Performance Specification

Make	HAWKER	HAWKER	HAWKER	HAWKER
Model	125-1A	125-3A	125-3A/RA	125-400A
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-731-3R-1H
Thrust LB Per Engine	3,880.00	3,880.00	3,880.00	3,880.00
Shaft HP Per Engine	0.00	0.00	0.00	0.00
Common TBO (hours)	5,500	5,500	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)	8.30	8.40	8.40	8.30
WEIGHTS (LBS)
Max Ramp	21,400	21,900	23,100	23,300
Max Takeoff	20,500	21,400	23,300	23,300
Zero Fuel	13,200	13,700	14,700	14,200
Basic Operating	11,000	12,000	13,800	12,500
Max Landing	19,550	20,000	20,000	20,000
FUEL CAPACITY
Standard lbs/gal	8,251  /  1,232	8,254  /  1,232	9,152  /  1,366	9,152  /  1,366
Optional lbs/gal	0  /  0	0  /  0	0  /  0	0  /  0
TAKEOFF PERFORMANCE
SL ISA BFL (ft)	3,600	4,800	3,800	4,090
5000+20C BFL (ft)	0	0	0	7,750
LANDING PERFORMANCE
FAA Field Length	0	0	2,450	1,960
RANGE (NAUTICAL MILES)
Max Range (NBAA IFR)	0	2,100	2,100	1,530
CLIMB (SL ISA MTOW)
Normal (fpm)	4,000	4,000	3,100	3,700
Engine Out (fpm)	0	0	656	1,042
SPEEDS (KNOTS)
Vs (Clean)	93	93	93	93
Vso (Landing)	110	110	110	77
Normal Cruise TAS	425	434	443	441
Vmo (Max Operating) IAS	290	285	285	285