British Aero BAe Jetstream 41

The stretched regional turboprop built for higher-capacity routes.

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Easter Airways British Aerospace Jetstream 41 – © Trevor Hannant

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Overview

BAE Systems United Kingdom ICAO: JS41 1992–1997 Active $1.6 million (1992)

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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G JMAC BAe Jetstream 41 at Liverpool Municipal Airport air Museum

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Operational Context

British Aerospace Jetstream 41 — 30-seat regional turboprop

The Jetstream 41 first flew in 1991 and entered airline service in 1992. It featured a stretched fuselage and redesigned wing compared with earlier Jetstream models. The aircraft was built to offer improved comfort and operating efficiency.

Powered by two AlliedSignal TPE331 turboprop engines producing approximately 1,650 shaft horsepower each, the Jetstream 41 cruises at around 285 knots (530 km/h). Maximum takeoff weight is roughly 24,000 pounds (10,900 kg). Seating capacity typically ranges from 29 to 30 passengers.

The Jetstream 41 served with regional airlines in Europe and North America. Although production numbers were limited, the type proved reliable in short-haul service. It remains in limited operation today.