Overview
The British Aerospace Jetstream 41 is a twin-engine turboprop developed as an enlarged derivative of the Jetstream 31. Designed for regional airline service, it entered operation in the 1990s. The aircraft aimed to compete in the 30-seat commuter market.
Live Fleet Activity (JS41)
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Specifications
Units
- 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
- Crew
- —
- 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
- Fuselage diameter
- —
- Wing span
- 60 ft 0 in · 18.29 m
- Baggage volume
- 170 ft³ · 4.8 m³
- Gross weight
- —
- Empty weight
- —
- 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
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- 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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Live fleet activity details
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