AEROSPATIALE SA-330 Puma
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
