S92
SIKORSKY S-92
SIKORSKY S-92
Aircraft
Name
S-92
Manufacturer
Wing
Rotary
Position
Four-blade main rotor
Tail
Four-blade tail rotor
WTC
M
Type Code
H2T
Engine
Turboshaft
Engine Count
Multi
Position
Above cabin
Landing gear
Tricycle retractable
Manufacturered as
SIKORSKY S-92 Helibus
SIKORSKY CH-148 Cyclone
SIKORSKY Cyclone
SIKORSKY H-92 Superhawk
SIKORSKY Superhawk
SIKORSKY Helibus
S92
Medium-lift two engine, four-blade transport/utility helicopter with 19/22 seats used for various types of operations - offshore oil transport, search and rescue, airline services and others.
Technical Data
Wing span (metric)
17.17 m
Length (metric)
17.10 m
Height (metric)
4.71 m
Powerplant
2 x General Electric CT7-8A turboshaft, 2,740 shp (2,043 kW) each.
Engine Model(s)
General Electric CT7
Indicative Performance Data
Take-Off
V2
n/a
Distance
n/a
MTOW
12000 kg
Initial Climb (to 5000 ft)
IAS
n/a
ROC
n/a
Initial Climb (to FL150)
IAS
n/a
ROC
n/a
Initial Climb (to FL240)
IAS
n/a
ROC
n/a
MACH Climb
MACH
n/a
ROC
n/a
Cruise
TAS
140 kts
MACH
n/a
Ceiling
150
Range
490 NM
Initial Descent (to FL240)
MACH
n/a
ROD
n/a
Descent (to FL100)
IAS
n/a
ROD
n/a
Descent (FL100 & below)
IAS
n/a
MCS
n/a
ROD
n/a
Approach
Vapp (IAS)
n/a
Distance
n/a
