Performance Specification

Make	MITSUBISHI	MITSUBISHI	MITSUBISHI	MITSUBISHI
Model	MARQUISE	MU-2F	MU-2J	SOLITAIRE
Serial Number	ORIGINAL	ORIGINAL	ORIGINAL	ORIGINAL
ENGINES
Number	2	2	2	2
Make	GARRETT	GARRETT	GARRETT-	GARRETT
Model	TPE-331-10-501M	TPE-331-1-151A	TPE-331-10AV	TPE-331-10-501M
Thrust LB Per Engine	0.00	0.00	0.00	0.00
Shaft HP Per Engine	778.00	665.00	724.00	727.00
Common TBO (hours)	5,400	3,600	5,400	5,400
FUSELAGE DIMENSIONS
Length	39.40	33.30	39.50	33.30
Height	13.70	12.90	13.80	12.90
Wing Span	39.20	39.20	39.20	39.20
TYPICAL CONFIGURATION
Crew	2	2	2	2
Passengers	7	7	7	6
Pressurization (psi)	6.00	5.00	5.00	6.00
WEIGHTS (LBS)
Max Ramp	11,625	9,920	10,850	10,520
Max Takeoff	11,575	9,920	10,800	10,470
Zero Fuel	9,950	3,420	9,950	9,700
Basic Operating	9,985	7,200	7,700	7,410
Max Landing	11,025	9,435	10,260	9,955
FUEL CAPACITY
Standard lbs/gal	2,700  /  403	2,251  /  336	2,452  /  366	2,700  /  403
Optional lbs/gal	0  /  0	2,452  /  366	0  /  0	0  /  0
TAKEOFF PERFORMANCE
SL ISA BFL (ft)	2,170	2,415	1,870	1,800
5000+20C BFL (ft)	4,375	3,445	0	4,700
LANDING PERFORMANCE
FAA Field Length	1,880	1,320	1,670	1,600
RANGE (NAUTICAL MILES)
Max Range (NBAA IFR)	1,391	1,356	1,150	1,600
CLIMB (SL ISA MTOW)
Normal (fpm)	2,200	2,875	2,690	2,350
Engine Out (fpm)	410	920	845	475
SPEEDS (KNOTS)
Vs (Clean)	99	93	93	93
Vso (Landing)	77	71	73	73
Normal Cruise TAS	296	270	265	313
Vmo (Max Operating) IAS	250	250	250	250