Tupolev

Tupolev Tu-124

The Tupolev Tu‑124, introduced in 1962, was the Soviet Union’s first short‑range, twin‑engine jet airliner and a direct descendant of the larger Tu‑104. Developed by the Tupolezdesign bureau to meet the growing demand for efficient regional transport, the Tu‑124 made its maiden flight on 29 March 1960 and entered commercial service with Aeroflot the following year. It could accommodate 56 passengers in a narrow‑body cabin and was powered by two Soloviev D‑20 turbofan engines mounted on the rear fuselage, a layout that reduced wing drag and simplified maintenance. The aircraft featured a tricycle landing gear, pressurised cabin, and an advanced (for its era) autopilot system, enabling reliable operation on routes up to 2,500 km. Its relatively low operating costs and short‑haul capability made the Tu‑124 popular on domestic Soviet routes and in allied states, where it served as a workhorse for both passenger and cargo flights. Although production ceased in 1965 after just 164 units, the Tu‑124’s design influenced subsequent Soviet jets, demonstrating the viability of twin‑engine, short‑range jetliners and playing a pivotal role in modernising mid‑20th‑century Soviet civil aviation.

Performance

Service Ceiling
11700 metre

Production & History

Units Produced
165
First Flight
1960
Service Entry
1962

Design & Classification

Country of Origin
Manufacturer
Tupolev
Developer
Tupolev
NATO Name
Cookpot
Engine
Soloviev D-20
Operator
Main directorate of civil air fleet of the Soviet Union Ministry of Civil Aviation of the USSR Iraqi Airways Air Force of the National People's Army Indian Air Force Czech Airlines Aeroflot
Wikidata ID
Q160469