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An-26

An-26

Military Transport Aircrafts
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Basic Information
Name
An-26
Designation
An-26
Alternate Designation
An-26B, An-26M, An-26SM, An-26ST, An-32 Cline, An-32B, An-32P, Curl, Y-7H, Y7H-500
Equipment Type
Military Transport Aircrafts
Manufacturer
Antonov ASTC
Date of Introduction
1970
Description

The An-26 tactical transport aircraft first flew in 1968 and entered service by 1970 with more than 1,400 airplanes built until production ceased in the 1980s. The An-26 aircraft features a rear loading ramp compared to the An-24 airliner. The An-26B is fitted with an improved freight handling system. The Y-7H light transport aircraft is a Chinese variant of the An-26 and the Y-7H-500 is the latest production standard. The aircraft is powered by more powerful AI-24VT turboprop engines. The An-26SM and An-26ST are signals intelligence (SIGINT) and electronic warfare (EW) variants. The An-26M is an electronic intelligence (ELINT) aircraft. The An-32, 'Cline' NATO name, is an upgraded version with engines mounted over the wings with increased diameter propellers and enhanced performance in 'hot-and-high'. The aircraft's payload was also increased to 6-7 tons. First flew in 1976 and is powered by AI-20D-5 engines while the turbojet APU is replaced by TG-16M. The An-32B introduced in 1993 is powered by more powerful engines AI-20D-5M. The An-32P is a firefighting aircraft. The existing An-26 twin-turboprop aircraft are being replaced by the more capable Il-112V, C-295 and C-27J light multirole transport aircraft. The Indian Air Force is upgrading its fleet of An-32 with assistance from Antonov. The Russian Air Force expects to replace their surviving An-26s by the Il-112B in the 2020-2025 timeframe.

Air & Air Defense Specifications
Crew 2
Max Speed 540.0 km/h
Range 2550.0 km
Service Ceiling 7500 m
Wingspan 29.20 m
Overview (Deagel)
Group Military Transport Aircrafts
Status Active
Also Known As An-26B, An-26M, An-26SM, An-26ST, An-32 Cline, An-32B, An-32P, Curl, Y-7H, Y7H-500
Origin Ukraine
Contractor Antonov ASTC
Initial Operational Capability (IOC) 1970
First Flight 1968
Total Production 1,400
Specifications (Deagel)
Crew 2
Number of Engines 2
Paratroops 42
Propeller Blades 4
Stretchers 24
Troops 50
Area — Wing Area 75.0 square meter
Dimensions — Height 8.6 meter
Dimensions — Length 23.8 meter
Dimensions — Wingspan 29.2 meter
Mass — Cargo 5,500 kilogram
Mass — Empty Weight 15,400 kilogram
Mass — Fuel Load 5,500 kilogram
Mass — Max Takeoff Weight 24,400 kilogram
Mass — Operational Weight 23,000 kilogram
Performance — Ceiling 7,500 meter
Performance — Landing Run Distance 730 meter
Performance — Max Range 2,550 kilometer
Performance — Min Range 1,100 kilometer
Performance — Operational Altitude 6,000 meter
Performance — Take Off Run Distance 1,240 meter
Power — Max Power at TakeOff 5,640 hp
Speed — Climb Rate 8 mps
Speed — Cruise Speed 440 kph
Speed — Top Speed at High Altitude 540 kph
Speed — Top Speed at Sea Level 510 kph
Time — Service Life 25 year
Gear (Deagel)
Item 1 Turboprop Engines: AI-20D-5 (2)
Item 2 Turboprop Engines: AI-24VT (2)
Variants
Variant 1 An-24
Variant 2 An-26
Details
Country of Origin Ukraine
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
23.8 m
Width
29.2 m
Height
8.6 m
Weight
24400 kg
Operators (38)
Russia
China
Germany
Ukraine
Poland
India
Iran
Czech Republic
Serbia
Afghanistan
Angola
Bangladesh
Benin
Bulgaria
Côte d'Ivoire
Cuba
Ethiopia
Guinea-Bissau
Hungary
Iraq
Laos
Latvia
Libya
Lithuania
Madagascar
Mali
Mauritania
Moldova
Mongolia
Mozambique
Nicaragua
Peru
Romania
Slovakia
Tanzania
Vietnam
Yemen
Zambia
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