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Name Jetstream 41
Body Narrow
Wing Fixed Wing
Position Low wing
Tail Cruciform tail
WTC Medium
Type code L2T
Engine Turboprop
Engine count Multi
Position (Front) Wing leading mounted
Landing gear Tricycle retractable
Mass group 3

Manufacturered as:

AI(R) Jetstream 41
AI(R) BAe-4100 Jetstream 41
BRITISH AEROSPACE BAe-4100 Jetstream 41
JETSTREAM BAe-4100 Jetstream 41
JETSTREAM Jetstream 41




Commuter airliner. In service since 1992. Improved stretched development of Jetstream 31 with more powerful engines and Electronic Flight Instrument System cockpit. The production was terminated in May 1997 after 100 aircraft had been delivered.

Technical Data

Wing span 18.29 m60.007 ft <br />
Length 19.25 m63.156 ft <br />
Height 5.74 m18.832 ft <br />
Powerplant 2 x Garrett TPE331-14 GR/HR (1.500 shp) or
2 x Garrett TPE331-14 (1.650 shp) turboprops with 5 blade propellers.
Engine model AlliedSignal TPE-331, Garrett AiResearch TPE-331

Performance Data

Take-Off Initial Climb
(to 5000 ft)
Initial Climb
(to FL150)
Initial Climb
(to FL240)
MACH Climb Cruise Initial Descent
(to FL240)
(to FL100)
Descent (FL100
& below)
V2 (IAS) 110 kts IAS 140 kts IAS 230 kts IAS 230 kts MACH TAS 290 kts MACH IAS 280 kts IAS kts Vapp (IAS) 120 kts
Distance 1525 m ROC 2200 ft/min ROC 1500 ft/min ROC 1100 ft/min ROC ft/min MACH ROD ft/min ROD 1500 ft/min MCS 170 kts Distance 1280 m
MTOW 1015010,150 kg <br />10.15 tonnes <br /> kg Ceiling FL260 ROD ft/min APC C
WTC M Range 10001,000 nm <br />1,852,000 m <br />1,852 km <br />6,076,115.49 ft <br /> NM

Accidents & Serious Incidents involving JS41

  • JS41, Birmingham UK, 2007 (On 26 June 2007, at Birmingham Airport UK, a BAe Jetstream 41 started an engine running pushback without using intercom between ground crew and flight crew. The pushback could not be completed as the towbar could not be disconnected and confusion over a decision to return the aircraft to the gate resulted in an attempt to do so with the aircraft brakes selected which caused the aircraft nose landing gear to collapse.)
  • JS41, Rhodes Greece, 2015 (On 2 February 2015, a Jetstream 41 made a hard and extremely fast touchdown at Rhodes and the left main gear leg collapsed almost immediately. The crew were able to prevent the consequent veer left from leading to a lateral runway excursion. The Investigation found that the approach had been significantly unstable throughout with touchdown at around 50 knots above what it should have been and that a whole range of relevant procedures had been violated by the management pilot who had flown the approach in wind shear conditions in which approaches to Rhodes were explicitly not recommended.)
  • JS41, en-route, North West of Aberdeen UK, 2008 (On 9 April 2008, a BAe Jetstream 41 departed Aberdeen in snow and freezing conditions after the Captain had elected not to have the airframe de/anti iced having noted had noted the delay this would incur. During the climb in IMC, pitch control became problematic and an emergency was declared. Full control was subsequently regained in warmer air. The Investigation concluded that it was highly likely that prior to take off, slush and/or ice had been present on the horizontal tail surfaces and that, as the aircraft entered colder air at altitude, this contamination had restricted the mechanical pitch control.)
  • JS41, vicinity Durban South Africa, 2009 (On 24 September 2009 a BAe Jetstream 41 being operated by SA Airlink on a positioning flight from Durban to Pietermaritzburg with only three crew members on board experienced an engine fire during take off and after reaching a height of about 500 feet agl then entered a semi controlled descent to a high impact forced landing in a residential area about 1400 metres beyond the runway end. The three occupants were all seriously injured and the aircraft commander subsequently died as a result of his injuries. A fourth person on the ground was also injured.)