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The Jetstream 41 (or J41) is based on the J31, stretched to compete in the 29 seat commuter airliner class alongside such types as the Brasilia, Dornier 328 and Saab 340. The increased span wing is mated lower on the fuselage so that it does not carry through the fuselage and interrupt the interior cabin aisle, unlike on the Jetstream 31. Additional modifications included a new reprofiled six piece windscreen and extended wing root fairing with improved baggage capacity. More powerful AlliedSignal TPE331 turboprops, mounted in new nacelles with increased ground clearance, drive advanced five blade McCauley propellers. The flightdeck has modern EFIS glass displays.
Development work on the J41 was announced in mid 1989, and certified November 23 1992 with first deliveries shortly afterwards.From mid 1994, all aircraft delivered benefited from various payload and range performance improvements, resulting from uprated engines and a higher maximum takeoff weight. The J41 was initially known as the BAe Jetstream 41, but BAe's establishment of a separate Jetstream Aircraft division in mid 1993 saw the name simplified to just Jetstream 41. From January 1996 the J41 became part of the Aero International (Regional) stable, but in May 1997 BAe announced that it was terminating J41 production. |
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| Seating (normal) |
29 |
Max Takeoff (lbs) |
23,100 |
| Seating (maximum) |
- |
Certified Ceiling (ft) |
26,000 |
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| Engines |
2 Allied Signal TPE33114GR |
To (Sealevel, ISA Temp) (ft) |
- |
| Output lbs ea. Flat Rating |
1650shp |
Landing Distance (ft) |
- |
| Maximum Mach No. |
0.65 |
Max Range (fuel) (nm) |
- |
| High Speed Cruise (Kts) |
295 |
Max Range (payload) (nm) |
590 |
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| Flight Time 300nm |
- |
Flight Time 1000nm |
- |
| Flight Time 600nm |
- |
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| External |
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Internal |
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| Length (ft) |
63.20 |
Length (ft) |
31.30 |
| Height (ft) |
18.80 |
Height (ft) |
5.90 |
| Span (ft) |
60.00 |
Width: Max floor (ft) |
6.10 |
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