


| Name / Designation | Sikorsky S-92A |
| Type / Role | Heavy Utility / Transport / Search & Rescue |
| Country of Origin | United States |
| Manufacturer | Sikorsky Aircraft (Lockheed Martin) |
| Introduced / Service Entry | 2004 |
| Operational Status | Active |
| Operators | Commercial Operators, Coast Guards, Global Heads of State |
| Maximum Speed (Road) | 306 km/h (165 knots) |
| Cruise Speed | 280 km/h (151 knots) |
| Range | 999 km (539 nautical miles) |
| Endurance | Up to 4.5 hours (standard internal fuel) |
| Service Ceiling | 4,270 m (14,000 feet) |
| Rate of Climb | 8.1 m/s (1,600 fpm) |
| Length | 17.10 m (56 ft 2 in) airframe / 20.88 m (68 ft 6 in) overall |
| Height | 4.71 m (15 ft 5 in) airframe / 5.46 m (17 ft 11 in) overall |
| Rotor Diameter | 17.17 m (56 ft 4 in) |
| Empty Weight | 7,030 kg (15,500 lbs) |
| Maximum Takeoff Weight (MTOW) | 12,020 kg (26,500 lbs) |
| Primary Armament | None (Civilian/Utility Standard) |
| Secondary Armament | None |
| Hardpoints / Weapon Stations | None |
| Payload Capacity | 4,422 kg (9,749 lbs useful load) |
| Countermeasures | Optional military grade modifications available for state variants |
| Radar Name | Weather Radar / Optional Search Radar for SAR configurations |
| Targeting System | Optional Forward Looking Infrared (FLIR) for SAR |
| Navigation System | Dual GPS / INS / Flight Management System |
| Communication System | VHF/UHF Secure Radios, Satellite Communication Links |
| Defensive Systems | Health and Usage Monitoring System (HUMS) |
| Engines | 2 ร Turboshaft Engines |
| Engine Model | General Electric CT7-8A |
| Power Output | 2,520 shp each |
| Fuel Capacity | 2,877 L (760 gal) standard sponson tanks |
| Crew | 2 (Pilot + Co-Pilot) |
| Passenger Capacity | Up to 19 passengers |
| Cabin Configuration | Passenger Transport / Medical Evacuation / VIP |
| Cargo Load (Internal/External) | Passenger Transport / Medical Evacuation / VIP |
| Mission Types | Offshore Oil Support, Search & Rescue, Executive Transport |
| Night Operation Capability | Yes |
| All-weather Operation | Yes |
| Combat Proven | No (Utilized in non-combat secondary military/state configurations) |
The Sikorsky S-92A stands as a premier heavy-lift twin-engine helicopter globally recognized for its exceptional safety profile, large passenger capacity, and rugged dependability. Designed initially to meet stringent Federal Aviation Administration (FAA) and European Aviation Safety Agency (EASA) safety regulations, it has become the default workhorse for offshore oil and gas industry crew changes, search and rescue (SAR) operations, and head-of-state transport roles. Equipped with a fully composite four-blade main rotor system and an advanced health and usage monitoring system (HUMS), the aircraft delivers smooth flight dynamics and high readiness levels under challenging conditions.
The S-92A is designed and manufactured by Sikorsky Aircraft, a subsidiary of the American defense giant Lockheed Martin. Built with a rich pedigree of military engineering derived from the H-60 Black Hawk series, this civilian and utility variant combines commercial efficiency with structural military durability. Production primarily takes place at facilities within the United States.
Powered by dual General Electric turboshaft engines, the S-92A can achieve a maximum cruise speed of 151 knots (approximately 280 km/h). The aircraft boasts an impressive standard operational range of 539 nautical miles (999 km), which can be further augmented via auxiliary internal fuel tanks mounted in the cabin or rear ramp areas, making it ideal for long-range oceanic transits and deep-water search operations.
A factory-new Sikorsky S-92A has an approximate baseline list price of $27 million, though this total fluctuates depending on custom interior configurations, specialized avionics suites, or SAR mission gear. On the pre-owned market, average acquisition costs range from $10 million to $15 million based on operational airframe hours and maintenance cycles.
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