33006 - 1985 ANTONOV AN 2CX

1985

ANTONOV

AN-2CX

1G21746

33006

Used

Dimensions: Length= 41 feet, 9 inches; Wing Span= 59 feet, 8 inches; Height= 13 feet, 2 inches (tail down). Total Wing Lift Area=256.6 sq. ft. 156.2 upper 100.4 lower Cargo compartment= 13.5 feet long by 5 feet wide by 5.9 feet tall (398.25 cubic feet). Cargo door opening: 4.5 feet wide by 5 feet tall. Weights: Empty= 7,600 lbs.; Max Take Off= 12,125 lbs.; Max Landing= 11,574 lbs.; Max fuel= 2,000 lbs. (312 USG); Oil Qty.=22 Gallons Max. (13 Gallons minimum to 18 Gallons normal.) Useful load with max fuel= 2,525 lbs. (3500 lbs with half fuel carried). PERFORMANCE: Red Line Speed: V-NE 162 kts. White Line Flaps: V-FE 70 kts. Best Glide: 65 kts. Maximum Speed: 139kts. or 160mph. (120kts. more typical) Economy Cruise Speed: 100kts. or 115mph. (95kts. more typical) Minimum Speed: 49kts. or 56mph. Take-Off Speed: 43kts. or 50mph. (15 degrees of flap). Landing Speed: 46kts. or 53mph. (30 degrees of flap). Stall Speed: 35-40kts. but controlled descents are possible at 25kts. or 30mph. Typical SL Take-Off distance to clear 50 foot obstacle: 1600 feet. Great STOL performance! Take off is possible under 300 feet. The biggest biplane @ price of a home car! Original agriculture spraying configuration!

3414.0

3414 Hr. Total time Wings are of an unequal span single bay biplane design, all metal construction, with fabric covering. Fuselage is of all-metal stressed skin semi-monocoque construction. Tail is a braced all metal structure with fabric covering. Wing area is 770 square feet total. Brand new fabric (Ceconite) Aircraft has been completely inspected and restored by professional mechanics. Controls: Ailerons, rudder, and elevators are all manually controlled with pushrods and cables. Flaps and trim electrically operated. Automatic leading edge slats provide excellent slow speed safety and high lift. Landing Gear: Conventional configuration (tail wheel design) with split axle, long stroke oleo shock absorbers on the main mounts and a fully castoring.

392

SMOH

1,000-hp Shvetsov 9 cyl. ASh-62 radial piston engine 392 hr SMOH

More projects considered, transport, parachute-dropping configurations.

All original (RU) avionics.