An-24

Turboprop Airplanes

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Basic Information

Name

An-24

Designation

An-24

Alternate Designation

An-24P, An-24RT, An-24RV, An-24T, An-24V, An-30 Clank, Coke, Y-7, Y7-100, Y7-200A/B

Equipment Type

Turboprop Airplanes

Manufacturer

Antonov ASTC

Date of Introduction

1963

Description

The Antonov An-24, 'Coke' NATO name, is a twin-turboprop passenger aircraft developed in the late 1950s and early 1960s by the Antonov design bureau in the former Soviet Union. The aircraft was designed to carry 30-50 passengers replacing the Il-12, Il-14 and Li-2 airplanes in the civil passenger aircraft market. The An-26, 'Curl' NATO name, is a new design based upon the An-24 but intended to serve as a tactical military transport aircraft. In the 1970s China started building its own version of the An-24 and An-26 aircraft called Y-7 and Y-7H respectively. These aircraft (all An-26s and some An-24s) are equipped with a RU-19A-300 turbojet Auxiliary Power Unit (APU) in the rear of the engine nacelle developing 1,765-lb of thrust that helps them to takeoff. So far more than 2,500 An-24/26/Y-7 aircraft and a variety of upgraded and mission specific versions have been built for a wide range of customers worldwide.

Air & Air Defense Specifications

Crew 2

Max Speed 450.0 km/h

Range 3000.0 km

Service Ceiling 8400 m

Wingspan 29.20 m

Overview (Deagel)

Group Turboprop Airplanes

Status Active

Also Known As An-24P, An-24RT, An-24RV, An-24T, An-24V, An-30 Clank, Coke, Y-7, Y7-100, Y7-200A/B

Origin Ukraine

Contractor Antonov ASTC

Initial Operational Capability (IOC) April 1963

First Flight December 20, 1959

Total Production 1,100

Specifications (Deagel)

Crew 2

Number of Engines 2

Passengers 50

Propeller Blades 4

Area — Wing Area 72.5 square meter

Dimensions — Height 8.3 meter

Dimensions — Length 23.5 meter

Dimensions — Wingspan 29.2 meter

Mass — Empty Weight 14,060 kilogram

Mass — Fuel Load 4,760 kilogram

Mass — Max Takeoff Weight 19,800 kilogram

Mass — Operational Weight 14,968 kilogram

Mass — Payload 4,612 kilogram

Performance — Ceiling 8,400 meter

Performance — Landing Run Distance 880 meter

Performance — Max Range 3,000 kilometer

Performance — Min Range 640 kilometer

Performance — Operational Altitude 7,000 meter

Performance — Take Off Run Distance 640 meter

Power — Max Power at TakeOff 5,100 hp

Speed — Cruise Speed 450 kph

Gear (Deagel)

Item 1 Turboprop Engines: AI-24A (2)

Variants

Variant 1 An-24

Variant 2 An-26

Details

Country of Origin Ukraine

Sources

deagel.com: https://www.deagel.com/x/x/a002598

Classification

Domain

Air & Air Defense

Equipment Status

Active

Dimensions

Length

23.5 m

Width

29.2 m

Height

8.3 m

Weight

19800 kg

Operators (21)

Russia

China

Ukraine

North Korea

Czech Republic

Afghanistan

Angola

Bulgaria

Cambodia

Cuba

Hungary

Iraq

Laos

Mali

Moldova

Mongolia

Romania

Slovakia

Sudan

Vietnam

Yemen

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