- Aircraft Overview
- Layout
- Powerplant
- Main Rotor
- Tail Rotor
- Performance
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Avicopter AC312A
The AC312A (variant of the AC312) is a 4 ton twin-turbine civil helicopter with a single main rotor and a fenestron; the main rotor 70 mm longer than the AC312. This version can carry a 1740 kg payload versus 1590 kg and has a Maximum Cruise Speed 7 km/h faster. With side by side seating arrangement, the cabin layout is [2 pilot + 12 pax]. In air medical service, the cabin layout may be [1-2 pilot + 4 stretchers + 1 med] or [1-2 pilot + 2 stretchers + 4 meds]. The AC312A is operated with either AVIC ENGINE WZ-8, or TURBOMECA Arriel 2C powerplants. Avicopter's AC312A obtained CAAC Type Certificate and Production Certificate, and passed the evaluation conducted by Aircraft Evaluation Group (AEG).
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Avicopter AC312A
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Avicopter AC312A
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Avicopter AC312A
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Avicopter AC312A
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Avicopter AC312A
This content is reserved for AHS members. If you are a current member, please use the Member Login link at the top of the page.
If you are not a member of AHS, why not join today? Be sure to also check out the many benefits enjoyed by AHS members.
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