primus II radio system,TCAS 2000
Wing tips
No winglets
Seats
6
Crew
Cabin width
4 ft 9 in  ·  1.44 m
Cabin height
4 ft 4 in  ·  1.31 m
Cabin length
12 ft 6 in  ·  3.80 m
Exterior length
46 ft 11 in  ·  14.30 m
Tail height
14 ft 1 in  ·  4.30 m
Fuselage diameter
4 ft 11 in  ·  1.50 m
Wing span
42 ft 4 in  ·  12.90 m
Baggage volume
71 ft³  ·  2.0 m³
Gross weight
Empty weight
Max takeoff weight
14,000 lb  ·  6,350 kg
Max landing weight
12,700 lb  ·  5,800 kg
Max payload
1,800 lb  ·  800 kg
Fuel capacity
710 gal · 2,700 L · 2,200 kg (Jet A)
Max cruise speed
486 kt  ·  559 mph  ·  900 km/h
Maximum speed
Cruise speed
Approach speed
93 kt  ·  107 mph  ·  172 km/h
Range
2,500 nm  ·  2,880 mi  ·  4,630 km
Fuel burn
8.11 nm/gal  ·  3.97 km/L
Ceiling
49,000 ft  ·  14,900 m
Rate of climb
3,663 ft/min  ·  19 m/s
Takeoff distance
3,950 ft  ·  1,200 m
Landing distance
2,550 ft  ·  780 m
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‘N30SJ’ Sino Swearingen SJ30-2

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Flight Airline Reg Alt Speed Heading V/S

Operational Context

Sino Swearingen SJ30-2 — high-speed light business jet

The SJ30 originated in the 1980s under Ed Swearingen’s vision for a compact but fast business jet. After multiple ownership changes and delays, the SJ30-2 variant entered service in the 2000s. The design emphasizes aerodynamic efficiency and a relatively high cruise speed for a light jet.

Powered by two Williams FJ44 turbofan engines producing approximately 2,300 pounds of thrust (10 kN) each, the SJ30-2 cruises at around 450 knots (830 km/h). Maximum takeoff weight is roughly 13,950 pounds (6,330 kg). Range approaches 2,500 nautical miles (4,630 km) depending on configuration.

The aircraft’s high cruise speed and long range distinguish it within the light jet segment. Production volumes have remained modest compared with larger manufacturers. The SJ30-2 stands as a technically ambitious design within business aviation.