Piper Arrow

PIPER ARROW SPECIFICATIONS

(PA-28R0200)

Aircraft has transponder and DME P28R/A

The performance figures are examples only. Pilots are responsible for computing performance for a given flight, under the conditions that pertain then

Engine: Lycoming IO-360-C1C, four cylinder, direct drive, horizontally opposed, air cooled, fuel injected.
Rated Horsepower: 200 BHP at sea level
Rated Engine Speed: 2700 RPM

Max Gross Weight - 2650 lbs
Empty Weight - 1611 lbs
Useful Load - 1039 lbs
AVgas: 100LL, Aviation Grade
Fuel Capacity: 50 gal. total; 48 gal usable
Total Oil Capacity: 8 quarts
Operate with Oil at: 6 - 6 1/2 quarts

Cruise Speed - 144 kts; 165 mph
Max crosswind on landing - 20 K
Takeoff distance, ground roll (@5000 ft.) - 1700 ft.
Takeoff distance over 50 ft. obstacle (@ 5000 ft.) - 2400 ft.
Rate of climb - 620 fpm

Operating ceiling - 15,000 ft.
Landing distance, ground roll (@ 5000 ft.) - 900 ft.
Landing distance over 50 ft. obstacle (@ 5000 ft.) - 1440 ft.

Max flaps extended speed - 109 K
Max gear extended speed - 130 K
Max gear retraction speed - 109 K

Tire Pressures: Nose - 27 psi; Main - 30 psi
Strut Heights: Nose - 2.75 in.; Main 2 in.

Best angle of climb speed (@ sea level)- gear down 74K; geap up 84K
Best rate of climb speed (@ sea level) - gear up 83K ; gear up 87K K
Cruise climb - 96 K
Typical final approach speed - 75K
Maneuvering speed - 124 K, at 2650 lbs. gross wt. - 114K
Stall, clean - 62 K
Stall, full flaps - 56 K

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