Sikorsky S-92A

	From the third prototype onward, and for all production aircraft including the S-92A, the tail plane was on the stbd side below the tail rotor
	Attribution Attribution	Overview Parent type S-92/H-92 Variant S-92 Design authority Sikorsky Aircraft Corp. Primary manufacturer Sikorsky Aircraft Corp. Key Characteristics Operational status Operational Max gross weight (ground)   269 12,020 n/a 12,020 n/a Crew 2 Seating arrangement Side-by-side Configuration VTOL type Helicopter Compound type None Lift configuration Single main rotor Control device type Tail rotor Features Number of engines 2 Number of propulsors 0 Number of lift devices 1 Number of control devices 1

Sikorsky S-92A

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Sikorsky S-92A

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Sikorsky S-92A

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Sikorsky S-92A

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Sikorsky S-92A

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Sikorsky S-92A

Sikorsky S-92A

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Articles from the Journal of the American Helicopter Society related to the Sikorsky S-92A

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Articles from NASA Technical Reports Server related to the Sikorsky S-92A

 

Patent information from the US Patent and Trademark Office related to the Sikorsky S-92A

 

Google Books related to the Sikorsky S-92A

Sikorsky S-92A

Overview

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Main rotor

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Tail rotor

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Miscellaneous

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Sikorsky S-92A

Aircraft Notes