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The Antonov An-124 Condor is a strategic airlift jet aircraft. It was designed by the Antonov design bureau in the Ukrainian SSR, then part of the Soviet Union.
The An-124 is the world's highest gross weight production cargo aeroplane and second heaviest operating cargo aircraft, behind the one-off Antonov An-225 (a greatly enlarged design based on the An-124).
During development it was known as Izdeliye 400 (Product #400) in house, and An-40 in the West. First flown in 1982, civil certification was issued on 30 December 1992. In July 2013, 26 An-124's were in commercial service with 10 on order.
General characteristics
Crew: 4–6 (pilot, copilot, navigator, senior flight engineer (+flight engineer, radio man) + 2 loadmasters) Capacity: 88 passengers or the hold can take an additional 350 on a palletised seating system Payload: 150,000 kg (330,000 lb) Length: 68.96 m (226 ft 3 in) Wingspan: 73.3 m (240 ft 5 in) Height: 20.78 m (68 ft 2 in) Wing area: 628 m² (6,760 sq ft) Empty weight: 175,000 kg (385,000 lb) Loaded weight: 405,000 kg (893,000 lb) Useful load: 230,000 kg (508,000 lb) Max. takeoff weight: 405,000 kg (893,000 lb)
Maximum speed: 865 km/h (467 kn (537 mph)) Cruise speed: 800–850 km/h (430 kn (490 mph)) Range: 5,200 km (2,808 nm, 3231 mi) Service ceiling: 12,000 m (39,370 ft) Wing loading: 365 kg/m² (74.7 lb/sq ft) Thrust/weight: 0.23 Take-off run distance (maximum take-off weight): 2,520 m (8,270 ft) Landing roll distance at maximum landing weight: 900 m (3,000 ft)
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Antonov An-26 "Condor" Flight Deck - Desktop Nexus AircraftDownload free wallpapers and background images: Antonov An-26 "Condor" Flight Deck. Desktop Nexus Aircraft background ID 1877885. The Antonov An-124 Condor is a strategic airlift jet aircraft. It was designed by the Antonov design bureau in the Ukrainian SSR, then part of the Soviet Union.
The An-124 is the world's highest gross weight production cargo aeroplane and second heaviest operating cargo aircraft, behind the one-off Antonov An-225 (a greatly enlarged design based on the An-124).
During development it was known as Izdeliye 400 (Product #400) in house, and An-40 in the West. First flown in 1982, civil certification was issued on 30 December 1992. In July 2013, 26 An-124's were in commercial service with 10 on order.
General characteristics
Crew: 4–6 (pilot, copilot, navigator, senior flight engineer (+flight engineer, radio man) + 2 loadmasters) Capacity: 88 passengers or the hold can take an additional 350 on a palletised seating system Payload: 150,000 kg (330,000 lb) Length: 68.96 m (226 ft 3 in) Wingspan: 73.3 m (240 ft 5 in) Height: 20.78 m (68 ft 2 in) Wing area: 628 m² (6,760 sq ft) Empty weight: 175,000 kg (385,000 lb) Loaded weight: 405,000 kg (893,000 lb) Useful load: 230,000 kg (508,000 lb) Max. takeoff weight: 405,000 kg (893,000 lb)
Maximum speed: 865 km/h (467 kn (537 mph)) Cruise speed: 800–850 km/h (430 kn (490 mph)) Range: 5,200 km (2,808 nm, 3231 mi) Service ceiling: 12,000 m (39,370 ft) Wing loading: 365 kg/m² (74.7 lb/sq ft) Thrust/weight: 0.23 Take-off run distance (maximum take-off weight): 2,520 m (8,270 ft) Landing roll distance at maximum landing weight: 900 m (3,000 ft)
Rating: 4
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Wallpaper Statistics
Total Downloads: 260
Times Favorited: 2
Uploaded By: woody2858
Date Uploaded: November 09, 2014
Filename: v-An-26-Flight-Deck.jpg
Original Resolution: 1280x845
File Size: 937.92KB
Category: Military