.jpg "An-26 P (An-24). First flight: 1987 © Konstantinos Panitsidis")
Photo from the personal collection of Kostas Panitsidis
Technical specifications 
Photos 
Video
TECHNICAL SPECIFICATIONS
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DESIGNER
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OKB Antonov
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|---|---|
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COUNTRY
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Russia/ Ukraine
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TYPE
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Firefighting
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CREW
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3
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POWER-PLANT
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Two turboprop engine ΑΙ-24VT
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Power, h.p
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2 x 2.820
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Booster engine-1 jet engine (backup system) Tumansky, RU-19A-300, Thrust, kN
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7,85
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DIMENSIONS
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|
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Length, m
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23,80
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Height, m
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8,58
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Wing span, m
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29,20
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Wing area m2
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74,98
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WEIGHT
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|
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Maximum take-off, kg
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23.800
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Normal take-off, kg
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-
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Empty aircraft, kg
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15.020
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Internal fuel, kg
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2.760
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PERFORMANCE
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|
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Maximum speed, km/h
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-
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Cruising speed, km/h
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400
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Service ceiling, m
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7.500
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Range, km
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-
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Combat range, km
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430
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Payload, kg
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30 passengers with 1.000 kg firefighting equipment or 4.000 ltr water.
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|
ARMAMENT
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-
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