Performance Specification

Make	CITATION	CITATION	CITATION	CITATION	CITATION
Model	500	525	CJ1	I	I/SP
Serial Number	ORIGINAL	ORIGINAL	ORIGINAL	ORIGINAL	ORIGINAL
ENGINES
Number	2	2	2	2	2
Make	PRATT & WHITNEY	WILLIAMS-ROLLS	WILLIAMS/ ROLLS	WILLAMS ROLLS RO	PRATT & WHITNEY
Model	JT15D-1	FJ44-1A	FJ44-1A	FJ44-2A	JT15D-1A
Thrust LB Per Engine	2,200.00	1,900.00	1,900.00	2,200.00	2,200.00
Shaft HP Per Engine	0.00	0.00	0.00	0.00	0.00
Common TBO (hours)	3,500	3,000	3,500	3,500	3,500
FUSELAGE DIMENSIONS
Length	43.50	42.60	42.60	43.50	43.50
Height	14.30	13.70	13.80	14.30	14.30
Wing Span	43.80	46.80	46.80	47.10	47.10
TYPICAL CONFIGURATION
Crew	2	2	1	2	1
Passengers	6	6	6	6	6
Pressurization (psi)	7.60	8.50	8.50	8.50	8.50
WEIGHTS (LBS)
Max Ramp	11,650	10,500	10,700	12,000	12,000
Max Takeoff	11,500	10,400	10,600	11,850	11,850
Zero Fuel	8,400	8,400	8,400	8,400	8,400
Basic Operating	5,856	6,900	6,860	7,403	6,670
Max Landing	11,000	9,700	9,800	11,350	11,350
FUEL CAPACITY
Standard lbs/gal	3,645  /  554	3,196  /  477	3,196  /  477	3,778  /  564	3,778  /  564
Optional lbs/gal	0  /  0	0  /  0	0  /  0	0  /  0	0  /  0
TAKEOFF PERFORMANCE
SL ISA BFL (ft)	3,275	3,280	3,280	2,930	2,930
5000+20C BFL (ft)	4,700	5,870	5,870	5,280	5,280
LANDING PERFORMANCE
FAA Field Length	2,310	2,486	2,486	2,270	2,270
RANGE (NAUTICAL MILES)
Max Range (NBAA IFR)	1,130	1,250	1,250	1,324	1,324
CLIMB (SL ISA MTOW)
Normal (fpm)	2,900	3,311	3,311	2,680	2,680
Engine Out (fpm)	906	868	868	800	800
SPEEDS (KNOTS)
Vs (Clean)	0	0	0	95	95
Vso (Landing)	76	82	82	82	82
Normal Cruise TAS	348	380	380	352	352
Vmo (Max Operating) IAS	287	260	260	275	260