Antonov An-10

· Antonov

Airplanes

Length

34 m

Flat Wing Span

38 m

Height

9.83 m

Flat Wing Area

120 m²

Max Seating

100

Cruise Speed

680 km/h

Max Speed

715 km/h

Max Ceiling

10200 m

Number of Engines

First Flight

1957-03-07

Entry Into service

1959-01-01

Number Built

104

Maximum Take-Off Weight

55.1 t (paragliders: kg)

Total Fuel Capacity

13000

Maximum Range

1200 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Antonov An-10	55.1	13000	1200

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Lockheed L-1049 Super Constellation		34.4424	37.4904	106	Compare
Shaanxi Y-8		34.02	38	90	Compare
Antonov An-12		33.1	38	60	Compare
Lockheed Constellation		35.3568	38.4048	95	Compare
Douglas DC-7	Wright R-3350 Duplex-Cyclone	34.1376	38.7096	105	Compare
Lockheed L-1249 Super Constellation		35.3568	35.6616	106	Compare

All data (24 fields)

Name: Antonov An-10
Manufacturer: Antonov
Description: The Antonov An-10 Ukraina (; NATO reporting name: Cat) is a four-engined turboprop passenger transport aircraft designed in the Soviet Union.
First Flight: 1957-03-07
Entry Into service: 1959-01-01
Service End: 1974-01-01
Designer: N. S. Trunchenkov & V. N. Ghel'prin
Type: Airliner
Length (m): 34
Height (m): 9.83
Cockpit Crew: 4
Max Seating: 100
Max Speed (km/h): 715
Cruise Speed (km/h): 680
Max Ceiling (m): 10200
Capacity Description: 100 or 130 pax / 14500 kg
Number Built: 104
Powerplant Description: 4 × Ivchenko AI-20K turboprop engines, 2983 kW (4000 hp) each
Primary Users: Aeroflot
Status: Retired
Wikipedia Article (URL): en.wikipedia.org/wiki/Antonov_An-10
Flat Wing Span (m): 38
Flat Wing Area (m²): 120
Number of Engines: 4