AEROSPATIALE SA-330 Puma

Aircraft
Name: 
SA-330 Puma
Manufacturer: 
Wing: 
Rotary
Position: 
Four-blade main rotor
Tail: 
Five-blade tail rotor
WTC
L
Type Code: 
H2T
Engine: 
Turboprop
Engine Count: 
Multi
Position: 
Above cabin
Landing gear: 
Tricycle retractable
Manufacturered as
AEROSPATIALE CH-33 Puma
AEROSPATIALE Puma
AEROSPATIALE SA-330 Puma
NURTANIO NSA-330 Puma
NURTANIO Puma
SUD Puma
SUD SA-330 Puma
WESTLAND Puma
IAR IAR-330 Puma
IAR Puma
ICA IAR-330 Puma
ICA Puma

PUMA

The Aérospatiale Puma is a four-bladed, twin-engined medium transport/utility helicopter. The Puma was originally manufactured by Sud Aviation of France under the designation SA.330.

Technical Data
Wing span: 
15.00 m
Length: 
18.15 m
Height: 
5.14 m
Powerplant: 

2 x Turboméca Turmo IVC turboshafts, 1,175 kW (1,575 hp) each

Indicative Performance Data
Take-Off
V2: 
n/a
Distance: 
n/a
MTOW: 
7400 kg
Initial Climb (to 5000 ft)
IAS: 
n/a
ROC: 
1400 ft/min
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: 
140 kts
MACH: 
n/a
Ceiling: 
195
Range: 
300 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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