SA330 Puma

Aircraft type

Data given for the Aérospatiale SA330 J Puma in basic configuration.

Manufacturer Aérospatiale
Aircraft family Helicopter
Engine type Turboshaft
Engine count 2
ICAO code PUMA

Technical specifications

Design
Main rotor blades
4
Main rotor count
1
Dimensions
Height
5.14 m
16.86 ft
Length
14.82 m
48.62 ft
Main rotor diameter
15.09 m
49.51 ft
Width
3 m
9.84 ft
Fuel
Fuel capacity
1,544 l
408 us gal
Performance
Service ceiling
13,500 ft
4,110 m
Speed limits
Vne
167 kt
309 km/h / 192 mph
Weight limits
MLW
7,400 kg
16,310 lb
MTOW
7,400 kg
16,310 lb

Aircraft models

Manufacturer Name
Aérospatiale SA330 A Puma
Prototype
Aérospatiale SA330 B Puma
Aérospatiale SA330 F Puma
Retired
Aérospatiale SA330 G Puma
Retired
Aérospatiale SA330 J Puma

Engine models

Manufacturer Name Cont. T/O
Safran Helicopter Engines Turmo IV C 960 kW 1115 kW