In numbers Through the lens Video
NATO reporting name: Helis
The letters "BC" indicate - British Columbia
Ka-32A11BC - export modification of the Ka-32A helicopter.
Ка-32А11ВС is designed for transportation of bulky cargoes on external sling, building and construction works, logging, SAR and fire-fighting operations, medical evacuation, law enforcement and special services support operations, passenger and cargo transportation inside the cabin. The helicopter can be successfully operated in densely built-up urban areas, adverse mountainous and wooded terrain, over land and vast water surfaces. The helicopter is capable of operating from small unprepared landing sites, vessels and oil rig platforms.
| The name of the helicopter version uses Latin letters, it is written in the same way in Russian as Ka-32A11BC and in English as Ka-32A11BC. Several times it appears as Ka-32A11VS (it may be mistranslated) © Konstantinos Panitsidis. |
Ка-32А11ВС helicopter has long-term off-base deployment and possibility of non-hangar storage.

Ka-32A11-the Ka-32A version intended for export to Canada (certified in line with US airworthiness standard FAR-29 in 1997). Currently received a certificate in accordance with the requirements of EASA.
Three-view drawing

Technical specifications
| DESIGNER | OKB Kamov |
| COUNTRY | Russia |
| TYPE |
Helicopter in role of firefighting
|
| CREW | 2 |
| POWER-PLANT | Two turboshaft engines TV3-117VMA Series 02 |
| Power, h.p. (H=0, V=0, ISA+15oC) | 2x2.256 |
| - emergency | |
| Maximum power take-off mode (ISA+25 / 15oC), h.p. | 2x2.200 |
| DIMENSIONS | |
| Length (with folded blades), m | 12,217 |
| Length (with blades), m | - |
| Helicopter width (with folded blades), m | 3,81 |
| Main rotor diameter, m | 15,90 |
| Number of blades | With the distinctive coaxial rotor (contra rotating blades, 2x3) |
| Height, m | 5,450 |
| Cabin internal dimensions, m: | |
|
- length, m
|
4,52
|
|
- width, m
|
1,30
|
|
- height (maximum), m
|
1,32
|
|
- area, m2
|
5,9
|
|
- volume, m3
|
7,3
|
|
Passengers, persons:
|
-
|
|
- passengers
|
13
|
|
- stretcher
|
2
|
|
- seats for the injured
|
6
|
| WEIGHT | |
| Maximum take-off, (with load on outer hook), kg | 12.700 |
| Normal take-off, kg | 11.000 |
| Empty, kg | 6.000 |
| Internal fuel, l | 2.450±26 |
| Warload, kg | - |
| Payload, kg | |
| - freight in cabin | 3.700 |
| - with on hook | 5.000 |
| PERFORMANCE | |
| Maximum speed, km/h | 260 |
| Cruising speed (with maximum continuous engine power), km/h | 245 |
| Maximum speed with load on external suspension (with on hook), km/h | 190 |
| Rate of climb, sea level (maximum power), m/sec | 15 |
| Maximum range with full fuel, km | 650 |
| Combat range, km | - |
| Service ceiling, m | 5.000 |
| Static ceiling, m | 3.700 |
| Maximum overload, g | - |
| ARMAMENT | Doesn't have (defensive). |
Photos Ka-32A11BC Multipurpose - firefighting helicopter