AIRCRAFT “British Aerospace - JS41
JetStream”
REFERENCE
INFORMATION (by Aircraft performance database)
*****Aircraft Features*****
Wing
position: Low wing
Engine
position: (Front) Wing leading mounted
Tail
configuration: Cruciform tail
Landing gear:
Tricycle retractable
Wing
Span:
Length:
Height:
Power
plant: 2 x 1.500SHP Garrett TPE331-14 GR/HR or
2 x
1.650SHP Garrett TPE33 -14 turboprops with 5 blade propellers.
Accommodation:
Flightcrew of
two and typical 16 passengers, up to 29 in high density configuration.
Notes: Commuter airliner. In service since
1992. Improved stretched development of Jetstream 31 with more powerful engines
and EFIS cockpit. The production was terminated in May 1997 after 100 aircraft
had been delivered.
Alternative names:
BAe-4100 Jetstream
41
British Aerospace Jetstream 41.
*****Total Flight Simulator aircraft weight
with full fuel*****
VMO -
Maximum Operating Speed 295 KIAS
MMO -
Maximum Operating Speed Mach ns Mach
Turbulent
Air Penetration Speed 000 KIAS/.00 Mach
VLO -
Maximum Gear Operating Speed 000 KIAS
VLE -
Maximum Landing Gear Extension Speed
000 KIAS/.00 Mach
*****Maximum Flap Placard Speeds*****
Flaps
degrees KIAS
1 000
2 000
5 000
10 000
15 000
25 000
30 000
40 000
*****Take-off*****
WTC: M
Distance: 1520 mt
V2
(IAS): 110 kts
*****Climbing*****
-(to
IAS: 140 kt
ROC: 2200 ft/min
-(to
FL150)
IAS: 230 kt
ROC: 1500 ft/min
-(to
FL240)
IAS: 230 kt
ROC: 1100
ft/min
-(mach)
mach: nd
ROC: nd ft/min
*****Cruise*****
TAS: 290 kt
MACh: no data
Ceiling: FL260
Range: 1000 NM
*****Descent *****
- (to
FL240)
mach: nd
ROD: nd ft/min
- (to
FL100)
IAS: 280 kt
ROD: 1500 ft/min
*****Approach*****
IAS: 250 kt
MCS: 170 kt
ROD: 1500 ft/min
*****Landing*****
Vht
(IAS): 120 kt
APC: B
Distance: 1280 mt