PERFORMANCE SPECSMU-2 Series AircraftMake MITSUBISHI MITSUBISHI MITSUBISHI MITSUBISHIModel MARQUISE MU-2F MU-2J SOLITAIRESerial Number ORIGINAL ORIGINAL ORIGINAL ORIGINAL

ENGINESNumber 2 2 2 2Make GARRETT GARRETT GARRETT- GARRETTModel TPE-331-10-501M TPE-331-1-151A TPE-331-10AV TPE-331-10-501MThrust LB Per Engine 0.00 0.00 0.00 0.00Shaft HP Per Engine 778.00 665.00 724.00 727.00Common TBO (hours) 5,400 3,600 5,400 5,400

FUSELAGE DIMENSIONSLength 39.40 33.30 39.50 33.30Height 13.70 12.90 13.80 12.90Wing Span 39.20 39.20 39.20 39.20

TYPICAL CONFIGURATIONCrew 2 2 2 2Passengers 7 7 7 6Pressurization (psi) 6.00 5.00 5.00 6.00

WEIGHTS (LBS)Max Ramp 11,625 9,920 10,850 10,520Max Takeoff 11,575 9,920 10,800 10,470Zero Fuel 9,950 3,420 9,950 9,700Basic Operating 9,985 7,200 7,700 7,410Max Landing 11,025 9,435 10,260 9,955

FUEL CAPACITYStandard lbs/gal 2,700 / 403 2,251 / 336 2,452 / 366 2,700 / 403Optional lbs/gal 0 / 0 2,452 / 366 0 / 0 0 / 0

TAKEOFF PERFORMANCESL ISA BFL (ft) 2,170 2,415 1,870 1,8005000+20C BFL (ft) 4,375 3,445 0 4,700

LANDING PERFORMANCEFAA 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 2,350Engine Out (fpm) 410 920 845 475

SPEEDS (KNOTS)Vs (Clean) 99 93 93 93Vso (Landing) 77 71 73 73Normal Cruise TAS 296 270 265 320Vmo (Max Operating) IAS 250 250 250 250