Kamov KA-32A
| Prix demandé | Prix sur demande |
|---|---|
| Localisation | London, UK |
| Seller | Exclusive Aircraft Sales Ltd |
| Vu pour la première fois | 2026-07-04 |
| Mis à jour | 2026-08-21 |
Voir sur exclusiveaircraft.co.uk →
Caractéristiques
Moteur & hélice
| Moteur | 2× TV3-117VMA TV3-117VMA |
|---|---|
| Type de moteur | turboshaft |
| Puissance | 2,200 hp |
Performances
| Vitesse de croisière | 119 kts |
|---|---|
| Vitesse maximale | 140 kts |
| Autonomie | 270 nm |
| Plafond pratique | 16,393 ft |
Poids & carburant
| Masse maximale au décollage | 11,000 kg |
|---|---|
| Poids à vide | 6,500 kg |
| Charge utile | 3,700 kg |
| Masse maximale au roulage | 11,000 kg |
| Capacité carburant | 2,650 L |
| Places | 13 |
Dimensions
| Longueur | 12.25 m |
|---|---|
| Hauteur | 5.4 m |
Description
Kamov Ka-32A For Sale. This KA 32A is an autonomous high-power-to-weight-ratio compact air transporter that can operate independently of ground support. The main roles of the Ka-32A civil helicopter are as passenger and cargo transport, a flying crane for building construction, transport for bulky cargo up to 5t carried on an external sling, logging, search and rescue, medical and emergency evacuation, loading and unloading ships at sea and offshore operations. If you are looking to buy a KA-32A this is a beautiful example avaliable now.
The helicopter construction, largely of titanium and composites, is highly corrosion resistant and therefore suitable for maritime roles.
The helicopter can be operated in adverse weather conditions, by day and night, over land and water surface, including marine climate and icing conditions, at geographical latitudes to 75. It can fly both by visual and instrumental flight rules (VFR and IFR).
The co-axial contra-rotating rotors allow very controlled, stable and precise flight, allowing the helicopter to carry loads with minimum deviation from the designated location, for example in narrow canyons and to allow precise placement of heavy loads for construction. The absence of the tail rotor contributes to the safety of the helicopter in manoeuvring near obstacles and in decreased sensitivity to changes in wind force and direction.
The Ka-32 has the capability to lift and transport 5t cargo loads on the external sling.
The lack of tail rotor ensures increased load lifting capacity, higher OGE hover ceiling and ability to fly at the altitude of 5000m (16393ft) due to higher efficiency of the helicopter coaxial configuration and lower (by 10÷15 %) power plant loss.
Absence of interaction between individual helicopter control channels makes the piloting easier and simpler.
Shorter tail boom and absence of a tail rotor make the helicopter very compact that, combined with its good piloting qualities, makes the helicopter very manoeuvrable and allows to operate the helicopter from off-shore platforms and landing sites of limited dimensions; the whole helicopter fuselage including its tail section is within the limits of the main rotors diameter.
The helicopter can land and takeoffs from unprepared sites including sites overgrown with shrubs.
Absence of tail rotor eliminates the personnel injuries when the helicopter is on the ground.
Photos
