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

 

Operated By
Irish Coast Guard Operational

Sikorsky S-92A

 

Forum Proceedings related to the Sikorsky S-92A

 

Vertiflite articles related to the Sikorsky S-92A

Fall 2008

How I Survived a Crash Involving the Fixed-Wing Support Aircraft During S-92A Icing Tests -

 

Vertiflite, Fall 2008

How I Survived a Crash Involving the Fixed-Wing Support Aircraft During S-92A Icing Tests -

 

 

Content from the AHS website related to the Sikorsky S-92A

 

We were unable to find any files on the AHS website for this aircraft.

 

Web pages

 

2014 Awards Recipients

 

 

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

 

 

Main rotor

 

 

Tail rotor

 

 

Miscellaneous

 

 

Sikorsky S-92A

Aircraft Notes

Ref. Author(s) Title Source Date Type
213 Kenneth I. Swartz "The CH-148 Cyclone Heads Out to Sea" Vertiflite, May/June 2016 2016 Periodical
269 Forecast International Rotorcraft Forecast 2013 May 2013 Report or Technical Manual