Performance Specification

Make	CITATION	CITATION	CITATION	CITATION
Model	CJ2	ENCORE	EXCEL	ULTRA
Serial Number	ORIGINAL	ORIGINAL	ORIGINAL	ORIGINAL
ENGINES
Number	2	2	2	2
Make	WILLIAMS/ ROLLS	PRATT & WHITNEY	PRATT & WHITNEY	PRATT & WHITNEY
Model	FJ44-2C	PW535A	PW545A	JT15D-5D
Thrust LB Per Engine	2,400.00	3,400.00	3,804.00	3,045.00
Shaft HP Per Engine	0.00	0.00	0.00	0.00
Common TBO (hours)	3,500	5,000	5,000	3,500
FUSELAGE DIMENSIONS
Length	47.70	48.90	51.80	48.90
Height	13.90	15.20	17.20	15.00
Wing Span	49.80	54.10	55.70	52.20
TYPICAL CONFIGURATION
Crew	1	2	2	2
Passengers	8	7	8	7
Pressurization (psi)	8.90	8.90	8.90	8.90
WEIGHTS (LBS)
Max Ramp	12,500	16,830	20,200	16,500
Max Takeoff	12,375	16,630	20,000	16,300
Zero Fuel	9,300	12,600	15,000	12,200
Basic Operating	7,810	10,520	12,550	9,795
Max Landing	11,500	15,200	18,700	15,200
FUEL CAPACITY
Standard lbs/gal	3,930  /  586	5,400  /  805	6,050  /  2,744	5,771  /  861
Optional lbs/gal	0  /  0	0  /  0	0  /  0	0  /  0
TAKEOFF PERFORMANCE
SL ISA BFL (ft)	3,420	3,490	3,590	3,180
5000+20C BFL (ft)	5,080	5,750	4,730	4,730
LANDING PERFORMANCE
FAA Field Length	2,612	2,429	2,327	2,870
RANGE (NAUTICAL MILES)
Max Range (NBAA IFR)	1,530	1,702	1,581	1,960
CLIMB (SL ISA MTOW)
Normal (fpm)	3,870	4,640	3,090	4,230
Engine Out (fpm)	1,123	1,440	728	1,185
SPEEDS (KNOTS)
Vs (Clean)	0	0	94	94
Vso (Landing)	0	0	82	82
Normal Cruise TAS	372	393	373	430
Vmo (Max Operating) IAS	275	292	290	292