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H-92 Superhawk Multi-Mission Helicopter

Crew

Three (Pilot, Co-pilot and observer)

Maiden Flight

December 2007

Manufacturer

Sikorsky Aircraft Corporation

Operators

CHC Helicopter, Bristow Helicopters, PHI and Cougar Helicopters

Length With Rotors Turning

20.88m

Fuselage Length

17.12m

Fuselage Width Including Sponsons

3.89m

Height With Rotors Turning

5.47m

Height to Top of Rotor Head

4.71m

Rotor Diameter

17.71m

Tail Rotor Diameter

3.35m

Empty Weight (SAR Configuration)

7,868kg

Empty Weight

6,895kg

Internal Fuel

2,143kg

Zero Fuel Weight

11,296kg

Number of Engines

Two

Maximum Take-Off Weight

12,995kg

Type

GE CT7-8A turboshaft engines

Rating

3,000shp each

Maximum Speed

306km/h

Maximum Cruise Speed

277km/h

Maximum Range

999km

Service Ceiling

4,563m

Avionics

Rockwell Collins

Flight Control Systems

BAE Systems

Countermeasure Systems and Radar Warning Receiver

Lockheed Martin

Engine

General Dynamics

Flight Deck

AIDC

Front of Sponsons

Embraer

Landing Gear and Fuel Integration System

Aerazur and Intertechnique

Cabin Interiors, Aft Fuselage, Tail Boom and Transmission Housing in the Upper Fuselage

Gamesa

Vertical Tail and Horizontal Stabiliser

Jingdezhen

Main Cabin

Mitsubishi

Maritime Surveillance Radar

Telephonics

Cockpit Seats

Martin-Baker
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