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AIRBUS HELICOPTERS EC-175

From SKYbrary Wiki
EC75
Aircraft
Name EC-175
Manufacturer AIRBUS HELICOPTERS
Body Narrow
Wing Rotary
Type code H2T
Engine Turboshaft
Engine count Multi
Mass group 3


Manufacturered as:


AIRBUS HELICOPTERS EC-175

AIRBUS HELICOPTERS EC-175

Description

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 14.80 m48.556 ft
Length 15.68 m51.444 ft
Height 5.34 m17.52 ft
Powerplant 2 x Pratt & Whitney Canada PT6C-67E turboshaft, 1,324 kW each.
Engine model Pratt & Whitney Canada PT6

Performance Data

Take-Off Initial Climb
(to 5000 ft)
Initial Climb
(to FL150)
Initial Climb
(to FL240)
MACH Climb Cruise Initial Descent
(to FL240)
Descent
(to FL100)
Descent (FL100
& below)
Approach
V2 (IAS) kts IAS kts IAS kts IAS kts MACH TAS 153 kts MACH IAS kts IAS kts Vapp (IAS) kts
Distance m ROC ft/min ROC ft/min ROC ft/min ROC ft/min MACH ROD ft/min ROD ft/min MCS kts Distance m
MTOW 70007,000 kg
7 tonnes
kg
Ceiling FL200 ROD ft/min APC
WTC Range 600600 nm
1,111,200 m
1,111.2 km
3,645,669.294 ft
NM

Accidents & Serious Incidents involving EC75

None on SKYbrary