Vertipedia - Airbus Helicopters AS332 C Super Puma Mk I

MTOW 8600kg available with mod kit

Overview

Data on design, manufacture and status

Design authority: Airbus Helicopters

Primary manufacturer: Airbus Helicopters

Parent type: Airbus Helicopters H225/EC225/AS332

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift devices: 1 Single main rotor

Dedicated control device: 1 Tail rotor

Crew required: 1-2 in Side-by-side arrangement

Landing gear: Wheels (all retractable)

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

Layout and Dimensions

Weights and Performance

Engine Details

Primary Lift Device

Primary Control Device

Overall Dimensions
Overall Height:	4.94 m	16.2 ft
Overall Length:	18.70 m	61.4 ft
Overall Width:	15.60 m	51.2 ft

Airframe Dimensions
Airframe Length:	15.53 m	51.0 ft
Airframe Width:	3.79 m	12.4 ft
Airframe Height:	4.94 m	16.2 ft

Landing Gear Dimensions
Landing Gear Base:	4.49 m	14.7 ft
Landing Gear Track:	3.00 m	9.8 ft

Cabin Dimensions
Cabin Internal Height:
Cabin Internal Length:
Cabin Internal Width:

Weights
Max Gross Weight (ground):	8,350 kg	18,409 lb
Max Gross Weight (airborne):
Max Take-off Weight:	8,350 kg	18,409 lb
Empty Weight:

Climb Performance
Max Rate of Climb:

Hover Performance
Hover Ceiling IGE:
Hover Ceiling OGE:

Limitations
Max Level Flight Speed:
Never Exceed Speed:
Service Ceiling:

Range and Endurance
Max Range:
Max Endurance:

Provided powerplant data is for uninstalled, sea level, static operations.

Powerplant
Number of engines:	2
Designation:	Turbomeca Makila 1A turbine
Manufacturer:	Turbomeca

Normal Ratings
Max continuous:
Take-off / rated:
Intermediate:
Maximum:

OEI Ratings
OEI contingency:
OEI continuous:
OEI 30-second:
OEI intermediate:

Main Rotor Characteristics
Diameter:	15.60 m	51.18 ft
RPM:	265.0 rpm	265.0 rpm
Direction of Rotation:	Clockwise
Hub Type:

Main Rotor Blade Characteristics
Blade Construction:
Blade Chord:
Blade Tip Geometry:	Conventional
Blade Twist:
Number of Blades:	4

Main Rotor Derived Characteristics
Disc Area:	191.13 m²	2057.4 ft²
Disc Loading:	43.69 kg/m²	8.948 lb/ft²
Solidity:

Main Rotor Blade Derived Characteristics
Blade area per blade:
Tip Speed:	216.46 m/s	710.2 fps

Tail Rotor Characteristics
Diameter:	3.05 m	10.01 ft
Configuration:	Pusher
Direction of Rotation:	Top blade aft
RPM:

Tail Rotor Blade Characteristics
Number of Blades:	5
Blade Construction:
Blade Chord:
Blade Twist:

Tail Rotor Derived Characteristics
Disc Area:	7.31 m²	78.6 ft²
Solidity:

Tail Rotor Blade Derived Characteristics
Tip Speed:
Blade Area (per blade):

References

References and sources used

EASA Type Certificate Data Sheet R.002

European Aviation Safety Agency
EASA Type Certificate Database, 25 Jun 2014 (page 10)
Website

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Number of engines:	2 Turbines
Max Level Flight Speed:
Max Range:
Max Endurance:

Main Rotor Diameter:	15.60 m	51.18 ft
Max Gross Weight (ground):	8,350 kg	18,409 lb