Time Period: Post-WW2
Country of Origin: Russia / USSR
Type: Transporter Aircraft
Manufacturer: Antonov
Antonov An-24 Aircraft Overview
The Antonov An-24 is a twin-turboprop transport aircraft designed by the Soviet Antonov Design Bureau in the late 1950s. It was created primarily for regional passenger and cargo transport across the vast and often rugged terrain of the Soviet Union. What makes the An-24 particularly notable is its ruggedness and versatility—traits that made it well-suited for short, unpaved runways and remote airfields where other aircraft might struggle.
Powered by two Ivchenko AI-24 engines, the An-24 was engineered to operate efficiently even in challenging weather and environmental conditions. Its high-mounted wings and sturdy landing gear allow it to handle rough airstrips, which contributed to its popularity in regions with limited infrastructure, like Siberia or parts of Africa and Asia. Inside, the aircraft was relatively simple and utilitarian, reflecting the Soviet philosophy of durable, no-frills aviation design.
First flown in 1959 and entering service in the early 1960s, the An-24 saw wide usage with Aeroflot and many Eastern Bloc countries. Over time, it was adapted into various roles, including military transport, aerial reconnaissance, and even maritime patrol. Several variants were developed, including the An-26 and An-30, which took the base design in new directions with added features like cargo ramps or photographic equipment.
Despite its age, many An-24s are still flying today, a testament to their solid construction and adaptability. They’ve gained a bit of a reputation for being noisy and somewhat spartan by modern standards, but among pilots and operators, the An-24 is often respected as a dependable workhorse.
Antonov An-24 Specifications
- Crew: 3
- Passenger capacity: Up to 50
- Overall length: 23.53 meters (77 feet 2 inches)
- Wingspan: 29.20 meters (95 feet 10 inches)
- Height: 8.32 meters (27 feet 4 inches)
- Wing surface area: 74.98 square meters (807.1 square feet)
- Wing aspect ratio: 11.7:1
- Empty weight: 13,300 kilograms (29,321 pounds)
- Maximum takeoff weight: 21,000 kilograms (46,297 pounds)
- Fuel storage capacity: 5,550 liters (1,470 US gallons; 1,220 imperial gallons)
- Engines: 2 × Ivchenko AI-24A turboprop engines, each delivering 1,900 kW (2,550 shp)
- Propellers: 4-blade AV-72 constant-speed units, 3.90 meters (12 feet 10 inches) in diameter
Antonov An-24 Performance
- Top speed: 485 km/h (301 mph, 262 knots) at 6,000 meters (20,000 feet)
- Cruising speed: 450 km/h (280 mph, 240 knots) at 6,000 meters (20,000 feet)
- Flight range: 2,400 km (1,500 miles, 1,300 nautical miles) with full fuel; 550 km (340 miles, 300 nautical miles) at full payload
- Maximum operating altitude: 8,400 meters (27,600 feet)
- Climb time:
– 17.5 minutes to reach 6,000 meters (20,000 feet)
– 45.2 minutes to reach 8,100 meters (26,600 feet)