| General Description
The Alouette III's fully articulated three-bladed main rotor helps to reduce noise and vibration.
The tail boom is of semi-monocoque contruction carrying a stabilizer with two lateral fins and a guarded
three-bladed tail rotor. Ground operations are facilitated by the tricycle landing gear's castering nose
wheel.
The aircraft's versatility is enhanced by:
- Fittings for various items of optional equipment such as hoist, cargo
hook, flotation gear, etc.
- External power receptacle.
- Integral hoisting rings, jacking pads and footsteps for access to rotor head.
- 3 adjustable and quick removal bench seats with back rests and safety belt.
- Cargo tie down rings.
- Provision for dual controls.
- Adjustable front ventilation system and adjustable ventilators on doors.
- Data case under front seats.
- 2 jettisonable sliding rear doors.
The Alouette III is powered by a Artouste III B1 (870 HP) turbine engine with a 4 kW, 28.5 volt DC
starter-generator, supported by a 40 amp hour battery.
Specifications
The following performance figures are based on the mean values obtained with a new engine. Unless
otherwise stated, they are given for clean aircraft, in zero wind at sea level and with standard atmospheric
conditions. Use for reference only, not for actual flight
calculations.
| Specification |
Unit |
Ac/Wt |
Ac/Wt |
Ac/Wt |
| Weight (standard aircraft 2,732 lbs.) |
lb |
3,750 |
4,190 |
4,850 |
| VNE |
kts |
113 |
113 |
113 |
| Cruising speed |
kts |
108 |
105 |
100 |
| Fuel consumption at cruising speed |
U.S. gal./nm |
0.54 |
0.56 |
0.59 |
| Rate of climb, oblique flight |
ft/min |
1,712 |
1,417 |
846 |
| Range |
nm |
281 |
275 |
267 |
| Endurance |
hr |
3.35 |
3.25 |
3.0 |
Hovering ceiling I.G.E. ISA |
ft |
19,520 |
16,080 |
9,350 |
Hovering ceiling I.G.E. ISA + 20 degrees |
ft |
17,060 |
13,165 |
7,050 |
Hovering ceiling O.G.E. ISA |
ft |
18,370 |
15,090 |
4,920 |
Hovering ceiling O.G.E. ISA + 20 degrees |
ft |
16,240 |
12,795 |
2,790 |
| Service Ceiling |
ft |
20,670 |
17,552 |
10,500 |
|