GlobalMilitary.net Open-source military intelligence Updated daily

AW101 vs S-92 Superhawk

AW101 vs S-92 Superhawk at a glance — top speed 309 vs 306 km/h, range 1,389 vs 850 km, built 137 vs 300 units.

AgustaWestland AW101 military helicopters side profile drawing
🇬🇧🇮🇹 AW101
Sikorsky S-92 Superhawk military helicopters side profile drawing
Specifications
AW101 S-92 Superhawk
Origin country 🇬🇧 United Kingdom🇮🇹 Italy 🇺🇸 United States
Category Military Helicopters Military Helicopters
Manufacturer AgustaWestland Sikorsky
First flight 19 October 1964 23 December 1998
Year introduced 1999 2004
Number produced 137 units 300 units
Average unit price $70 million $32 million
Wingspan 18.6 m 17.2 m
Height 6.6 m -- m
Length 20.4 m -- m
Maximum speed 309 km/h 306 km/h
Operational range 1,389 km 850 km
Service ceiling 2,600 m 4,267 m
Max. takeoff weight 12,900 kg -- kg
Empty weight 6,850 kg 7,031 kg
Total thrust 3 x 1,044 kW --
Performance Radar Chart

Detailed Comparison

The AgustaWestland (now Leonardo) AW101 and the Sikorsky S-92 represent the divergence between clean-sheet military procurement and the commercial-off-the-shelf (COTS) militarization trend. While the AW101 emerged from a specific Cold War requirement to hunt Soviet submarines, the S-92 began as a bus for the offshore energy sector, attempting to wear a uniform later in its life cycle.

Development and Design

The AW101 is defined by its three-engine configuration, a requirement driven by the Royal Navy and Italian Navy for safe loitering during sonar dipping operations. This architecture provides a One Engine Inoperative (OEI) safety margin that twin-engine helicopters cannot match. Its design integrates active vibration control and armored crew seats from the outset, reflecting a philosophy prioritizing survivability and sensor stability over economy.

Conversely, the S-92 utilizes dynamic components from the S-70/Black Hawk lineage but pairs them with a high-volume, commercial airframe. Sikorsky's approach focused on economics and cabin volume for the oil and gas market. The difficulties in militarizing this platform are best illustrated by Canada’s CH-148 Cyclone program, where transforming the S-92 into a naval asset resulted in over a decade of delays and massive cost overruns. The S-92 lacks the AW101's bespoke military DNA, relying instead on retrofitting mission systems into a civilian shell.

Specifications and Performance

Performance metrics favor the European platform for blue-water and heavy-lift operations. The AW101’s range of nearly 1,400 km dwarfs the S-92’s 850 km, a direct result of the triple-turbine architecture and larger fuel fraction. This range advantage allows the AW101 to conduct long-range SAR or ASW screens without the immediate refueling tether required by the S-92.

While the S-92 is theoretically cheaper at $32 million compared to the AW101's $70 million, this delta evaporates when the S-92 is militarized (the VH-92 and CH-148 are significantly more expensive than the base airframe). The AW101 offers a higher Maximum Takeoff Weight (14,600 kg on newer variants vs roughly 12,000 kg for S-92), translating to superior payload capacity for torpedoes, anti-ship missiles, or troop contingents.

Deployment and Usage

The AW101 possesses a combat record the S-92 cannot claim. RAF Merlin HC3s saw heavy utilization in Iraq (Operation Telic) and Afghanistan (Operation Herrick). These aircraft were often outfitted with heavy armor and defensive aid suites, earning a reputation for taking punishment and bringing crews home. The platform functions effectively as both a tactical transport and a high-end ASW hunter.

The S-92’s military service is largely limited to VIP transport (the US Marine Corps VH-92 "Marine One") and the troubled Canadian maritime patrol role. It has found success in civilian and para-public SAR (UK Coastguard, Irish Coast Guard), replacing aging Sea Kings and S-61s. However, the operational history is marred by the 2009 Cougar Helicopters crash off Newfoundland, which exposed vulnerabilities in the main gearbox mounting studs—a catastrophic failure mode for a helicopter marketed on safety.

Conclusion

For naval commanders and combat operators, the AW101 is the superior machine. Its three-engine redundancy, range, and purpose-built fuselage justify its high acquisition cost and maintenance demands. It is a warfighter's airframe. The S-92 remains a commercial design forced into a military role; while competent for VIP lift or benign environment SAR, it lacks the kinetic resilience and raw performance required for high-intensity conflict.

Change comparison vs

Frequently Asked Questions

Which is faster, the AW101 or S-92 Superhawk?
The AW101 is faster with a maximum speed of 309 km/h compared to the S-92 Superhawk's 306 km/h, a difference of 3 km/h.
Which has longer range, the AW101 or S-92 Superhawk?
The AW101 has a longer range at 1,389 km compared to the S-92 Superhawk's 850 km.
Which can fly higher, the AW101 or S-92 Superhawk?
The S-92 Superhawk has a higher service ceiling at 4,267 meters (13,999 ft) compared to the AW101's 2,600 meters (8,530 ft).
Which is heavier, the AW101 or S-92 Superhawk?
The AW101 has a higher maximum takeoff weight at 12,900 kg compared to the S-92 Superhawk's 0 kg.
Which is larger, the AW101 or S-92 Superhawk?
The AW101 is longer at 20.4 meters compared to the S-92 Superhawk's 0.0 meters.
Which is more expensive, the AW101 or S-92 Superhawk?
The AW101 is more expensive at approximately $70 million per unit compared to the S-92 Superhawk at $32 million.
Which entered service first, the AW101 or S-92 Superhawk?
The AW101 entered service first in 1999, 5 years before the S-92 Superhawk which entered service in 2004.
Which has been built in greater numbers, the AW101 or S-92 Superhawk?
The S-92 Superhawk has been produced in greater numbers with 300 units compared to 137 units of the AW101.