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S-92

S-92

Civil Helicopters
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Basic Information
Name
S-92
Designation
S-92
Alternate Designation
S-92A, S-92A+
Equipment Type
Civil Helicopters
Manufacturer
United Technologies
Date of Introduction
2004
Description

The S-92 designation applies to the commercial market variant which features multi-mission, high levels of safety, reliability, maintainability and low operating costs. H-92 designation is for military variants. Sikorsky claims that the levels of safety achieved by the new helicopter make it the world's safest rotorcraft. To do so, a state-of-the-art protection package was provided to crew and passengers. The S-92 itself builds on mission flexibility and low operating costs as key areas. It was fully certified to the latest FAA/JAA Part 29 requirements in 2002. In June 2004, it was certified by the European Aviation Safety Agency/Joint Aviation Authorities (EASA/JAA). Two powerful General Electric's CT7-8 engines are the key to the S-92 range, speed and maneuverability. The CT7-8 engine is a derivative of T700 engine family widely used on the successful H-60/S-70 Black Hawk helicopter family. In addition, these engines provide enough power to allow the aircraft to take-off weighing up to 11,800 kilograms and carrying 4,500 kilograms using an external cargo hook. The S-92 cabin is spacious and comfortable which allows to accommodate up to 19 passengers as well as two pilots. The S-92 helicopter can be configured to conduct Corporate/VIP transport, search and rescue (SAR), VVIP transport, scheduled airline service and offshore operations. In 2003, Cougar Helicopters of Canada became the launch customer for the S-92 with three helicopters on order. The first S-92 entered into service in September 2004 with Petroleum Helicopters, Inc. (PHI) on the Gulf of Mexico.

Air & Air Defense Specifications
Crew 2
Max Speed 281.0 km/h
Range 996.0 km
Service Ceiling 3261 m
Overview (Deagel)
Group Civil Helicopters
Status Active
Also Known As S-92A, S-92A+
Origin United States of America
Contractor United Technologies
Initial Operational Capability (IOC) September 2004
Total Production 244
Unitary Cost USD $17.0 million
Specifications (Deagel)
Crew 2
Main Rotor Blades 4
Number of Engines 2
Passengers 19
Tail Rotor Blades 4
Dimensions — Height 4.7 meter
Dimensions — Length 17.1 meter
Dimensions — Width 3.2 meter
Mass — Max Takeoff Weight 11,861 kilogram
Performance — Ceiling 3,261 meter
Performance — Max Range 996 kilometer
Power — Max Power at TakeOff 4,086 shp
Speed — Cruise Speed 254 kph
Speed — Top Speed at High Altitude 281 kph
Gear (Deagel)
Item 1 Turboshaft Engines: CT7-8 (2)
Item 2 Turboshaft Engines: RTM322-04/7 (2)
Variants
Variant 1 S-92
Variant 2 MH-92
Variant 3 VH-92A Patriot
Variant 4 S-92B
Details
Country of Origin United States
Category Rotary Wing Aircraft
Air > Rotary Wing Aircraft
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
17.1 m
Width
3.2 m
Height
4.7 m
Weight
11861 kg
Operators (17)
China
United States
United Kingdom
South Korea
Brazil
Azerbaijan
Bahrain
Brunei
Canada
Ireland
Kuwait
Mexico
Norway
Qatar
Saudi Arabia
Thailand
Turkmenistan
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