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An-32 Cline vs C-295 Persuader

An-32 Cline vs C-295 Persuader at a glance — top speed 530 vs 576 km/h, range 1,400 vs 5,750 km, max takeoff weight 28,500 vs 23,200 kg, built 373 vs 209 units.

Specifications
An-32 Cline C-295 Persuader
Origin country 🇺🇦 Ukraine 🇪🇸 Spain
Category Military Transport Aircraft Military Transport Aircraft
Manufacturer Antonov Airbus
First flight 9 July 1976 28 November 1997
Year introduced 1982 2001
Number produced 373 units 209 units
Average unit price $15 million $78 million
Wing area -- m² 59.0 m²
Wingspan 29.2 m 25.8 m
Height 8.8 m 8.6 m
Length 24.5 m 24.5 m
Maximum speed 530 km/h 576 km/h
Operational range 1,400 km 5,750 km
Service ceiling 9,000 m 7,620 m
Max. takeoff weight 28,500 kg 23,200 kg
Empty weight 16,800 kg 9,250 kg
Total thrust 2 x 3,812 kW 2 x 1,972 kW
Performance Radar Chart

Detailed Comparison

The Antonov An-32 and Airbus C-295 occupy the same tactical medium-transport weight class but serve entirely opposing procurement requirements. The An-32 is a brute-force modification of the An-26 airframe, engineering raw power to overcome austere, high-altitude environments. The C-295 relies on aerodynamic efficiency, extended range, and modular avionics to secure export markets demanding multi-mission adaptability over sheer short-field payload limits.

Development and Design

Antonov developed the An-32 by mating 5,100 hp Ivchenko AI-20 turboprops to the An-26. Placing these oversized engines 1.5 meters above the wing generated clearance for larger propellers and mitigated foreign object damage on unpaved strips. This resulted in a hot-and-high transport tailor-made for its primary backer, the Indian Air Force. Airbus derived the C-295 from the CASA/IPTN CN-235, stretching the fuselage to increase payload capacity by 50% while transitioning to Pratt & Whitney PW127G engines. Where the An-32 relies on mechanical simplicity and high thrust, the C-295 prioritizes systems integration, utilizing the Thales Topdeck digital suite and modular hardpoints to allow configurations ranging from troop transport to anti-submarine warfare (MPA/Persuader) and airborne early warning (AEW&C).

Specifications and Performances

The performance delta between the two airframes dictates their tactical application.

  • The An-32 utilizes a massive thrust surplus to lift its 28,500 kg maximum takeoff weight (MTOW), yielding a 6,700 kg payload limit.
  • The C-295 achieves a higher 7,100 kg payload class (at a 23,200 kg MTOW) using nearly half the engine output (1,972 kW per engine).

This efficiency disparity translates directly to endurance. The C-295 executes theater-level logistics with a 5,750 km range, whereas the An-32 is restricted to localized hubs by its 1,400 km radius. However, the An-32's power reserve grants it a 9,000 m service ceiling—1,380 m higher than the C-295—enabling operations over mountain ranges that structurally limit the Airbus platform.

Deployment and usage

India remains the primary arbiter of the An-32's operational record, utilizing over 100 airframes to sustain outposts in the Himalayas where low air density grounds competing transports. The C-295 dominates the contemporary export market, securing fleets in Egypt (21 aircraft), Poland, and Canada. While it lost the US Joint Cargo Aircraft bid to the C-27J Spartan due to the latter's wider cabin and floor strength, the C-295 capitalized on lower operating costs globally. Combat feedback from Polish and Egyptian operators indicates high dispatch reliability for standard logistics, though the Canadian CC-295 Kingfisher variant suffered multi-year procurement delays due to software and equipment integration failures.

Conclusion

The C-295 defeats the An-32 in any modern, integrated air force requiring range, sensor networking, or multi-role tasking. Its ability to pivot from dropping paratroopers to deploying anti-tank missiles or conducting maritime patrol justifies its $78.0 million unit cost for mature militaries. Conversely, for specialized Himalayan operations or underdeveloped airstrips where raw thrust and mechanical resilience supersede loiter time, the An-32 is the only viable platform. Militaries prioritizing cost-effective endurance should acquire the C-295; those tasked with lifting heavy equipment off unpaved, high-altitude runways require the An-32.

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Frequently Asked Questions

Which is faster, the An-32 Cline or C-295 Persuader?
The C-295 Persuader is faster with a maximum speed of 576 km/h compared to the An-32 Cline's 530 km/h, a difference of 46 km/h.
Which has longer range, the An-32 Cline or C-295 Persuader?
The C-295 Persuader has a longer range at 5,750 km compared to the An-32 Cline's 1,400 km.
Which can fly higher, the An-32 Cline or C-295 Persuader?
The An-32 Cline has a higher service ceiling at 9,000 meters (29,527 ft) compared to the C-295 Persuader's 7,620 meters (25,000 ft).
Which is heavier, the An-32 Cline or C-295 Persuader?
The An-32 Cline has a higher maximum takeoff weight at 28,500 kg compared to the C-295 Persuader's 23,200 kg.
Which is larger, the An-32 Cline or C-295 Persuader?
Both the An-32 Cline and C-295 Persuader are 24.5 meters long.
Which is more expensive, the An-32 Cline or C-295 Persuader?
The C-295 Persuader is more expensive at approximately $78 million per unit compared to the An-32 Cline at $15 million.
Which entered service first, the An-32 Cline or C-295 Persuader?
The An-32 Cline entered service first in 1982, 19 years before the C-295 Persuader which entered service in 2001.
Which has been built in greater numbers, the An-32 Cline or C-295 Persuader?
The An-32 Cline has been produced in greater numbers with 373 units compared to 209 units of the C-295 Persuader.