Performance Specification

Make	CITATION	CITATION	CITATION	CITATION
Model	III	VI	VII	X
Serial Number	ORIGINAL	ORIGINAL	ORIGINAL	ORIGINAL
ENGINES
Number	2	2	2	2
Make	GARRETT	GARRETT	GARRETT	ROLLS-ROYCE
Model	TFE-731-3B-100S	TFE-731-3B-100S	TFE-731-4R-2S	AE-3007C
Thrust LB Per Engine	3,650.00	3,650.00	4,000.00	6,764.00
Shaft HP Per Engine	0.00	0.00	0.00	0.00
Common TBO (hours)	4,200	4,200	4,200	6,000
FUSELAGE DIMENSIONS
Length	55.60	55.50	55.50	72.30
Height	16.90	16.80	16.80	19.00
Wing Span	53.60	53.50	53.50	63.60
TYPICAL CONFIGURATION
Crew	2	2	2	2
Passengers	8	9	9	8
Pressurization (psi)	9.30	9.30	9.30	9.30
WEIGHTS (LBS)
Max Ramp	22,200	22,200	22,650	36,400
Max Takeoff	22,000	22,000	22,450	36,100
Zero Fuel	15,300	15,400	16,500	24,400
Basic Operating	13,200	13,300	12,120	22,020
Max Landing	19,000	20,000	20,000	31,800
FUEL CAPACITY
Standard lbs/gal	7,329  /  1,094	7,332  /  1,094	7,329  /  1,094	12,931  /  1,930
Optional lbs/gal	0  /  0	0  /  0	0  /  0	0  /  0
TAKEOFF PERFORMANCE
SL ISA BFL (ft)	5,150	5,030	4,940	5,200
5000+20C BFL (ft)	8,370	7,545	7,460	7,350
LANDING PERFORMANCE
FAA Field Length	2,900	2,900	2,910	3,410
RANGE (NAUTICAL MILES)
Max Range (NBAA IFR)	2,470	2,345	2,220	3,300
CLIMB (SL ISA MTOW)
Normal (fpm)	3,699	3,699	4,442	4,000
Engine Out (fpm)	805	805	1,080	213
SPEEDS (KNOTS)
Vs (Clean)	125	125	0	123
Vso (Landing)	97	97	97	109
Normal Cruise TAS	450	468	470	512
Vmo (Max Operating) IAS	278	278	278	350