Please spend some time with all our web links to see more data for all An2 for Sale:

http://www.avioservicebgltd.com/

CURRENT HAVE 12 , AN2 , Aircrafts FOR SALE!

AN-2 TECHNICAL DATA

Wing span upper, lower 18.18m, 14.24m
Length Overall (tail up), (tail down) 12.71m, 12.40m
Height overall (tail up), (tail down) 6.10m, 4.00m
Wheel track 3.45m
Propeller diameter 3.60m
Propeller ground clearance 0.69m
Wing area 71.6m
Cargo door (port) mean height, mean width 1.55m, 1.39m
Dimensions internal:
Cargo compartment length, Max height, Max width
4.10m, 1.80m, 1.60m

 
 WEIGHTS AND LOADINGS
Weight empty 3450kg
Max T-O weight 5500kg
Useful load 2050kg
Maximum fuel weight 900kg
Max wing loading 78.82kg/m
Max power loading 5.5kg/hp
Performance (at AUW of 5250 kg)
Max level speed at 1500 m 253km/h
Econ. cruising speed 185km/h
Stalling speed 90km/h
Max rate of climb at S/L 3m/s
Service ceiling 4400m
T-O run. (grass) 170m
T-O to 10.7, m (grass) 320m
Landing run (grass) (hard runway) 185m, 170m
Range at 1000m with 700 kg payload 1370

Great STOL performance! Take off is possible under 105 m! Landing distance 140 m!

Fuel burn /AVGAS/: 125 kg (200 L) per hour; 45 kg/hr on ground
Max operational altitude: 4200 m

Airframe:
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.

Engine Specs:
1,000-hp Shvetsov 9 cyl. ASh-62IR radial piston engine

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.

INTERIOR:

Aircraft is for parachute jumping and cargo configurations!
Possible to put equip for  agricultural spraying.