Performance Specification

Make	CITATION	CITATION	CITATION	CITATION	CITATION
Model	BRAVO	II	II/SP	S/II	V
Serial Number	ORIGINAL	ORIGINAL	ORIGINAL	ORIGINAL	ORIGINAL
ENGINES
Number	2	2	2	2	2
Make	PRATT & WHITNEY	PRATT & WHITNEY	PRATT & WHITNEY	PRATT & WHITNEY	PRATT & WHITNEY
Model	PW530A	JT15D-4	JT15D-4	JT15D-4B	JT15D-5A
Thrust LB Per Engine	2,750.00	2,500.00	2,500.00	2,500.00	2,900.00
Shaft HP Per Engine	0.00	0.00	0.00	0.00	0.00
Common TBO (hours)	4,000	3,500	3,500	3,500	3,500
FUSELAGE DIMENSIONS
Length	47.20	47.20	47.20	47.20	48.90
Height	15.00	15.00	15.00	15.00	15.00
Wing Span	52.00	52.20	52.20	52.20	52.20
TYPICAL CONFIGURATION
Crew	2	2	1	2	2
Passengers	7	7	7	8	7
Pressurization (psi)	8.90	8.70	8.70	8.80	8.90
WEIGHTS (LBS)
Max Ramp	14,300	13,500	12,700	15,300	16,100
Max Takeoff	14,100	13,300	12,500	15,100	15,900
Zero Fuel	11,000	9,500	11,000	11,200	11,200
Basic Operating	8,223	8,200	7,648	8,459	9,350
Max Landing	13,500	12,700	12,000	14,400	15,200
FUEL CAPACITY
Standard lbs/gal	4,971  /  742	4,971  /  742	4,971  /  742	5,782  /  863	5,771  /  861
Optional lbs/gal	0  /  0	0  /  0	0  /  0	0  /  0	0  /  0
TAKEOFF PERFORMANCE
SL ISA BFL (ft)	3,460	2,990	2,990	3,240	3,160
5000+20C BFL (ft)	5,330	6,300	6,300	6,490	4,490
LANDING PERFORMANCE
FAA Field Length	2,295	2,270	2,270	2,640	2,870
RANGE (NAUTICAL MILES)
Max Range (NBAA IFR)	1,551	1,760	1,250	1,970	1,960
CLIMB (SL ISA MTOW)
Normal (fpm)	3,195	3,070	3,370	3,040	3,684
Engine Out (fpm)	998	1,055	1,055	860	1,332
SPEEDS (KNOTS)
Vs (Clean)	100	94	95	0	94
Vso (Landing)	83	84	84	82	82
Normal Cruise TAS	336	384	375	410	425
Vmo (Max Operating) IAS	275	275	260	276	292