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Leading the Business of Aviation for 80 Years

Piper



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Contact


NORTH TEXAS
Larry Johnson
Phone 972-562-5555
Fax: 214-467-6067
ljohnson@cutteraviation.com

SOUTH TEXAS
John DeLawyer
Phone 210-601-5246
Fax: 210-340-8804
jdelawyer@cutteraviation.com

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Piper Archer III

With great pleasure, we invite you to experience the New Piper Archer III.  As the cornerstone of Piper's fleet, the Archer III continues to command the respect & admiration of Pilots worldwide.

Archer3 

PERFORMANCE SPECIFICATIONS

 

ENGINE
Manufacturer
Model
Horsepower


Lycoming
IO-360-A4M
180 hp

WEIGHTS
Maximum Takeoff Weight
Standard Empty Equipped Weight (b and c)
Standard Useful Load (a)


2550 lbs/1157 kg
1689 lbs/766 kg
861 lbs/391 kg

DIMENSIONS
Wing Span
Length
Height
Wing Area


35.5 ft/10.8 m
24.0 ft/7.32 m
7.3 ft/2.2 m
171.8 ft2/16 m2

FUEL CAPACITY
Usable Fuel
MAXIMUM SPEED
Gross Weight, Best Power Mixture
CRUISING SPEEDS
75% Power, Best Power Mixture
CRUISING RANGE
45 minute reserves at 55% power, @ sea level, peak EGT mixture

 
48 gal/182 liters
TAS
133 kts/246 km/h
TAS
128 kts/237 km/h

522 nm/967 km

STALL SPEED
Flaps Down Full 40°
SERVICE CEILING
100 FPM
TAKE-OFF DISTANCE
Total over 50 ft Obstacle
LANDING DISTANCE
Total over 50 ft Obstacle

IAS
45 kts/83 km/h

14,100 ft/4,298 m

1135 ft/346 m

1400 ft/427 m

a. Standard useful load is maximum takeoff weight minus standard equipped weight.
b. The standard empty weight and standard equipped weight are the same.
c. Standard equipped aircraft.