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| PIPER PA-28-161 WARRIOR II |
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| SPECIFICATIONS |
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| ENGINES |
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Manufacturer |
Lycoming |
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Model |
O-320-D3G |
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Rating (hp @ rpm) |
160 @ 2700 |
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Number of Cylinders |
4 |
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Recommended TBO (hrs) |
2000 |
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| PROPELLERS |
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Manufacturer |
Sensenich |
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Number of Blades |
2 |
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Type |
Fixed Pitch |
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Diameter (in/cm) |
74/188 |
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| WEIGHTS |
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Ramp Weight (lbs/kg) |
2447/1110 |
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Gross Weight (lbs/kg) |
2440/1107 |
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Standard Empty Weight (lbs/kg) |
1348/611 |
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(Includes unusable fuel, full operating fluids and full oil) |
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Standard Useful Load (lbs/kg) |
1099/499 |
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| WING AREA AND LOADINGS |
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Wing Area (ft.2/m2) |
170/15.8 |
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Wing Loading (lbs/ft.2) (kg/m2) |
14.4/70.1 |
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Power Loading (lbs/hp)/(kg/hp) |
15.3/6.9 |
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| DIMENSIONS |
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Wing Span (ft/m) |
35.0/10.7 |
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Length (ft/m) |
23.8/7.3 |
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Height (ft/m) |
7.3/2.2 |
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Cabin Length (Instrument Panel to Rear Bulkhead) (in/cm) |
98/248.9 |
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Cabin Width (in/cm) |
41.25/104.8 |
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Cabin Height (in/cm) |
44.25/112.4 |
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Headroom (Seat to Ceiling) |
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Front Seat (in/cm) |
38/96.5 |
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Rear Seat (in/cm) (optional) |
34/86.4 |
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Baggage Door Size (in/cm) |
22/55.9 x 20/50.8 |
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Cabin Door Size (in/cm) |
36/91.4 x 35/88.9 |
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Wheel Base (ft/m) |
6.67/2.03 |
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Wheel Tread (ft/m) |
10/3.05 |
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| FUEL CAPACITY |
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Two 25 gal. tanks (gal/L) |
50/189 |
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Usable Fuel (gal/L) |
48/182 |
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| OIL CAPACITY (qts/L) |
8/7.57 |
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| BAGGAGE |
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Volume (ft3/m3) |
24/.68 |
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Capacity (lbs/kg) |
200/91 |
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| PERFORMANCE |
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| MAXIMUM SPEED (kts/kmh) |
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(TAS at Mid Cruise Weight) |
127/235 |
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| CRUISING SPEEDS |
Best Power |
Best Economy |
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(TAS at Mid Cruise Weight) |
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75% at 9,000 ft (kts/kmh) |
126/233 |
122/226 |
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65% at 12,500 ft (kts/kmh) |
118/219 |
116/215 |
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55% at 12,500 ft (kts/kmh) |
107/198 |
105/195 |
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| CRUISE RANGE |
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(Cruising range includes 45-minute fuel reserve at max. range power plus
allowance for fuel used during taxi, take-off, climb at MCP, cruise at stated
mixture and descent) |
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Best Power |
Best Economy |
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75% at 9,000 ft (nm/km) |
525/973 |
590/1093 |
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65% at 12,500 ft (nm/km) |
553/1024 |
633/1173 |
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55% at 12,000 ft (nm/km) |
565/1047 |
640/1186 |
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| FUEL CONSUMPTION |
Best Power |
Best Economy |
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75% power (gph/lph) |
10.0/37.9 |
8.5/32.2 |
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65% power (gph/lph) |
8.8/33.3 |
7.5/28.4 |
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55% power (gph/lph) |
7.8/29.5 |
6.6/25 |
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| RATE OF CLIMB (At Sea Level and Gross Wt) |
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Full Throttle (fpm/mpm) |
644/196 |
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| STALL SPEED |
IAS |
CAS |
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Flaps Down Full 40o (kts/kmh) |
44/82 |
50/93 |
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Flaps Up (kts/kmh) |
50/93 |
56/104 |
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| SERVICE CEILING (100 fpm) (ft/m) |
11,000/3353 |
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| TAKE-OFF DISTANCE |
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(Sea Level, Zero Wind, Standard Temperature, 25o flaps) |
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Ground Run (ft/m) |
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1050/320 |
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Total over 50 ft obstacle (ft/m) |
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1650/503 |
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| LANDING DISTANCE |
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(Sea Level, Zero Wind, Standard Temperature) |
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Ground Roll (ft/m) |
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625/191 |
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Total over 50 ft obstacle (ft/m) |
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1160/353 |
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Reference: Piper Aircraft Corporation Brochure, Vero Beach, FL, 1 Nov. 1988 |
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Given data is only for information. Please refer to the manufacturer for current
data. |
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