Antonov

Antonov An-3 Super Colt

Transport

13 May 1980

  • First flight13 May 1980
  • Introduction21 november 2000
  • StatusOperational
  • Number built28

History

The Antonov An-3 is a Soviet (later Ukrainian and Russian) 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 (An-3T) is supplemented by a cargo/passenger version (An-3TK), an agricultural version (An-3SH), a forest fire-fighting version (An-3P), as well as an ambulance version.[1][2] It is designed to carry passengers and cargo, operating from paved or unpaved airfields, including snow covered surfaces up to 35 cm (14 in) deep (using a ski landing gear).[3]

Upgrading

The upgrading consisted of replacement of the piston engine with a 1,025 kW (1,375 shp) TVD-20 turboprop engine, featuring a three-blade reversible pitch (type AV-17) propeller and a R-17 speed governor. The flight compartment was rearranged; a heating and ventilation system was installed as well as advanced electric and flight and navigation equipment; centralized warning system; a new fire extinguishing system; and an improvement of the external wide-spreading dispensing equipment for agricultural needs. The upgrades allowed the aircraft to be more reliable and to increase the cargo lifting capacity of the aircraft by 20%, as well as ensuring more comfortable conditions for the crew, including the lowering of the noise and vibration inside the cockpit. The rate of climb was increased by 1.9 times, and the take-off and landing performance of the aircraft was increased. The upgrading allowed the use of kerosene and lubricants commonly used for other aircraft instead of gasoline.[2] The take-off weight and payload was also increased and the upgrade allowed the landing performance to use ground strips 500 metres (1,600 ft) long.[1] The upgrading was arranged at both the “Polyot” Production Association in Omsk, Russian Federation, and at Antonov ASTC, Kyiv, Ukraine.[3]

The first example flew as early as May 13, 1980, but because of a lack of official interest in the project, work proceeded very slowly. Flight testing was not complete until 1991. It is one of the few turbine-powered biplane designs to date. The An-3T received its Type Certificate on 31 August 2000. Supplements to the Type Certificate included version with ski landing gear and an agricultural version.[

Technical data

Specifications

01

Crew & dimensions

Crew
2
Length
14 m (45 ft 11 in)
Wingspan
18.176 m (59 ft 8 in)
Height
4.235 m (13 ft 11 in)
02

Performance

Maximum speed
260 km/h (160 mph, 140 kn)
Range
550 km (340 mi, 300 nmi) with a 1,500 kg (3,300 lb) payload
Service ceiling
4,400 m (14,400 ft)
03

Powerplant

Powerplant
1 × Glushenkov TVD-20-03 Turboprop ( hp / 1,010 kW / lbf / kN / lbf with afterburner)
04

Developed from

Developed from
Antonov An-2