Performance Specification

Make	HAWKER	HAWKER	HAWKER	HAWKER
Model	125-600A	125-600AS	125-700A	800A
Serial Number	ORIGINAL	ORIGINAL	ORIGINAL	ORIGINAL
ENGINES
Number	2	2	2	2
Make	GARRETT	GARRETT	GARRETT	GARRETT
Model	TFE-731-3R-1H	TFE-731-3R-1H	TFE-731-3R-1H	TFE-731-5R-1H
Thrust LB Per Engine	3,750.00	3,880.00	3,880.00	4,500.00
Shaft HP Per Engine	0.00	0.00	0.00	0.00
Common TBO (hours)	4,000	4,200	4,200	4,200
FUSELAGE DIMENSIONS
Length	50.50	50.50	50.70	51.10
Height	17.30	17.30	17.60	17.60
Wing Span	47.00	47.00	47.00	51.40
TYPICAL CONFIGURATION
Crew	2	2	2	2
Passengers	8	8	8	8
Pressurization (psi)	8.40	8.40	8.40	8.60
WEIGHTS (LBS)
Max Ramp	25,000	25,000	25,000	27,520
Max Takeoff	25,000	25,000	24,800	27,400
Zero Fuel	15,550	15,550	16,050	17,520
Basic Operating	13,603	13,755	14,550	16,000
Max Landing	22,000	22,000	22,000	23,350
FUEL CAPACITY
Standard lbs/gal	9,507  /  1,419	9,501  /  1,418	9,500  /  1,418	10,016  /  1,495
Optional lbs/gal	0  /  0	0  /  0	0  /  0	0  /  0
TAKEOFF PERFORMANCE
SL ISA BFL (ft)	5,530	5,800	5,800	5,600
5000+20C BFL (ft)	7,550	0	6,950	9,400
LANDING PERFORMANCE
FAA Field Length	2,125	2,125	3,600	2,800
RANGE (NAUTICAL MILES)
Max Range (NBAA IFR)	1,620	2,660	2,330	2,415
CLIMB (SL ISA MTOW)
Normal (fpm)	4,900	0	4,900	3,500
Engine Out (fpm)	1,380	0	1,493	780
SPEEDS (KNOTS)
Vs (Clean)	96	96	104	115
Vso (Landing)	83	83	87	105
Normal Cruise TAS	435	435	424	424
Vmo (Max Operating) IAS	320	292	320	320