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Yak-42 (Clobber) Russian Jet Airliner

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Basic Information
Name
Yak-42 (Clobber) Russian Jet Airliner
Designation
Alternate Designation
Equipment Type
Manufacturer
Saratov Aviation Plant
Date of Introduction
1975
Description

The Yakovlev Yak-42 (Russian: Яковлев Як-42; NATO reporting name: "Clobber") is a 100/120-seat three-engined mid-range passenger jet. It was the first airliner produced in the Soviet Union to be powered by modern high-bypass turbofan engines

Air & Air Defense Specifications
Crew 2
Engine Turbofan (63 hp)
Max Speed 810.0 km/h
Range 4000.0 km
Service Ceiling 9600 m
Variants
Yak-42 Original production version. Max. takeoff weight 54,000 kg (119,050 lb).
Yak-42ML Version with modified avionics for use on international use (mezhdunarodnyye linii – international services). Entered service in July 1981 on the Leningrad-Helsinki route.
Yak-42D Long-range version (Dahl'niy – long range) increased fuel. Replaced standard Yak-42 in production.
Yak-142 Derivative of Yak-42D with updated, western AlliedSignal avionics, spoilers to allow faster descent and enlarged cabin door to accommodate jet bridge. Also designated Yak-42A, Yak-42-100 and Yak-42D-100.
Yak-42R Yak-42 used as testbed for radar for Yakovlev Yak-141 fighter.
Yak-42F Conversion of a Yak-42 for geophysical survey and environmental monitoring. Fitted with large underwing pods containing electro-optical sensors.
Yak-42LL Conversion as testbed for Progress D-236 propfan engine. Single D-236 (rated at 8,090 kW (10,850shp)) mounted in place of starboard engine, on special pylon to give sufficient clearance for 4.2 m (13 ft 9¾ in) propellers. First flew 15 March 1991.
Yak-42M A projected but unbuilt stretched airliner. Planned to be powered by three Progress D-436 turbofans, a stretched fuselage and new wings. Design developed into Yak-242.
Yak-242 Further developed Yak-42M, with two underwing Aviadvigatel PS-90 turbofans. Design evolved into Irkut MC-21.
System
Alternate Designation(s) Yak-42; NATO: Clobber
Primary Function / Type Jet Airliner
Manufacturer Saratov Aviation Plant
Crew 2 pilots plus optional flight engineer
Passengers up to 120 passengers (normally eight first class and 96 economy class)
Number of Engines 3
Number of Hard Points INA
Dimensions
Length 36.38 m
Height 9.83 m
Width (Wing Span) 34.88 m
Wing Area 150 m2
Empty Weight 33,000 kg
Maximum Takeoff Weight 57,500 kg
Automotive
Engine Name 3 × Lotarev D-36
Number of Engines 3
Engine Type Turbofan
Engine Power 63.75 kN (14,330 lbf) thrust each
Maximum Range 4,000 km
Maximum Speed 810 km/h
Service Ceiling 9,600 m
Fire Control / Avionics
Fire Control System Type INA
Fire Control Radar None
Navigation Radar INA
Protection
Stealth Properties None
Heat Signature Reduction No
Add on Armor No
NBC Protection No
EW Counter Measures No
Chaffs/Flares No
Details
Country of Origin Russia
Category Fixed Wing Aircraft
Air > Fixed Wing Aircraft
Filter Label
Y
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
36.38 m
Width
34.88 m
Height
9.83 m
Weight
57500 kg
Operators (2)
Russia
China
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