HOME OF THE SMALL AIRCRAFT


   
PIPER PA-28R-201 ARROW

SPECIFICATIONS

ENGINES
Manufacturer Lycoming
Model IO-360-C1C6
Rating (hp @ rpm) (Take-off) 200 @ 2700
Rating (hp @ rpm) (Continuous) 196 @ 2650
Number of Cylinders 4
Recommended TBO (hrs) 1600
PROPELLERS
Manufacturer McCauley
Number of Blades 2
Type Constant Speed
Diameter (in/cm) 76/193
WEIGHTS
Ramp Weight (lbs/kg) 2760/1252
Gross Weight (lbs/kg) 2750/1249
Standard Empty Weight (lbs/kg) 1612/731
(Includes unusable fuel, full operating fluids and full oil)
Standard Useful Load (lbs/kg) 1148/521
WING AREA AND LOADINGS
Wing Area (ft.2/m2) 170/15.8
Wing Loading (lbs/ft.2) (kg/m2) 16.2/79.1
Power Loading (lbs/hp)/(kg/hp) 13.7/6.2
DIMENSIONS
Wing Span (ft/m) 35.4/10.8
Length (ft/m) 24.7/7.5
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)   152/282 (S.L.)
(TAS at Gross Weight) (175 mph)
CRUISING SPEEDS Best Power Best Economy
(TAS at Gross Weight)
  Optimum Altitude    
High Speed Cruise Power - 75% (kts/kmh) 143/265 135/250
Economy Cruise Power - 65% (kts/kmh) 138/256 129/239
Long Range Cruise Power - 75% (kts/kmh) 131/243 122/226
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) 725/1343 810/1500
Economy Cruise Power - 65% (nm/km) 770/1426 845/1565
Long Range Cruise Power - 55%(nm/km) 795/1472 875/1620
FUEL CONSUMPTION Best Power Best Economy
High Speed Cruise Power - 75% (gph/lph) 11.6/43.9 10.2/38.6
Economy Cruise Power - 65% (gph/lph) 10.4/39.4 9.2/34.8
Long Range Cruise Power - 55% (gph/lph) 9.1/34.4 8.0/30.3
RATE OF CLIMB (At Sea Level and Gross Wt)
Full Power (fpm/mpm) 831/254
STALL SPEED IAS CAS
Flaps Down Full 40o (kts/kmh) 55/101 55/101
Flaps Up (kts/kmh) 60/111 60/111
SERVICE CEILING (100 fpm) (ft/m) 16,200/4950
TAKE-OFF DISTANCE
(Sea Level, Zero Wind, Standard Temperature, 25o flaps)
Ground Run (ft/m) 1025/313
Total over 50 ft obstacle (ft/m) 1600/487
LANDING DISTANCE
(Sea Level, Zero Wind, Standard Temperature)
Ground Roll (ft/m) 615/187
Total over 50 ft obstacle (ft/m) 1525/465
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.

[Home] [Aircraft List]

2004 - 2009 - aeroengineer.net