Performance Specification

Make	KING AIR	KING AIR	KING AIR	KING AIR	KING AIR
Model	300	350	A100	B100	B200
Serial Number	ORIGINAL	ORIGINAL	ORIGINAL	ORIGINAL	ORIGINAL
ENGINES
Number	2	2	2	2	2
Make	PRATT & WHITNEY	PRATT & WHITNEY	PRATT & WHITTNEY	GARRETT	PRATT & WHITNEY
Model	PT6A-60A	PT6A-60A	PT6A-34	TPE-331-10AV	PT6A-42
Thrust LB Per Engine	0.00	0.00	0.00	0.00	0.00
Shaft HP Per Engine	1,050.00	1,050.00	680.00	715.00	850.00
Common TBO (hours)	3,600	3,600	3,600	5,000	3,600
FUSELAGE DIMENSIONS
Length	43.90	46.70	39.90	39.90	43.80
Height	15.00	15.00	15.40	15.40	15.00
Wing Span	54.50	57.90	45.90	45.90	54.50
TYPICAL CONFIGURATION
Crew	2	2	2	2	2
Passengers	8	8	8	8	8
Pressurization (psi)	6.50	6.50	4.60	4.60	6.50
WEIGHTS (LBS)
Max Ramp	14,100	15,100	11,568	11,875	12,590
Max Takeoff	14,000	15,000	11,500	11,800	12,500
Zero Fuel	11,500	12,500	9,600	9,600	11,000
Basic Operating	8,890	9,640	7,197	7,482	8,592
Max Landing	14,000	15,000	11,210	11,210	12,500
FUEL CAPACITY
Standard lbs/gal	3,611  /  539	3,611  /  539	3,149  /  470	3,149  /  470	3,645  /  544
Optional lbs/gal	0  /  0	0  /  0	0  /  0	0  /  0	0  /  0
TAKEOFF PERFORMANCE
SL ISA BFL (ft)	1,992	3,300	3,245	2,951	2,579
5000+20C BFL (ft)	3,600	5,376	4,710	4,600	3,800
LANDING PERFORMANCE
FAA Field Length	2,907	2,508	2,944	2,679	2,845
RANGE (NAUTICAL MILES)
Max Range (NBAA IFR)	1,795	1,966	1,000	1,080	1,972
CLIMB (SL ISA MTOW)
Normal (fpm)	2,844	2,979	1,963	1,963	2,450
Engine Out (fpm)	867	912	452	452	740
SPEEDS (KNOTS)
Vs (Clean)	100	96	89	0	99
Vso (Landing)	81	81	75	83	75
Normal Cruise TAS	315	311	235	258	279
Vmo (Max Operating) IAS	259	263	226	223	270