Performance Specification

Make	GULFSTREAM	GULFSTREAM	GULFSTREAM
Model	G-II	G-IIB	G-III
Serial Number	ORIGINAL	ORIGINAL	ORIGINAL
ENGINES
Number	2	2	2
Make	ROLLS ROYCE	ROLLS-ROYCE	ROLLS-ROYCE
Model	SPEYMK 511-8	SPEYMK 511-8	SPEYMK 511-8
Thrust LB Per Engine	11,400.00	11,400.00	11,400.00
Shaft HP Per Engine	0.00	0.00	0.00
Common TBO (hours)	8,000	7,000	7,000
FUSELAGE DIMENSIONS
Length	79.90	79.90	83.10
Height	24.60	24.50	24.30
Wing Span	68.90	77.80	77.80
TYPICAL CONFIGURATION
Crew	2	2	2
Passengers	11	11	14
Pressurization (psi)	9.50	9.50	9.50
WEIGHTS (LBS)
Max Ramp	65,300	68,700	70,200
Max Takeoff	64,800	68,200	69,700
Zero Fuel	42,000	42,000	44,000
Basic Operating	36,944	38,550	38,000
Max Landing	58,500	58,500	58,500
FUEL CAPACITY
Standard lbs/gal	23,300  /  3,478	27,900  /  4,164	28,300  /  4,224
Optional lbs/gal	0  /  0	0  /  0	0  /  0
TAKEOFF PERFORMANCE
SL ISA BFL (ft)	56,250	5,115	5,115
5000+20C BFL (ft)	0	0	8,000
LANDING PERFORMANCE
FAA Field Length	3,200	3,250	3,250
RANGE (NAUTICAL MILES)
Max Range (NBAA IFR)	2,592	3,680	3,691
CLIMB (SL ISA MTOW)
Normal (fpm)	4,345	4,049	4,049
Engine Out (fpm)	1,520	1,403	1,105
SPEEDS (KNOTS)
Vs (Clean)	102	100	122
Vso (Landing)	108	104	108
Normal Cruise TAS	459	459	459
Vmo (Max Operating) IAS	367	340	340