Piper Aztec F
PA 23-250
The Piper PA-23 is a six-seat twin-engine light aircraft aimed at the general aviation market that also saw service with the United States Navy and other countries’ military forces in small numbers.
General characteristics.
. Crew: one (two upon request)
. Capacity: 5 passengers
. Payload: 1600 lb (725 kg) Cargo 300lbs
. Length: 31 ft (9.52 m)
. Wingspan: 37 ft (11.34 m )
. Height: 10 ft (3.35 m)
. Wing area: 207.6 ft2 (19.28 m2)
. Airfoil: YSA 35-b (modified)
. Aspect ratio: 6.8:1
. Empty weight: 3180 lb (1442 kg)
. Max . takeoff weight: 5200lb (2360 kg)
. Powerplant: 2 X Lycoming IO-C4B5 normally aspirated air cooled flat six piston engines, 250 hp (187kW) each
. Propellers: two bladed hartzell HC- E2YK-2RB constant speed propeller
Piper PA-23 F Aztec – Performance Data
Horsepower: 250
Gross Weight: 5200 lbs
Top Speed: 178 kts
Empty Weight: 3184 lbs
Cruise Speed: 160 kts
Fuel Capacity: 177 gal
Stall Speed (dirty): 55 kts
Range: 1519 nm
Takeoff
Ground Roll: 1190 ft.
Over 50 ft obstacle: 1980 ft
Landing
Ground Roll 951 ft
Over 50 ft obstacle: 1585 ft
Rate Of Climb: 1470 fpm
Ceiling: 18950 ft
Rate of Climb (One Engine): 225 fpm
Ceiling (One Engine): 17000 ft