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Piper PA28-181 Archer III
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Manufacturer
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Lycoming
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Model
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O-360-A4M
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Horsepower
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180 hp
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Number of Cylinders
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4
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Manufacturer
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Sensenich
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Number of Blades
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2
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Type
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Fixed Pitch
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Maximum Take-off Weight
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2,550 lbs/1,157 kg
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Standard Empty Equipped
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Weight (b and c)
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1,682 lbs/763 kg
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Standard Useful Load (a)
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876 lbs/397 kg
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a. Standard useful load is maximum ramp weight minus standard equipped weight.
b. The standard empty weight and standard equipped weight are the same.
c. Standard equipped aircraft.
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Wing Span
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35.5 ft/10.8 m
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Length
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24.0 ft/7.32 m
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Height
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7.3 ft/2.2 m
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Cabin Length
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98 in/248.9 cm
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(Instrument Panel to Rear Bulkhead)
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Cabin Width
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41.75 in/106.0 cm
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Cabin Height
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45.0 in/114.3 cm
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Headroom (Seat to Ceiling)
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Front Seat
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38 in/96.5 cm
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Rear Seat
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34.5 in/87.6 cm
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Wing Area
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171.8 ft2/16 m2
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Usable Fuel
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48 gal/182 liters
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Oil Capacity
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8 qts/7.57 liters
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Gross Weight, Sea Level,
Best Power Mixture
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133 kts/246 km/h
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75% Power, 7,900 ft
Best Power Mixture
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128 kts/237 km/h
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Cruising range includes 45 minute fuel reserve at long range cruise power plus allowance for fuel used during taxi, take-off, climb at maximum climb power and cruise at stated mixture and descent.
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75% @ sea level
65% @ sea level
55% @ sea level
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444 nm/822 km
487 nm/902 km
522 nm/967 km
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Flaps Full Down 40°
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45 kts/83 km/h
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(100fpm)
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14,100 ft/4,298 m
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Volume
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26 ft3/0.74 m3
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Capacity
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200 lbs/91 kg
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Ground Roll
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1,135 ft/346 m
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Total over 50 ft obstacle
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1,608 ft/490 m
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(Flaps 25°, 2,550 lbs)
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Ground Roll
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920 ft/280 m
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Total over 50 ft obstacle
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1,400 ft/427 m |
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