EC75
AIRBUS HELICOPTERS EC-175
AIRBUS HELICOPTERS EC-175
Aircraft
Name
EC-175
Manufacturer
Body
Narrow
Wing
Rotary
Type Code
H2T
Engine
Turboshaft
Engine Count
Multi
Manufactured as
Cite This Page
SKYbrary Aviation Safety. (March 8, 2021). EC75.
Retrieved June 4, 2026
from https://skybrary.aero/aircraft/ec75
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EC75
The Airbus Helicopters EC175 (also Avicopter Z-15) is a 7-ton class medium utility helicopter being developed by Airbus Helicopters (formerly Eurocopter) Group and AVIC.
Technical Data
Wing span (metric)
14.80 m
Length (metric)
15.68 m
Height (metric)
5.34 m
Powerplant
2 x Pratt & Whitney Canada PT6C-67E turboshaft, 1,324 kW each.
Engine Model(s)
Pratt & Whitney Canada PT6
Indicative Performance Data
Take-Off
V2
n/a
Distance
n/a
MTOW
7000 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
153 kts
MACH
n/a
Ceiling
200
Range
600 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
