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PIPER PA-28R-201T TURBO ARROW
SPECIFICATIONS
ENGINES
Manufacturer Continental
Model TSIO-360-FB
Rating (hp @ rpm) (Take-off) 200 @ 2575
Rating (hp @ rpm) (Continuous) 200 @ 2575
Number of Cylinders 6
Recommended TBO (hrs) 1800
PROPELLERS
Manufacturer Hartzell
Number of Blades 2
Type Constant Speed
Diameter (in/cm) 76/193
WEIGHTS
Ramp Weight (lbs/kg) 2912/1321
Gross Weight (lbs/kg) 2900/1315
Standard Empty Weight (lbs/kg) 1667/756
(Includes unusable fuel, full operating fluids and full oil)
Standard Useful Load (lbs/kg) 1245/565
WING AREA AND LOADINGS
Wing Area (ft.2/m2) 170/15.8
Wing Loading (lbs/ft.2) (kg/m2) 17.0/83.0
Power Loading (lbs/hp)/(kg/hp) 14.5/6.6
DIMENSIONS
Wing Span (ft/m) 35.4/10.8
Length (ft/m) 25/7.6
Height (ft/m) 7.9/2.4
Cabin Length (Instrument Panel to Rear Bulkhead) (in/cm) 93.25/236.9
Cabin Width (in/cm) 41.75/106.1
Cabin Height (in/cm) 44.75/113.7
Headroom (Seat to Ceiling)
Front Seat (in/cm) 38/96.5
Rear Seat (in/cm) 34.5/87.6
Baggage Door Size (in/cm) 22/55.9 x 20/50.8
Cabin Door Size (in/cm) 36/91.4 x 35/88.9
Wheel Base (ft/m) 7.86/2.40
Wheel Tread (ft/m) 10.47/3.19
FUEL CAPACITY
Two 38.5 gal. tanks (gal/L) 77/291.4
Usable Fuel (gal/L) 72/272.5
OIL CAPACITY (qts/L) 8/7.57
BAGGAGE
Volume (ft3/m3) 26/.74
Capacity (lbs/kg) 200/91

PERFORMANCE
MAXIMUM SPEED (kts/kmh)   178/328 (14,000 ft)
(TAS at Gross Weight) (205 mph)
CRUISING SPEEDS Best Power Best Economy
(TAS at Gross Weight)
  Optimum Altitude    
High Speed Cruise Power - 75% (kts/kmh) 172/318 168/311
Economy Cruise Power - 65% (kts/kmh) 167/308 164/302
Long Range Cruise Power - 75% (kts/kmh) 157/291 154/285
CRUISE RANGE
(Cruising range includes 45-minute fuel reserve at long range cruise power plus
allowance for fuel used during taxi, take-off, climb at MCP, cruise at optimum
altitude and stated mixture and descent.)
Best Power Best Economy
High Speed Cruise Power - 75% (nm/km) 675/1245 785/1454
Economy Cruise Power - 65% (nm/km) 705/1300 830/1537
Long Range Cruise Power - 55%(nm/km) 740/1365 860/1590
FUEL CONSUMPTION Best Power Best Economy
High Speed Cruise Power - 75% (gph/lph) 14.0/53.0 12.0/45.4
Economy Cruise Power - 65% (gph/lph) 12.7/48.1 10.8/40.9
Long Range Cruise Power - 55% (gph/lph) 11.0/41.6 9.2/34.8
RATE OF CLIMB (At Sea Level and Gross Wt)
Full Power (fpm/mpm) 940/286
STALL SPEED IAS CAS
Flaps Down Full 40o (kts/kmh) 56/104 58/107
Flaps Up (kts/kmh) 63/116 63/117
SERVICE CEILING (100 fpm) (ft/m) 20,000+/6,100+*
TAKE-OFF DISTANCE
(Sea Level, Zero Wind, Standard Temperature, 25o flaps)
Ground Run (ft/m) 1110/337
Total over 50 ft obstacle (ft/m) 1620/493
LANDING DISTANCE
(Sea Level, Zero Wind, Standard Temperature)
Ground Roll (ft/m) 645/196
Total over 50 ft obstacle (ft/m) 1560/475
* 20,000 ft is maximum approved altitude for the Turbo Arrow.    
Reference: Piper Aircraft Corporation Brochure, Vero Beach, FL, 1 Nov. 1988
Given data is only for information. Please refer to the manufacturer for current data.
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