An-26

· Antonov
Airplanes
Length
23.8 m
Flat Wing Span
29.3 m
Height
8.58 m
Flat Wing Area
74.98 m²
Flat Wing Aspect Ratio
11.7
Max Seating
40
Cruise Speed
440 km/h
Max Ceiling
7500 m
Number of Engines
2
First Flight
1969-05-21
Entry Into service
1972-01-01
Number Built
1403
Maximum Take-Off Weight
24 t (paragliders: kg)
Maximum Range
2500 km

Pictures

No pictures yet for this family.

Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Maximum Range (km)
An-26 24 2500

Similar airplanes

Name Length (m) Flat Wing Span (m) Max Seating
Hawker Siddeley Andover 23.7744 29.8704 52 Compare
Antonov An-30 24.26 29.2 Compare
De Havilland Canada DHC-5 Buffalo 24.0792 29.2608 41 Compare
Xi'an Y-7 24.218 29.666 52 Compare
Antonov An-32 23.78 29.2 42 Compare
Xi'an MA60 24.71 29.2 62 Compare
All data (26 fields)
Name
An-26
Manufacturer
Antonov
Description
AI-24VT
ICAO Code
AN26
EASA TCDSN
EASA.IM.A.351
First Flight
1969-05-21
Entry Into service
1972-01-01
Type
Transport aircraft / regional airliner
Length (m)
23.8
Height (m)
8.58
Max Seating
40
Cruise Speed (km/h)
440
Max Ceiling (m)
7500
Rate of Climb (m/s)
8
Capacity Description
40 passengers / 5500 kg
National Origin
Soviet Union
Number Built
1403
Powerplant Description
2 × Progress AI-24VT Turboprop engines, 2103 kW (2820 hp) each
Primary Users
Soviet Air Forces (former), Russian Aerospace Forces , Ukrainian Air Force , People's Liberation Army Air Force
Status
In service
Wikipedia Article (URL)
en.wikipedia.org/wiki/Antonov_An-26
Flat Wing Span (m)
29.3
Flat Wing Area (m²)
74.98
Flat Wing Aspect Ratio
11.7
Wake Category
M
Number of Engines
2