TUPOLEV TU-124 Civil Aircraft Model Details

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General Information of TUPOLEV TU-124

Developed From : Tupolev Tu-104

First Flight : 22004

Introduction : 22921

Manufacturer : Tupolev OKB

Number Built : 164

Primary Users : Aeroflot; CSA

Produced : 1960-1965

Retired : 1980 (civil aviation), 1992 (military service)

Role : Short-range airliner

Status : Retired

Variants : Tupolev Tu-134

General characteristics of TUPOLEV TU-124

Capacity : 56 passengers

Crew : three

Empty Weight : 22,900 kg (50,486 lb)

Height : 8.08 m (26 ft 6 in)

Length : 30.58 m (100 ft 4 in)

Max Takeoff Weight : 37,500 kg (82,673 lb)

Powerplant : 2 × Soloviev D-20P turbofans, 53.1 kN (11,905 lbf) each

Wing Area : 119.4 m² (1,284 ft²)

Wingspan : 25.55 m (83 ft 10 in)

Performance of TUPOLEV TU-124

Cruise Speed : 800–870km/h (432–469 knots, 497–540mph)

Maximum Speed : 970km/h (523 knots, 602mph) at 8,000m (26,000ft)

Range : 2,100km (1,133nmi, 1,304mi) (maximum fuel, 3,000kg (6,600lb) payload)

Rate Of Climb : 12.0m/s[13](2,360ft/min)

Service Ceiling : 11,700m (38,385ft)

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