AEROSPATIALE AS-332 Super Puma
AEROSPATIALE AS-332 Super Puma
Aircraft
Name:
AS-332 Super Puma
Manufacturer:
Wing:
Rotary
Position:
Four-blade main rotor
Tail:
Five-blade tail rotor
WTC:
M
APC:
A
Type Code:
H2T
Engine:
Turboshaft
Engine Count:
Multi
Position:
In fuselage
Landing gear:
Tricycle retractable
Manufacturered as
AEROSPATIALE AS-332B Super Puma
AEROSPATIALE AS-332B1 Super Puma
AEROSPATIALE AS-332C Super Puma
AEROSPATIALE AS-332F1 Super Puma
AEROSPATIALE AS-332L Super Puma
AEROSPATIALE AS-332L Tiger
AEROSPATIALE AS-332L1 Super Puma
AEROSPATIALE AS-332M Super Puma
AEROSPATIALE AS-332M1 Super Puma
AEROSPATIALE AS-532SC Cougar
AEROSPATIALE AS-532UC Cougar
AEROSPATIALE AS-532UL Cougar
AEROSPATIALE Cougar
AEROSPATIALE Hkp10 Super Puma
AEROSPATIALE Super Puma
AEROSPATIALE Tiger
ATLAS Oryx
ATLAS SA-330 Oryx
CASA AS-332 Super Puma
CASA Cougar
AS32
Twin engine medium lift helicopter.
Technical Data
Wing span:
15.00 m
Length:
16.36 m
Height:
4.92 m
Powerplant:
2 x Turboméca Makila 1A1 turboshaft, 1,300 kW (1,742 shp) each.
Engine Model:
Turboméca Makila
Indicative Performance Data
Take-Off
V2:
n/a
Distance:
n/a
MTOW:
7800 kg
Initial Climb (to 5000 ft)
IAS:
80 kts
ROC:
1500 ft/min
Initial Climb (to FL150)
IAS:
80 kts
ROC:
700
Initial Climb (to FL240)
IAS:
n/a
ROC:
n/a
MACH Climb
MACH:
n/a
ROC:
n/a
Cruise
TAS:
157 kts
MACH:
n/a
Ceiling:
170
Range:
460 NM
Initial Descent (to FL240)
MACH:
n/a
ROD:
n/a
Descent (to FL100)
IAS:
130 kts
ROD:
1000 ft/min
Descent (FL100 & below)
IAS:
90 kts
MCS:
n/a
ROD:
1000 ft/min
Approach
Vapp (IAS):
40 kts
Distance:
n/a
