Passenger Turbo Props

British Aero BAe Jetstream 41

$1.6 million in 1992 / $ 6-7 million If Sold New At Present
Easter Airways British Aerospace Jetstream 41
© Trevor Hannant
BAE Systems · United Kingdom · ICAO: JS41 · 1992–1997 ·
$1.6 million (1992)

The Competitive Regional Turboprop The BAe Jetstream 41

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Engine:
2× AlliedSignal TPE331-14GR/HR turboprop
Engine type:
Turboprop
Power:
2 × 1,650 shp  ·  1,230 kW
Avionics:
Honeywell FZ450 Digital
Wing Tips:
No winglets
Seats:
29
Cabin width:
6 ft 1 in · 1.85 m
Cabin height:
5 ft 10 in · 1.78 m
Cabin length:
31 ft 4 in · 9.55 m
Exterior length:
63 ft 2 in · 19.25 m
Tail height:
18 ft 10 in · 5.74 m
Wing span / rotor:
60 ft 0 in · 18.29 m
Baggage volume:
170 ft³  ·  4.8 m³
Max takeoff weight:
24,000 lb  ·  10,900 kg
Max landing weight:
23,300 lb  ·  10,600 kg
Max Payload:
6,900 lb  ·  3,150 kg
Fuel capacity:
870 gal  ·  3,300 L  ·  2,600 kg  (Jet A)
Max cruise speed:
295 kt  ·  339 mph  ·  546 km/h
Range:
774 nm  ·  890 mi  ·  1,430 km
Fuel burn:
1.01 nm/gal  ·  0.49 km/L
Ceiling:
26,000 ft  ·  7,900 m
Rate of climb:
2,200 ft/min  ·  11 m/s
Takeoff distance:
5,000 ft  ·  1,520 m
Landing distance:
4,200 ft  ·  1,280 m
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