Super Puma
Main description
The AS332 L1 is a twin engine medium-weight civil helicopter equipped with a « new avionics » glass cockpit.
Its operational characteristics and its large cabin explain its success particularly for passenger transport.
The extensive power reserve, its safety level, and comfort make the SUPER PUMA AS332 L1 an aircraft perfectly suited for offshore or other civil operations.
Characteristics
WEIGHTS |
|
|
| Empty weight, standard aircraft (including engine oil & unusable fuel)
|
4,510 kg |
9,943 lb
|
| Useful load | 4,090 kg
|
9,017 lb
|
| Maximum all-up weight | 8,600 kg
|
18,960 lb
|
| Maximum cargo-sling load | 4,500 kg
|
9,920 lb
|
| Maximum all-up weight
in external load configuration |
9,350 kg
|
20,615 lb
|
Note: Empty weight accuracy: within + 2%
PERFORMANCE
|
||
| Maximum speed, VNE (Never Exceed Speed) | 278 km/h
|
150 kts
|
| Fast Cruise speed at MCP (Max Continuous Power) | 262 km/h | 141 kts
|
| Rate of climb (85kt, 2 engines at MCP) | 8.2 m/s
|
1,618 ft/min
|
| Service ceiling (Rate-of-climb : 0.508m/s 100 ft/mn) | 2,895 m
|
9,500 ft
|
| Hover ceiling In Ground Effect (IGE) | 3,250 m
|
10,663 ft
|
| Hover ceiling Out of Ground Effect (OGE) | 2,300 m
|
7,546 ft
|
| Maximum range with standard tank | 841 km
|
454 nm
|
At Max Gross Weight, at Sea Level (SL), in International Standard Atmosphere (ISA) and zero wind condition.
ENGINES |
|
|
| Maximum emergency power (OEI 30â€) | 1,400 kW
|
1,877 shp
|
| Intermediate emergency power (OEI 2’) | 1,330 kW
|
1,783 shp
|
| Take-off power | 1,357 kW
|
1,819 shp
|
| Maximum continuous power | 1,185 kW
|
1,588 shp
|
Power per engine, in standard atmosphere, at sea level
