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

Overview

Data on design, manufacture and status

Design authority: Sikorsky Aircraft Corp.

Primary manufacturer: Sikorsky Aircraft Corp.

Parent type: Sikorsky S-92/H-92

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift devices: 1 Single main rotor

Dedicated control device: 1 Tail rotor

Crew required: 2 in Side-by-side arrangement

Landing gear: Wheels (all retractable)

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

References

References and sources used

"The CH-148 Cyclone Heads Out to Sea"
Kenneth I. Swartz
Vertiflite, May/June 2016, 2016 (page 20)
Periodical

Rotorcraft Forecast 2013
Forecast International
May 2013 (page Section B)
Report or Technical Manual

Related VFS Resources

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Related Public Resources

Resources related to the S-92A , provided by public sources across the internet.

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