Performance Specification

Make	PILATUS	SOCATA	STARSHIP
Model	PC-12	TBM-700	2000A
Serial Number	ORIGINAL	ORIGINAL	ORIGINAL
ENGINES
Number	1	1	2
Make	PRATT & WHITNEY	PRATT & WHITNEY	PRATT & WHITNEY
Model	PT6A-67B	PT6A-64	PT6A-67A
Thrust LB Per Engine	0.00	0.00	0.00
Shaft HP Per Engine	1,200.00	700.00	1,200.00
Common TBO (hours)	3,000	3,000	3,000
FUSELAGE DIMENSIONS
Length	47.30	34.90	46.10
Height	14.00	14.30	12.90
Wing Span	53.30	41.60	54.40
TYPICAL CONFIGURATION
Crew	2	1	2
Passengers	6	6	8
Pressurization (psi)	5.80	6.20	8.40
WEIGHTS (LBS)
Max Ramp	9,965	6,614	15,010
Max Takeoff	9,920	6,579	14,900
Zero Fuel	9,040	4,100	12,600
Basic Operating	3,295	4,500	10,485
Max Landing	9,920	6,250	13,680
FUEL CAPACITY
Standard lbs/gal	2,704  /  402	1,883  /  281	3,785  /  565
Optional lbs/gal	0  /  0	0  /  0	0  /  0
TAKEOFF PERFORMANCE
SL ISA BFL (ft)	2,300	2,133	3,854
5000+20C BFL (ft)	3,770	3,033	5,101
LANDING PERFORMANCE
FAA Field Length	1,830	2,034	2,390
RANGE (NAUTICAL MILES)
Max Range (NBAA IFR)	1,852	1,563	1,722
CLIMB (SL ISA MTOW)
Normal (fpm)	1,680	2,380	2,748
Engine Out (fpm)	0	0	670
SPEEDS (KNOTS)
Vs (Clean)	86	75	97
Vso (Landing)	59	61	92
Normal Cruise TAS	267	291	328
Vmo (Max Operating) IAS	270	270	335