page_title: Antonov An-3
section_title: Specifications (An-3T)
hierarchical_section_title: Antonov An-3 / Specifications (An-3T)
caption_attribution_description: English: Side silhouette views of the prototype Antonov An-3 and An-3V floatplane.
context_page_description: The Antonov An-3 is a Soviet civil multipurpose and agricultural aircraft. It is essentially a turboprop-powered development of the An-2, designed to upgrade or replace it. The basic transport version is supplemented by a cargo/passenger version, an agricultural version, a forest fire-fighting version, as well as an ambulance version. It is designed to carry passengers and cargo, operating from paved or unpaved airfields, including snow covered surfaces up to 35 cm.
context_section_description: Data from Antonov An-2
  General characteristics
  Crew: two
  Capacity: Useful Load 1,800kg (3,970lb)
  Length: 14 m (45 ft 11 in)
  Wingspan: 18.176 m (59 ft 8 in)
  Height: 4.235 m (13 ft 11 in)
  Wing area: 71.51 m² (769.7 sq ft)
  Max takeoff weight: 5,800 kg (12,787 lb)
  Powerplant: 1 × Glushenkov TVD-20-03 Turboprop, 1,010 kW (1,350 hp)
  Performance
  Maximum speed: 260 km/h (160 mph, 140 kn)
  Cruise speed: 220 km/h (140 mph, 120 kn) at 2,000m (6,560ft)
  Range: 550 km (340 mi, 300 nmi) with a 1,500kg (3,300lb) payload
  Service ceiling: 4,400 m (14,400 ft)
  Rate of climb: 5 m/s (980 ft/min)
  Wing loading: 81 kg/m² (17 lb/sq ft)
  Power/mass: 0.174kW/kg
caption: Antonov An-3
exif: {}