F900
DASSAULT Falcon 900
DASSAULT Falcon 900
Aircraft
Name
Falcon 900
Manufacturer
Body
Narrow
Wing
Fixed Wing
Position
Low wing
Tail
Cruciform tail
WTC
M
APC
B
Type Code
L3J
Engine
Jet
Engine Count
Multi
Position
Both sides of rear fuselage and fin-integrated
Landing gear
Tricycle retractable
Manufactured as
DASSAULT Mystere 900
DASSAULT Falcon 900
F900
Large size transcontinental corporate jet. In service since 1986 (900EX since 1996). Substantially revised development of Falcon 50 with new larger and longer fuselage. Falcon 900B with more powerful engines and increased range. Falcon 900EX ultra long range development. New version Falcon 900C. Combines the airframe and avionics of the Falcon 900B with 900EX engines. First customer deliveries beginning in 2000. The Falcon 900C is in parallel production with the 900EX.
Technical Data
Wing span (metric)
19.30 m
Length (metric)
20.20 m
Height (metric)
7.60 m
Powerplant
3 x 20 kN Garrett TFE731-5AR-1C or 3 x 21,1 kN Allied Signal TFE731-5BR turbofans.
Engine Model(s)
Garrett TFE731
Honeywell TFE731
Indicative Performance Data
Take-Off
V2
125 kts
Distance
1500 m
MTOW
21200 kg
Initial Climb (to 5000 ft)
IAS
155 kts
ROC
3000 ft/min
Initial Climb (to FL150)
IAS
290 kts
ROC
2500
Initial Climb (to FL240)
IAS
290 kts
ROC
2500 ft/min
MACH Climb
MACH
0.72
ROC
1500 ft/min
Cruise
TAS
510 kts
MACH
0.85
Ceiling
510
Range
4500 NM
Initial Descent (to FL240)
MACH
0.72
ROD
1000 ft/min
Descent (to FL100)
IAS
290 kts
ROD
4000 ft/min
Descent (FL100 & below)
IAS
n/a
MCS
180 kts
ROD
n/a
Approach
Vapp (IAS)
110 kts
Distance
700 m
