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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