Performance Specification

Make	HAWKER	HAWKER	HAWKER	HAWKER
Model	125-1AS	125-3A/RAS	125-3AS	125-400AS
Serial Number	ORIGINAL	ORIGINAL	ORIGINAL	ORIGINAL
ENGINES
Number	2	2	2	2
Make	GARRETT	GARRETT	GARRETT	GARRETT
Model	TFE-731-3R-1H	TFE731-3R-1H	TFE-731-3R-1H	TFE-731-3R-1H
Thrust LB Per Engine	3,880.00	3,880.00	3,880.00	3,700.00
Shaft HP Per Engine	0.00	0.00	0.00	0.00
Common TBO (hours)	5,500	5,000	5,500	5,500
FUSELAGE DIMENSIONS
Length	47.40	47.40	47.40	47.40
Height	16.50	16.50	16.50	16.50
Wing Span	47.00	47.00	47.00	47.00
TYPICAL CONFIGURATION
Crew	2	2	2	2
Passengers	6	7	7	7
Pressurization (psi)	8.40	8.40	8.40	8.40
WEIGHTS (LBS)
Max Ramp	21,900	23,100	21,900	23,300
Max Takeoff	21,400	23,300	21,400	23,300
Zero Fuel	13,700	14,700	13,700	14,200
Basic Operating	12,000	13,800	12,000	12,595
Max Landing	19,550	20,000	20,000	20,000
FUEL CAPACITY
Standard lbs/gal	8,254  /  1,232	9,152  /  1,366	8,254  /  1,232	9,152  /  1,366
Optional lbs/gal	0  /  0	0  /  0	0  /  0	0  /  0
TAKEOFF PERFORMANCE
SL ISA BFL (ft)	4,800	3,800	4,800	5,100
5000+20C BFL (ft)	0	0	0	0
LANDING PERFORMANCE
FAA Field Length	0	2,450	0	1,990
RANGE (NAUTICAL MILES)
Max Range (NBAA IFR)	2,100	2,100	2,100	2,100
CLIMB (SL ISA MTOW)
Normal (fpm)	4,000	3,100	3,000	3,500
Engine Out (fpm)	0	656	0	0
SPEEDS (KNOTS)
Vs (Clean)	93	93	93	0
Vso (Landing)	110	110	110	77
Normal Cruise TAS	434	443	434	436
Vmo (Max Operating) IAS	285	285	285	270