Performance Specification

Make	KING AIR	KING AIR	KING AIR	KING AIR
Model	C90	C90A	E90	F90
Serial Number	ORIGINAL	ORIGINAL	ORIGINAL	ORIGINAL
ENGINES
Number	2	2	2	2
Make	PRATT & WHITNEY	PATT & WHITNEY	PRATT & WHITNEY	PRATT & WHITNEY
Model	PT6A-20	PT6A-21	PT6A-28	PT6A-135
Thrust LB Per Engine	0.00	0.00	0.00	0.00
Shaft HP Per Engine	550.00	550.00	550.00	750.00
Common TBO (hours)	3,600	3,600	3,600	3,600
FUSELAGE DIMENSIONS
Length	35.50	35.50	35.50	39.80
Height	14.30	14.30	14.30	15.10
Wing Span	50.30	50.30	50.30	45.90
TYPICAL CONFIGURATION
Crew	2	2	2	2
Passengers	7	7	7	7
Pressurization (psi)	5.00	5.00	5.00	5.00
WEIGHTS (LBS)
Max Ramp	9,710	10,160	10,160	11,030
Max Takeoff	9,650	10,100	10,100	10,950
Zero Fuel	8,879	9,389	0	9,600
Basic Operating	6,165	6,780	6,452	7,169
Max Landing	9,168	9,600	9,700	10,950
FUEL CAPACITY
Standard lbs/gal	2,573  /  384	2,573  /  384	3,176  /  474	3,149  /  470
Optional lbs/gal	0  /  0	0  /  0	0  /  0	0  /  0
TAKEOFF PERFORMANCE
SL ISA BFL (ft)	2,261	2,577	2,024	2,856
5000+20C BFL (ft)	3,600	4,400	0	4,500
LANDING PERFORMANCE
FAA Field Length	1,672	1,672	2,110	2,275
RANGE (NAUTICAL MILES)
Max Range (NBAA IFR)	1,120	1,120	1,290	1,235
CLIMB (SL ISA MTOW)
Normal (fpm)	1,955	2,137	1,870	2,380
Engine Out (fpm)	539	626	470	600
SPEEDS (KNOTS)
Vs (Clean)	89	88	0	94
Vso (Landing)	76	78	77	77
Normal Cruise TAS	217	240	245	251
Vmo (Max Operating) IAS	208	226	226	253