
Piper
Contact
NORTH TEXAS
Larry Johnson
Phone 214-467-6063
Fax: 214-467-6067
ljohnson@cutteraviation.com
SOUTH TEXAS
John DeLawyer
Phone 210-384-3381
Fax: 210-340-8804
jdelawyer@cutteraviation.com
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.
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.
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.
PERFORMANCE SPECIFICATIONS
Manufacturer
Model
Horsepower
Lycoming
IO-360-A4M
180 hp
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
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
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.