Tupolev Tu-124

· Tupolev

Airplanes

Length

30.58 m

Flat Wing Span

25.55 m

Height

8.08 m

Flat Wing Area

119.48 m²

Max Seating

Cruise Speed

800 km/h

Max Speed

970 km/h

Max Ceiling

11700 m

Number of Engines

First Flight

1960-03-29

Entry Into service

1962-10-02

Number Built

164

Maximum Take-Off Weight

37.5 t (paragliders: kg)

Maximum Range

2100 km

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Tupolev Tu-124	37.5	2100

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Fokker 70	Rolls-Royce RB.183 Tay	30.91	28.08		Compare
McDonnell Douglas DC-9		31.6992	27.1272	90	Compare
Beriev Be-12		30.11	29.84		Compare
Bombardier CRJ700 series	General Electric CF34	36.2	24.9	90	Compare
Gulfstream V	Rolls-Royce BR700	29.3827	28.4836		Compare
Gulfstream G550	Rolls-Royce BR700	29.2608	28.3464	19	Compare

All data (26 fields)

Name: Tupolev Tu-124
Manufacturer: Tupolev
Description: The Tupolev Tu-124 (NATO reporting name: Cookpot) is a 56-passenger short-range twin-jet airliner built in the Soviet Union.
First Flight: 1960-03-29
Entry Into service: 1962-10-02
Production End: 1965-01-01
Service End: 1980-01-01
Designer: Tupolev
Type: Short-range jetliner
Length (m): 30.58
Height (m): 8.08
Cockpit Crew: 3
Max Seating: 56
Max Speed (km/h): 970
Cruise Speed (km/h): 800
Max Ceiling (m): 11700
Rate of Climb (m/s): 12
Capacity Description: 56 passengers
Number Built: 164
Powerplant Description: 2 × Soloviev D-20P turbofan engines, 53.1 kN thrust each
Primary Users: Aeroflot, ČSA , Interflug , Iraqi Airways
Status: Retired
Wikipedia Article (URL): en.wikipedia.org/wiki/Tupolev_Tu-124
Flat Wing Span (m): 25.55
Flat Wing Area (m²): 119.48
Number of Engines: 2