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An-22 Cock vs Il-76 Candid

An-22 Cock vs Il-76 Candid at a glance — top speed 740 vs 850 km/h, range 10,950 vs 5,000 km, max takeoff weight 250,000 vs 195,000 kg, built 68 vs 960 units.

Antonov An-22 Cock military transport aircraft side profile drawing
🇺🇦 An-22 Cock
Ilyushin Il-76 Candid military transport aircraft side profile drawing
🇷🇺 Il-76 Candid
Specifications
An-22 Cock Il-76 Candid
Origin country 🇺🇦 Ukraine 🇷🇺 Ex-USSR
Category Military Transport Aircraft Military Transport Aircraft
Manufacturer Antonov Ilyushin
First flight 27 February 1965 25 March 1971
Year introduced 1967 1974
Number produced 68 units 960 units
Average unit price -- --
Wing area 345.0 m² 300.0 m²
Wingspan 64.4 m 50.5 m
Height 12.5 m 14.8 m
Length 57.9 m 46.6 m
Maximum speed 740 km/h 850 km/h
Operational range 10,950 km 5,000 km
Service ceiling 8,000 m 13,000 m
Max. takeoff weight 250,000 kg 195,000 kg
Empty weight 114,000 kg 92,500 kg
Total thrust 4 x 11,186 kW 4 x 14,500 kgf
Performance Radar Chart

Detailed Comparison

The Antonov An-22 Antaeus served as the Soviet Union's first true strategic heavy lifter, bridging the capability gap between tactical turboprops and the jet age, while the Ilyushin Il-76 Candid effectively democratized strategic mobility for the Eastern Bloc. While the An-22 maximized payload through sheer scale and turboprop torque, the Il-76 prioritized cycle times, versatility, and jet-powered rapid reaction, eventually displacing the An-22 in all but the most specialized heavy-lift roles.

Development and Design

Antonov's design philosophy for the An-22 was evolutionary scaling. By enlarging the An-12 concept and utilizing four Kuznetsov NK-12MA contra-rotating turboprops—derived from the Tu-95 bomber—Antonov created a wide-body airframe capable of austere field operations without waiting for high-bypass turbofan technology. Its 639 cubic meter pressurized cargo hold was specifically dimensioned to accommodate surface-to-air missile systems and armor that smaller transports could not fit.

Conversely, the Il-76 represented a shift toward high-speed operational mobility. Ilyushin adopted a configuration similar to the US C-141 Starlifter—swept wings and T-tail—but retained the Soviet requirement for unpaved strip capability. The inclusion of a glass nose for navigation and rear turret (on military variants) highlighted its dual nature as a frontline tactical transport and a strategic lifter. The shift to Soloviev D-30KP turbofans sacrificed some fuel efficiency compared to props but integrated the Soviet Airborne Forces (VDV) into the jet age.

Specifications and Performances

The An-22 dominates in raw lifting capacity, with a maximum payload of 80,000 kg, significantly outclassing the standard Il-76’s approximate 40,000–50,000 kg limit (depending on the variant). This allows the An-22 to transport up to four BMD-1s or heavy construction equipment that simply physically fits better in its wider fuselage.

However, the Il-76 holds the operational advantage in speed and ceiling. With a cruise speed of 850 km/h versus the An-22's 740 km/h, the Il-76 generates faster sortie rates during intensive airlifts. While the An-22 boasts a range of 10,950 km, the complex maintenance required for the NK-12 gearboxes and contra-rotating propellers reduces its availability compared to the more robust turbofans of the Il-76. Both aircraft feature rugged landing gear with low ground pressure, but the An-22’s ability to adjust tire pressure in flight gave it an edge on the softest surfaces during the 1970s.

Deployment and Usage

The An-22 was critical during the 1973 Yom Kippur War, airlifting heavy air defense systems to Egypt and Syria that smaller aircraft could not carry. It was also instrumental in the initial 1979 invasion of Afghanistan, delivering the heavy armor required to secure airfields. However, its acoustic signature and vulnerability to MANPADS limited its frontline utility in later years.

The Il-76 became the logistical workhorse of the Soviet-Afghan War, performing the bulk of resupply and troop rotation missions. Its combat resilience and faster climb rates made it preferable for operations in contested airspace. Unlike the An-22, the Il-76 airframe proved adaptable enough for conversion into the A-50 Mainstay (AEW&C) and Il-78 Midas (tanker), cementing its place in modern Russian doctrine.

Conclusion

The Ilyushin Il-76 is the superior asset for 90% of military logistics requirements. Its higher speed, lower maintenance burden, and adaptability allow it to sustain high-tempo operations that the An-22 cannot match. The An-22 remains a niche capability; it excels only when the payload exceeds 50 tons or involves outsized dimensions that preclude the Candid. While the An-22 proved the concept of Soviet strategic airlift, the Il-76 perfected its execution.

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Frequently Asked Questions

Which is faster, the An-22 Cock or Il-76 Candid?
The Il-76 Candid is faster with a maximum speed of 850 km/h compared to the An-22 Cock's 740 km/h, a difference of 110 km/h.
Which has longer range, the An-22 Cock or Il-76 Candid?
The An-22 Cock has a longer range at 10,950 km compared to the Il-76 Candid's 5,000 km.
Which can fly higher, the An-22 Cock or Il-76 Candid?
The Il-76 Candid has a higher service ceiling at 13,000 meters (42,650 ft) compared to the An-22 Cock's 8,000 meters (26,246 ft).
Which is heavier, the An-22 Cock or Il-76 Candid?
The An-22 Cock has a higher maximum takeoff weight at 250,000 kg compared to the Il-76 Candid's 195,000 kg.
Which is larger, the An-22 Cock or Il-76 Candid?
The An-22 Cock is longer at 57.9 meters compared to the Il-76 Candid's 46.6 meters.
Which entered service first, the An-22 Cock or Il-76 Candid?
The An-22 Cock entered service first in 1967, 7 years before the Il-76 Candid which entered service in 1974.
Which has been built in greater numbers, the An-22 Cock or Il-76 Candid?
The Il-76 Candid has been produced in greater numbers with 960 units compared to 68 units of the An-22 Cock.