Performance Specification

Make	FALCON	FALCON	FALCON	FALCON
Model	100	200	50	50EX
Serial Number	ORIGINAL	ORIGINAL	ORIGINAL	ORIGINAL
ENGINES
Number	2	2	3	3
Make	GARRETT	GARRETT	GARRETT	ALLIEDSIGNAL
Model	TFE-731-2-1C	ATF3-6A-4C	TFE-731-3-1C	TFE731-40-1C
Thrust LB Per Engine	3,230.00	5,200.00	3,700.00	3,700.00
Shaft HP Per Engine	0.00	0.00	0.00	0.00
Common TBO (hours)	4,200	0	4,200	4,200
FUSELAGE DIMENSIONS
Length	45.50	56.30	60.80	60.90
Height	15.10	17.50	22.90	22.90
Wing Span	42.90	53.50	61.80	61.80
TYPICAL CONFIGURATION
Crew	2	2	2	2
Passengers	8	9	9	9
Pressurization (psi)	8.80	8.50	9.50	9.20
WEIGHTS (LBS)
Max Ramp	18,740	32,000	38,800	39,900
Max Takeoff	18,740	32,000	38,800	39,700
Zero Fuel	13,560	22,500	25,570	25,570
Basic Operating	11,200	19,200	21,900	22,250
Max Landing	17,640	28,880	35,715	35,715
FUEL CAPACITY
Standard lbs/gal	5,909  /  882	10,687  /  1,595	15,510  /  2,315	15,520  /  2,315
Optional lbs/gal	0  /  0	0  /  0	0  /  0	0  /  0
TAKEOFF PERFORMANCE
SL ISA BFL (ft)	4,500	5,260	4,700	4,935
5000+20C BFL (ft)	7,600	8,750	6,670	9,234
LANDING PERFORMANCE
FAA Field Length	2,750	2,860	2,900	2,920
RANGE (NAUTICAL MILES)
Max Range (NBAA IFR)	1,475	2,204	3,160	3,382
CLIMB (SL ISA MTOW)
Normal (fpm)	4,600	3,065	3,430	2,176
Engine Out (fpm)	1,535	830	601	322
SPEEDS (KNOTS)
Vs (Clean)	0	0	128	130
Vso (Landing)	84	89	77	95
Normal Cruise TAS	459	435	480	459
Vmo (Max Operating) IAS	370	380	370	370