S-92

S-92^® Helicopter

Power, agility and spacious cabin for multi-mission flexibility

The spacious, stand-up cabin of the S-92® helicopter provides the ultimate in comfort, safety and mission-flexibility required by demanding operators for a variety of roles, including offshore oil transport, executive transport, search and rescue, airline and utility. Airline configured S-92 helicopters seat up to 19 passengers in quiet, smooth and spacious airliner comfort, with power and endurance that enable fully loaded flights up to 430 nautical miles. Whatever your mission, the S-92 helicopter will provide a solution that best meets your needs.

Powerplant and fuel system

Number of Engines	2
Engine Type	GE CT7-8A
Take-off Shaft horsepower (5 min)	2,520 shp	1,897 kw
OEI Shaft horsepower (30 sec)	2,740 shp	2.043 kw

Performance

Maximum Gross Weight	26,500 lbs	12,020 kg
Maximum Cruise Speed	151 kts	280 kph
Maximum Range - No Reserve	539 nm	999 km
HIGE Ceiling	9,000 ft	2,743 m
HOGE Ceiling	6,500 ft	1,981 m
OEI Service Ceiling	5,000 ft	1,524 m
AEO Service Ceiling	15,000 ft	4,572 m

Accommodations

Cabin Length	20 ft	6.1 m
Cabin Width	6.6 ft	2.0 m
Cabin Height	6.0 ft	1.8 m
Cabin Area	128 ft2	11.9 m2
Cabin Volume	700 ft3	19.8 m3
Baggage Volume	140 ft3	3.96 m3

Airframe

Cabin: 6 ft high, 6.58 ft wide, 20 ft long
Hydraulic cargo ramp (140 cuft/3.9cum)
10 cabin windows
Air conditioning system
Active vibration control system
Retractable, energy-absorbing, tricycle landing gear

Cockpit

Health and Usage Monitoring System (HUMS)
Four-axis, fully-coupled autopilot
Enhanced Ground Proximity Warning System (EGPWS)
Traffic Collision Avoidance System (TCAS1)
Weather radar
Four 6 x 8 inch multi-function displays
Nav Management System
Collins Proline IV avionics
Cockpit Voice Recorder/Flight Data Recorder

Powerplant and fuel system

Integral inlet particle separator
Two GE CT7-8A turboshaft engines
Honeywell 30-150 APU
Pressure refueling system
Dual crashworthy fuel cells located in sponsons(380 gal / 1,440 l each)

Rotor and drive system

Four blade fully articulated main rotor system
Rotor brake system

Electrical

Two 60/75 KVA, oil spray cooled, 12,600 R.P.M. three phase generators
One APU driven, 30/35 KVA, air-cooled, 12,000 R.P.M. three-phase generator
Two generator control units
Two 400 amp, 28VDC regulated transformer rectifiers
One 125 amp, 28 VDC backup regulated transformer rectifier
One 15 amp-hour (cont. rating) 19-cell nickel-cadmium battery charged by DC converter
External power receptacles, one 28 VDC and 115 VAC
Two fixed landing lights
One controllable landing light
Provisions for Rotor Ice Protection System (RIPS)

Press Releases

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	05.08.13 Sikorsky Delivers First of Two VIP S-92® Helicopters to Turkish National Police for Service to the Turkish Prime Ministry Sikorsky Aircraft Corp. today announced it has delivered the first of two VIP S-92® helicopters to the Turkish National... more
	05.06.13 FAA Approves Sikorsky Aircraft’s New Platform Approach System for S-92® Helicopters — Feature Offers Enhanced Safety Through Reduced Pilot Workload Sikorsky Aircraft Corp. today announced the Federal Aviation Administration (FAA) has approved a new functionality on... more
	04.11.13 Sikorsky Aerospace Services Establishes Forward Stocking Location Facility in Brazil Sikorsky Aerospace Services (SAS) today announced in-country warehousing of spare parts in support of Brazil’s S-76® and... more