Turbo Arrow IV PA 28RT-201 T Specifications - Aero Resources Inc
Turbo Arrow IV PA 28RT-201 T Specifications - Aero Resources Inc
Turbo Arrow IV PA 28RT-201 T Specifications - Aero Resources Inc
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PiperAircraftCorporation1984Spec ificati on sl Perform an ce<strong>Turbo</strong> <strong>Arrow</strong> <strong>IV</strong><strong>PA</strong> <strong>28RT</strong>-<strong>201</strong> T
1'3.12"~"'-1"'4:---110.32"--211.15"!T3'1.12"_J
Piper AircraftCorporation<strong>Turbo</strong> <strong>Arrow</strong> <strong>IV</strong> <strong>PA</strong> <strong>28RT</strong>-<strong>201</strong> T<strong>Specifications</strong>ENGINEManufacturerModelRating (hp @ rpm) (Take-off)Rating (hp @ rpm) (Continuous)Number of CylindersRecommended TBO (hrs.)PROPELLERManufacturerNumber of BladesTypeDiameter (in./cm.)WEIGHTSRamp Weight (Ibs./kg.)Gross Weight (Ibs.lkg.)Standard Empty Weight (Ibs.lkg.)(<strong>Inc</strong>ludes; unusable fuel, full operating fluidsand full oil)Standard Useful Load (Ibs./kg.)WING AREA AND LOADINGSWing Area (ft2/m2)Wing Loading (lbs./ft.2) (kg./m2)Power Loading (Ibs./hp) (kg./hp)PerformanceContinentalTSIO-360-FB200 @ 2575200 @ 2575618001Hartzell2Constant Speed76/1932912/13212900/13151692/7671208/548170/15.817.0/83.014.5/6.6DIMENSIONSWing Span (ft.lm)Length (It./ m)Height (fUm)Cabin Length (Instrument Panel to Rear Bulkhead)(in./cm.)Cabin Width (in.lcm.)Cabin Height (in./cm.)Headroom (Seat to Ceiling)Front Seat (in.lcm.)Rear Seat (in.lcm.)Baggage Door Size (in.lcm.)Cabin Door Size (in.lcm.)Wheel Base (ft.lm)Wheel Tread (ft.lm)FUEL CA<strong>PA</strong>CITYTwo 38.5 gal. tanks (gaL/L)Usable Fuel (gaL/L)OIL CA<strong>PA</strong>CITY (qts.lL)BAGGAGEVolume (ft3/m3)(with 2 cu. ft. hat shelf)Capacity (Ibs./kg.)35.4/10.827.3/8.38.3/2.593.25/236.941.75/106.144.75/113.738/96.5- 34.5/87.622/55.9 x 20/55.836/91.4 x 35/88.97.86/2.4010.47/3.1977/291.472/272.58/7.5726/.74200/91MAXIMUM SPEED (kts.lkmh)178/328 (14,000 ft.)(TAS at Gross Weight)(205 mph)CRUISING SPEEDSBest Power Best Economy(TAS at Gross Weight)Optimum AltitudeHigh Speed Cruise Power (75%)(kts./kmh)Economy Cruise Power (65%)(kts./kmh)Long Range Cruise Power (55%)(kts./kmh)CRUISE RANGE172/318167/308157/291168/311164/302153/284(Cruising range includes 45-minute fuel reserve at long rangecruise power plus allowance for fuel used during taxi, take-offclimb at MCP, cruise at optimum altitude and stated mixtureplus descent)High Speed Cruise Power (75%)(nm/km)Economy Cruise Power (65%)(nm/km)Long Range Cruise Power (55%)(nm/km)Best Power695/1278725/1343775/1435Best Economy790/1463830/1537900/1667FUEL CONSUMPTIONHigh Speed Cruise Power (75%)(gph.llph)Economy Cruise Power (65%)(gph.llph)Long Range Cruise Power (55%)(gph.llph)Best Powe r14.0/53.012.7/48.111.0/41.6RATE OF CLIMB (At Sea Level and Gross Wt.)Full Throttle (fpm/mpm)STALL SPEEDFlaps Down, Full 40° (kts.lkmh)Flaps Up (kts.lkmh)SERVICE CEILING (100 fpm) (ft./m)TAKE-OFF DISTANCE(Sea Level, Zero Wind, Standard Temperature,25° Flaps)Ground Run (ft./m)Total over 50-ft. obstacle (ft.lm)LANDING DISTANCE(Sea.Level, Zero Wind, Standard Temperature)Ground Roll (ft.lm)Total over 50-ft. obstacle (ft.lm)BestEconomy12.0/45.410.8/40.99.2/34.8940/286IASCAS61/113 58/10766/122 63/11720,000+ /6100+*1110/3371620/493645/1961560/475*20,000 ft. is maximum approved altitude for the <strong>Turbo</strong> <strong>Arrow</strong> <strong>IV</strong>.
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