Seneca III - Aero Resources Inc

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PiperAircraftCorporation1984Spec ifica ti 0nsf Pe rfo r m.a n ceSeneca IIIPA-34-220T

28'7.«"-I1g' 10.5"STATIC GROUND LINEr6'4.90'!n10'3.43" -38'10.87"12'5.4",........... ~ 6'4" DIAMETER7° DIHEDRAL

Piper Aircraft CorporationSeneca III PA-34-220TSpecificationsENGINESManufacturerModelRatings (hp @ rpm)Take-off Power (5 Min. Limit)Maximum Continuous PowerNumber of CylindersRecommended TBO (hrs.)PROPELLERSManufacturerNumber of BladesTypeDiameter (in./cm.)WEIGHTSRamp Weight (lbs./kg)Gross Take-off Weight (lbs./kg)Gross Landing Weight (Ibs./kg)Standard Empty Weight (Ibs./kg)(Includes: unusable fuel. full oil and fulloperating fluids)Standard Useful Load (lbs./kg)WING AREA AND LOADINGSWing Area (ft.2/m2)Wing Loading (lbs./ft.2)/(kg/m2)Power Loading (lbs./hp)/(kg/hp)ContinentalTSIO-360-KB & LTSIO-360-KB220 @ 2800200 @ 260061800Hartzell2Constant Speed. Full Feathering76/1934773/21 654750/2154451 3/20472852/12941921/871208.7/19.422.8/111.010.8/4.9DIMENSIONSWing Span (ft./m)Length (ft./m)Height (ft./m)Cabin Length (Instrument panel to rear bulkhead)(in./cm.)Cabin Width (in./cm.)Cabin Height (in./cm.)Headroom (Seat to Ceiling)Front Seats (in./cm.)Middle Seats (in./cm.)Rear Seats (in./cm)Forward Baggage Door Size (in./cm)Aft Baggage/Utility Door Size (in./cm)Forward Cabin Door Size (in./cm)Aft Cabin Door Size (in./cm)Wheel Base (ft./m)Wheel Tread (ft./m)FUEL CAPACITYTotal Capacity (gal./L)Usable Fuel (gal./L)OIL CAPACITY (qts./L)BAGGAGEVolume (ft.3/m3)Forward CompartmentAft CompartmentCapacity (Ibs./kg)Forward CompartmentAft CompartmentStandard Fuel98/37193/35138.9/11.928.6/8.79.9/3.0125.0/317.549.0/124.542.0/106.738/96.536.5/90.834.5/87.621/53.3 x 24/61.020.5/52.1 x 26/66.035/88.9 x 36/91.428.5/72.4 x 28/71.17/2.1311.1/3.39OptionalFuel128/484123/4668/7.5715.3/.4317.3/.49100/45.4100/45.4PerformanceMAXIMUM SPEED (kts/kmh)(TAS at Mid-Cruise Weight) 196/363CRUISING SPEEDS 10.000 ft. Opt. Altitude(TAS at Mid-Cruise Weight)High Speed Cruise Power (75%) 179/332 193/358(kts/kmh)Economy Cfuise Power (65%) 175/324 191/354(kts/kmh)'Long Range Cruise Power (45%) 143/265 168/311(kts/kmh)CRUISE RANGE(Cruising range includes 45 minute reserve at long rangecruise power plus allowance for fuel used during taxi. take-off,climb at MCP. cruise and descent)High Speed Cruise Power (75%)(nm/km)Economy Cruise Power (65%)(nm/km)Long Range Cruise Power (45%)(nm/km)High Speed Cruise Power (75%)(nm/km)Economy Cruise Power (65%)(nm/km)Long Range Cruise Power (45%)(nm/km)OptimumStandard fuelAltitudeOptional Fuel462/300 665/1232550/1019670/124210.000 foot AltitudeStandard Fuel Optional Fuel450/834 640/1186535/1020632/1171785/1455990/1835760/1400900/1168FUEL CONSUMPTIONHigh Speed Cruise Power (75%)(gph/lph)Economy Cruise Power (65%)(gph/lph)Long Range Cruise Power (45%)(gph/lph)RATE OF CLIMB(At Sea Level and Gross Wt.)Two Engine (fpm/mpm)Single Engine (fpm/mpm)STALL SPEEDFlaps Down Full 40° (kts./kmh)Flaps Up (kts./k.mh)SERVICE CEILING (MCP POWER)Two Engines (100 fpm) (ft./m)Single Engine (50 fpm) (fUm)TAKE-OFF DISTANCE(Sea Level, Zero Wind, StandardTemperature. 25° Flaps)Ground Run (ft./m)Total Distance over 50 ft. Obstacle (ft./m)LANDING DISTANCE(Sea Level, Zero Wind, StandardTemperature)Ground Roll (ft./m)Total Distance over 50 ft. Obstacle(fUm)ACCELERATE-STOP DISTANCE(Sea Level. Zero Wind. StandardTemperature. 25° Flaps) (ft./m)Takeoff PowerIAS64/11967/124Std. Brake.2160/658Std. Brake.29.0/11023.3/8816.0/611400/427 1300/396240/73 200/611400/4272400/732Continuous PowerCAS62/11566/122*25.000+/7620+12,300/3749920/2801210/369H.D. Brakes1218/3711978/603H.D Brakes2088/636* 25.000 feet is the maximum approved altitude for the Seneca III