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PIPER PA-28-161 WARRIOR II

SPECIFICATIONS

ENGINES
Manufacturer Lycoming
Model O-320-D3G
Rating (hp @ rpm) 160 @ 2700
Number of Cylinders 4
Recommended TBO (hrs) 2000
PROPELLERS
Manufacturer Sensenich
Number of Blades 2
Type Fixed Pitch
Diameter (in/cm) 74/188
WEIGHTS
Ramp Weight (lbs/kg) 2447/1110
Gross Weight (lbs/kg) 2440/1107
Standard Empty Weight (lbs/kg) 1348/611
(Includes unusable fuel, full operating fluids and full oil)
Standard Useful Load (lbs/kg) 1099/499
WING AREA AND LOADINGS
Wing Area (ft.2/m2) 170/15.8
Wing Loading (lbs/ft.2) (kg/m2) 14.4/70.1
Power Loading (lbs/hp)/(kg/hp) 15.3/6.9
DIMENSIONS
Wing Span (ft/m) 35.0/10.7
Length (ft/m) 23.8/7.3
Height (ft/m) 7.3/2.2
Cabin Length (Instrument Panel to Rear Bulkhead) (in/cm) 98/248.9
Cabin Width (in/cm) 41.25/104.8
Cabin Height (in/cm) 44.25/112.4
Headroom (Seat to Ceiling)
Front Seat (in/cm) 38/96.5
Rear Seat (in/cm) (optional) 34/86.4
  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) 6.67/2.03
Wheel Tread (ft/m) 10/3.05
FUEL CAPACITY
Two 25 gal. tanks (gal/L) 50/189
Usable Fuel (gal/L) 48/182
OIL CAPACITY (qts/L) 8/7.57
BAGGAGE
Volume (ft3/m3) 24/.68
Capacity (lbs/kg) 200/91


PERFORMANCE

MAXIMUM SPEED (kts/kmh)
(TAS at Mid Cruise Weight) 127/235
CRUISING SPEEDS Best Power Best Economy
(TAS at Mid Cruise Weight)
75% at 9,000 ft (kts/kmh) 126/233 122/226
65% at 12,500 ft (kts/kmh) 118/219 116/215
55% at 12,500 ft (kts/kmh) 107/198 105/195
CRUISE RANGE
(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)
Best Power Best Economy
75% at 9,000 ft (nm/km) 525/973 590/1093
65% at 12,500 ft (nm/km) 553/1024 633/1173
55% at 12,000 ft (nm/km) 565/1047 640/1186
FUEL CONSUMPTION Best Power Best Economy
75% power (gph/lph) 10.0/37.9 8.5/32.2
65% power (gph/lph) 8.8/33.3 7.5/28.4
55% power (gph/lph) 7.8/29.5 6.6/25
RATE OF CLIMB (At Sea Level and Gross Wt)
Full Throttle (fpm/mpm) 644/196
STALL SPEED IAS CAS
Flaps Down Full 40o (kts/kmh) 44/82 50/93
Flaps Up (kts/kmh) 50/93 56/104
SERVICE CEILING (100 fpm) (ft/m) 11,000/3353
TAKE-OFF DISTANCE
(Sea Level, Zero Wind, Standard Temperature, 25o flaps)
Ground Run (ft/m) 1050/320
Total over 50 ft obstacle (ft/m) 1650/503
LANDING DISTANCE
(Sea Level, Zero Wind, Standard Temperature)
Ground Roll (ft/m) 625/191
Total over 50 ft obstacle (ft/m) 1160/353
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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