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AN-74 (Coaler-B) Ukrainian Transport/Passenger Aircraft

AN-74

Twin-Engine Utility Aircraft
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Basic Information
Name
AN-74 (Coaler-B) Ukrainian Transport/Passenger Aircraft
Designation
AN-74
Alternate Designation
Equipment Type
Twin-Engine Utility Aircraft
Manufacturer
Antonov
Date of Introduction
1983
Description

AN-74 (Coaler-B) is a Ukrainian transport aircraft developed by Antonov. It is a variant of the An-72. The An-72 and An-74 get their nickname, Cheburashka, from the large engine intake ducts, which resemble the oversized ears of the popular Soviet animated mouse character of the same name. The An-74 was initially an upgrade of the An-72 test aircraft, intended to be used in the Arctic and Antarctica; and had the designation An-72A "Arctic". The aircraft's main purpose is to deliver cargo, equipment, and personnel over short- and medium-range routes in any climatic conditions ranging from −60 to 45 °C (−76 to 113 °F) and at any latitude, including the North Pole, and high altitudes. It can operate to and from low-grade airstrips such as concrete, pebble, ice, and snow aerodromes. Produced in tandem with the An-72, the An-74 can be fitted with wheel-ski landing gear, de-icing equipment, and a number of other upgrades allowing the aircraft to support operations in the Arctic or Antarctic environments. An unusual design feature of the An-74 (as well as An-72) is the use of the Coandă effect to improve STOL performance, utilizing engine exhaust gases blown over the wing's upper surface to boost lift. The powerplant used is the Lotarev D-36 turbofan engine. The An-74 bears some resemblance to the unsuccessful Boeing YC-14, a prototype design from the early 1970s which had also used overwing engines. The rear fuselage of the aircraft has a hinged loading ramp with a rear fairing that slides backward and up to clear the opening. The An-74 has a payload of 7.5 tons including up to ten passengers in the cargo version, or up to 52 seats in the passenger version; the operating ceiling is 10,100 meters (33,100 ft), and the cruising speed is 550 to 700 kilometers per hour (300 to 380 kn; 340 to 430 mph).

Air & Air Defense Specifications
Crew 5
Engine Turbofan (63 hp)
Range 4325.0 km
Payload Capacity 10000 kg
Variants
An-74 Arctic/Antarctic support model with room for five crew, increased fuel capacity, larger radar in bulged nose radome, improved navigation equipment, better de-icing equipment, and can be fitted with wheel-skis landing gear.
An-74A Passenger or freighter model.
An-74MP Marine Patrol version. Can transport 44 soldiers, 22 paratroops, 16 stretchers with medical staff, or ten tons of cargo.
An-74T Freighter version equipped with an internal winch, roller equipment, and cargo mooring points, can also be fitted with static lines for paratroops or dropping air cargo.
An-74T-100 Variant of the An-74T fitted with a navigator station.
An-74D INA
An-74-100 Variant of the An-74T fitted with a navigator station.
An-74-200 Military transport based on the An-74T.
An-74TK Convertible passenger/cargo model that can be equipped for up to 52 passengers, all cargo, or a mix of the two.
An-74TK-100 Variant of the An-74TK fitted with a navigator station.
An-74TK-200 Variant of the An-74TK configured for only two flight crew.
An-74TK-200C Cargo variant of An-74TK-200.
An-74T-200 Military Transport aircraft.
An-74T-200A Military Transport aircraft.
An-74TK-300 An-74TK model primarily for civil customers with more fuel-efficient engines on conventional underwing pylons that gives up the STOL capabilities of earlier models in favor of lower operating cost and higher speed, also incorporates improved avionics and passenger comfort features.
An-74TK-300D An An-74 with engines fitted underneath the wings.
An-74-400 Proposed stretch model of the An-74TK-300 with a fuselage insert to extend its length by 26 ft (8 m), also would be equipped with uprated engines.
System
Alternate Designation(s) An-74; NATO: Coaler-B; Nickname: Cheburashka
Type Transport Aircraft
Manufacturer Antonov
Crew 5 (captain, first officer, navigator, flight engineer, loadmaster)
Passengers 52 ea
Number of Engines 2 ea
Number of Hard Points INA
Payload Capacity 10,000 kg
Loading Ramp The An-74 has a hinged loading ramp at the rear.
Landing Gear Tricycle retractable
Note The aircraft may also be used for highly specialized operations: pilotage and vessel escort; establishing and servicing of drifting stations; research operations in Arctic or Antarctic regions; visual ice patrol; fishery reconnaissance.
Dimensions
Length 28.07 m
Height 8.65 m
Width (Wing Span) 31.89 m
Wing Area 98.62 m sq
Cabin Length 10.50 m
Cabin Height 2.20 m
Cabin Width 2.15 m
Maximum Payload 10,000 kg
Maximum Takeoff Weight 34,500 kg
Automotive
Engine Name 2 x Lotarev D-36
Engine Type Turbofan
Engine Power 63.9 kN (14,330 lbf) thrust each
Maximum Range 4,325 km
Maximum Cruise Speed 700 km/h
Normal Cruise Speed 550 km/h
Approach Speed 180 km/h
Ceiling 10,100 m
Takeoff Roll 1,170 m to 10.7 m at 34,500 kg
Communications
HF Radio 1 x "Arlekin" DA HR Radio
VHF Radio 2 x VHF Radios
Main Weapon System
Note There are no weapons mounted on the An-74 (Coaler-B) Russian Transport/Passenger Aircraft.
Protection
Stealth Properties None
Heat Signature Reduction No
Add on Armor No
EW Counter Measures INA
Chaffs/Flares INA
Details
Country of Origin Russia
Category Fixed Wing Aircraft
Air > Fixed Wing Aircraft
Filter Label
A
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
28.07 m
Width
31.89 m
Height
8.65 m
Weight
34500 kg
Operators (5)
Russia
Ukraine
Iran
Egypt
Turkmenistan
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