British Aerospace Jetstream 41

· British Aerospace

Airplanes

Length

19.2024 m

Flat Wing Span

18.288 m

Height

5.4864 m

Flat Wing Area

32.5904 m²

Max Seating

Cruise Speed

546.3395 km/h

Max Speed

546.3395 km/h

Max Ceiling

7924.8 m

Number of Engines

First Flight

1991-09-25

Entry Into service

1992-11-25

Number Built

100

Maximum Take-Off Weight

10.8862 t (paragliders: kg)

Total Fuel Capacity

3305.007

Maximum Range

1433.448 km

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
British Aerospace Jetstream 41	10.8862	3305.007	1433.448

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All data (28 fields)

Name: British Aerospace Jetstream 41
Manufacturer: British Aerospace
Description: The British Aerospace Jetstream 41 is a turboprop-powered feederliner and regional airliner, designed by British Aerospace as a stretched version of the Jetstream 31.
ICAO Code: JS41
First Flight: 1991-09-25
Entry Into service: 1992-11-25
Production End: 1997-01-01
Designer: British Aerospace
Type: Regional airliner/Feederliner
Length (m): 19.2024
Height (m): 5.4864
Cockpit Crew: 3
Max Seating: 29
Max Speed (km/h): 546.3395
Cruise Speed (km/h): 546.3395
Max Ceiling (m): 7924.8
Rate of Climb (m/s): 11.176
Capacity Description: 29 passengers
National Origin: United Kingdom
Number Built: 100
Powerplant Description: 2 × Allied Signal TPE331-14GR/HR turboprop engines, 1230 kW (1650 hp) each
Primary Users: Guna Airlines , Proflight Zambia
Status: In service
Wikipedia Article (URL): en.wikipedia.org/wiki/British_Aerospace_Jetstream_41
Flat Wing Span (m): 18.288
Flat Wing Area (m²): 32.5904
Wake Category: M
Number of Engines: 2