Performance Specification

Make	LEARJET	LEARJET	LEARJET	LEARJET
Model	55	55B	55C	60
Serial Number	ORIGINAL	ORIGINAL	ORIGINAL	ORIGINAL
ENGINES
Number	2	2	2	2
Make	GARRETT	GARRETT	GARRETT	PRATT & WHITNEY
Model	TFE-731-3A-2B	TFE-731-3A-2B	TFE-731-3A-2B	PW305A
Thrust LB Per Engine	3,700.00	3,700.00	3,700.00	4,600.00
Shaft HP Per Engine	0.00	0.00	0.00	0.00
Common TBO (hours)	4,200	4,200	4,200	5,000
FUSELAGE DIMENSIONS
Length	55.10	55.10	55.10	58.70
Height	14.70	14.70	14.70	14.70
Wing Span	43.80	43.80	43.80	43.80
TYPICAL CONFIGURATION
Crew	2	2	2	2
Passengers	8	8	8	8
Pressurization (psi)	9.40	9.40	9.40	9.40
WEIGHTS (LBS)
Max Ramp	19,750	21,750	21,250	23,750
Max Takeoff	19,500	21,500	21,000	23,500
Zero Fuel	15,000	15,000	15,000	17,000
Basic Operating	12,530	12,855	13,258	14,700
Max Landing	17,000	18,000	18,000	19,500
FUEL CAPACITY
Standard lbs/gal	6,707  /  1,001	6,707  /  1,001	6,707  /  1,001	7,910  /  1,180
Optional lbs/gal	0  /  0	0  /  0	0  /  0	0  /  0
TAKEOFF PERFORMANCE
SL ISA BFL (ft)	5,600	5,600	4,900	5,450
5000+20C BFL (ft)	6,900	6,900	6,375	8,520
LANDING PERFORMANCE
FAA Field Length	3,300	3,300	3,250	3,420
RANGE (NAUTICAL MILES)
Max Range (NBAA IFR)	2,296	2,250	2,222	2,428
CLIMB (SL ISA MTOW)
Normal (fpm)	4,059	4,059	4,176	4,500
Engine Out (fpm)	1,000	1,000	1,240	1,340
SPEEDS (KNOTS)
Vs (Clean)	126	136	129	129
Vso (Landing)	103	114	106	107
Normal Cruise TAS	419	419	419	453
Vmo (Max Operating) IAS	350	350	350	340