AIRBUS HELICOPTERS H225 Super Puma Mk II+

Aircraft
Name: 
H225 Super Puma Mk II+
Manufacturer: 
Body: 
Narrow
Wing: 
Rotary
WTC
M
APC
A
Type Code: 
H2T
Engine: 
Turboshaft
Engine Count: 
Multi
Manufacturered as
EUROCOPTER Caracal
EUROCOPTER Cougar Mk2+
EUROCOPTER EC-225 Super Puma Mk2+
EUROCOPTER EC-725 Caracal
EUROCOPTER EC-725 Cougar Mk2+
EUROCOPTER Super Puma Mk2+
AIRBUS HELICOPTERS Cougar Mk2+
AIRBUS HELICOPTERS EC-225 Super Puma Mk2+
AIRBUS HELICOPTERS EC-725 Cougar Mk2+
AIRBUS HELICOPTERS H-225 Cougar Mk2+
AIRBUS HELICOPTERS H-225 Super Puma Mk2+
AIRBUS HELICOPTERS Super Puma Mk2+

EC25

The The Airbus Helicopters H225 Super Puma Mk II+ is a long-range passenger transport helicopter developed as the next generation in the civilian Super Puma family. It is a twin-engined aircraft and can carry up to 24 passengers along with 2 crew and a cabin attendant, dependent on customer configuration. The helicopter is marketed for offshore support and VIP passenger transport duties, as well as public service missions.

The H225 (and EC-225) is based on the Eurocopter AS332L2 Super Puma, improving upon the design with a five-blade main rotor incorporating a new airfoil shape to reduce vibration levels. The helicopter is powered by two Turbomeca Makila 2A1 turboshaft engines mounted over the cabin, which feature a dual-channel Full Authority Digital Engine Control (FADEC) system and anti-icing system to enable it to operate in very cold climates. Other improvements include a reinforced main rotor gearbox and a full glass cockpit with Active Matrix Liquid Crystal Displays.

Technical Data
Wing span: 
16.20 m
Length: 
19.50 m
Height: 
4.97 m
Powerplant: 

2 x Turboméca Makila 2A1 turboshaft engines, 1,776 kW (2,382 hp) each

Engine Model: 
Turboméca Makila
Indicative Performance Data
Take-Off
V2: 
n/a
Distance: 
n/a
MTOW: 
11200 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: 
130 kts
MACH: 
n/a
Ceiling: 
200
Range: 
250 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

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