Piper 1999 PA-28-181 Archer III

Tuesday, January 01, 2008 at 12:00 AM ET

Verified

Edited By: Omar Filipović

Key Takeaways:

The article details the specifications of the 1999 Piper PA-28-181 Archer III, an aircraft powered by a 180 HP Lycoming O-360-A4M engine with a 2000-hour TBO.
This 4-seater aircraft features fixed landing gear and propeller, with a useful load of 847 lbs and a maximum gross weight of 2550 lbs.
Key performance figures include a cruise speed of up to 125 knots (at 65% power) and a maximum range of 487 nautical miles (at 65% power with reserve).
It boasts a service ceiling of 14,100 feet, a stall speed of 45 knots, and requires a takeoff ground roll of 1135 ft and a landing ground roll of 920 ft.

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Piper 1999 PA-28-181 Archer III

Engine make/model:

Lyc. O-360-A4M

Horsepower:

180

TBO hrs.:

2000

Propeller:

Fixed

Landing gear type:

Tri/Fixed

Gross weight (lbs.):

2550

Empty weight, std. (lbs.):

1703

Useful load, std. (lbs.):

847

Fuel (gals.):

48

Wingspan:

35 ft. 6 in.

Overall length:

24 ft.

Height:

7 ft. 4 in.

Wing area (sq. ft.):

171.8

Seating capacity:

4

Cabin width (in.):

42

Cabin height (in.):

45

Baggage capacity (lbs.):

100

PERFORMANCE

Cruise speed (kts.):

75% power:

120

65% power:

125

Max range (w/ reserve) (nm):

75% power:

444

65% power:

487

Fuel consumption (gph):

75% power:

10.0

65% power:

8.6

Estimated endurance (65% power with 1-hr. reserve):

4 hrs. 42 mins.

Stall speed (gear, flaps down) (knots):

45

Best rate of climb (fpm):

667

Service ceiling (ft.):

14,100

Takeoff ground roll (ft.):

1135

Landing ground roll (ft.):

920

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