Tupolev Tu-134

Public Joint Stock Company Tupolev

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Tupolev Tu-134 aircraft
Public Joint Stock Company TupolevTupolev Tu-134
Photo: Barristacuber · CC BY-SA 3.0 · Modified

Details

The Tupolev Tu-134 is a Soviet twin-engine narrow-body jet airliner designed for short and medium-haul routes, serving as a workhorse of Soviet and Eastern Bloc aviation from the 1960s through the 1990s. First flown in July 1963 and entering service in September 1967, the Tu-134 was developed as a successor to the Tu-124, featuring a distinctive rear-mounted twin-engine configuration with Soloviev D-30 turbofan engines and a T-tail design. The aircraft is characterized by its twin Soloviev D-30-II low-bypass turbofan engines mounted on the rear fuselage, a swept wing with anhedral (negative dihedral), retractable tricycle landing gear suitable for unpaved runways, and glazed nose on early variants housing the navigator station (later replaced with conventional radar nose on Tu-134A onwards). The Tu-134 family includes the original Tu-134 with glazed nose (72 passengers, 34.3m length), the stretched Tu-134A (1970) with 2.1m fuselage extension for 84 passengers and conventional nose, and the Tu-134B (1980) with improved avionics and capacity for up to 96 passengers. Production ran from 1966 to 1989 at the Kharkiv Aviation Factory, with 854 aircraft built including prototypes, serving Aeroflot and numerous Soviet bloc airlines. The Tu-134 became one of the most successful Soviet airliners, providing reliable service on domestic and regional international routes throughout Eastern Europe, and continuing limited operations into the 21st century. NATO reporting name: "Crusty".

3

Variants

854

Built

Weightscompared to Boeing 757-300

MTOW (Maximum Takeoff Weight)

47,600kg
0
50k
100k
124k

MLW (Maximum Landing Weight)

43,000kg
0
50k
102k

Empty Weight

29,050kg
0
50k
100k

Capacitycompared to Boeing 757-300

Passenger Capacity

96passengers
0
100
200
295

33% of 757-300 maximum capacity

Crew

Total
5
Cockpit
3
Cabin
2

Dimensions

Length

37.0m

Wingspan

29.0m

Height

9.1m

Wing Area

127.3m²

Cabin Width

2.71m

Engine Specifications

Engine Count

2×

Engine Model

Soloviev D-30-II

Thrust per Engine

67.0 kN(15062 lbf)

Fuel & Cargo

Fuel Capacity

13,249 L

Cargo Volume

14.5 m³

Production & History

Total Produced

854

Production Status

Out of production

Manufacturing Period

1966–1989

First Flight

July 29, 1963

Entered Service

September 9, 1967

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