Tupolev Tu-134A
Explore the Tupolev Tu-134A in side view and top view to compare its silhouette and proportions.
37.1 m121.7 ft
29.01 m95.2 ft
From Wikipedia
The Tupolev Tu-134 is a twin-engined, narrow-body jet airliner built in the Soviet Union for short and medium-haul routes from 1966 to 1989. The original version featured a glazed-nose design and, like certain other Russian airliners, it can operate from unpaved airfields.
Summary of “Tupolev Tu-134” from Wikipedia, the free encyclopedia, used under CC BY-SA 4.0. Retrieved 2026-10-11.
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Drawing of the Tupolev Tu-134A by AirwayControl Aircraft Library (https://aircraft.intelsystems.ai/aircraft/T134/), CC BY 4.0Specifications
- Length
- 37.1 m121.7 ft
- Wingspan
- 29.01 m95.2 ft
- Max take-off weight
- 47.6 t104,900 lb
- Cruise speed
- 850 km/h528 mph
- Max speed
- 950 km/h590 mph
- Range
- 3,000 km1,864 mi
- Ceiling
- 12,100 m39,700 ft
- Engines
- 2 × Soloviev D-30-II turbofan engines
- Power
- 66.68 kN (14,990 lbf) thrust each
- First flight
- 1963
- In service
- 1967
From the AirwayControl spec register, curated from Wikipedia and manufacturer pages. Figures vary by variant.
