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
Manufacturered as
DASSAULT Falcon 900
DASSAULT Mystere 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: 
19.30 m
Length: 
20.20 m
Height: 
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: 
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

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