Technical Data Ka-32A11BC Rev. A (eng.) · 2019. 12. 31. · Kamov Ka-32A11BC is a multifunctional...

Ka-32A11BCTechnical Data

KA32A11BC.A051F.TD00.00-P Revision A


This document contains a description of the helicopter, specifications and features that are provided for general information purposes only. Accurate description, characteristics and aircraft performance parameters of any particular helicopter may vary and depend on the final configuration chosen by the Customer, as well as the particular application, operating conditions and maintenance of the helicopter. On the characteristics and operating limitations must make reference to the approved Flight Manual and other relevant documentation.

The information contained in this document is subject to change without notice, but in any case, it is neither an offer nor contractual obligation until it is agreed in writingbetween the JSC “Russian Helicopters” and the buyer of the helicopter.

General data in this document are for information only. For details of specifications and operation limitations, please refer to operation manual and other official documents.

TABLE OF CONTENTS

1. Ка-32А11BC Program

2. Main Data

3. Overall Dimensions

4. Equipment and Design Features (standard configuration)

5. Helicopter configuring

6. Performance in Flight

7. Applications

8. Options

9. Operating Conditions

10. Perceived Noise Level

11. Helicopter and Component Life Time and Service Life

12. Maintenance and Overhaul

KA32A11BC.A051F.TD00.00-P Revision AGeneral data in this document are for information only.

For details of specifications and operation limitations, please refer to operation manual and other official documents.

КА-32А11BC PROGRAM

Kamov Ka-32A11BC is a multifunctional weatherproof helicopter assigned for passenger transportation, cargo transportation in cabin or on external sling, execution of special S&R operations, altitude-assembly works and also for complicated fire-fighting measures. The integration of modern developments the world's leading manufacturers of aircraft equipment can increase the complexity and quality of work and special operations.The design considers operational experience of Kamov KA-32 Family, as well as operator and customer requirements. Kamov Ка-32А11М meets the requirements of FAR29, АП-29 (AP-29).Ka-32A11BC is the only Russian helicopter, having the EASA type certificate and successfully operated in Canada, Spain, Portugal, Switzerland, China, Austria, South Korea, Indonesia.

Advantages

Кamov Ка-32А11BC shows maximum efficiency in its class when used for search-and-rescue operations, cargo transportation, patrolling the area.Кamov Ка-32А11BC has no rivals when operating in high mountains, at strong horizontal and vertical wind loads and in polar conditions.Capable of lifting 5 tons of load on its external load sling, Kamov Ка-32А11BC is the absolute leader among helicopters of similar load class.Advantages provided by coaxial main rotors system and high lifting capacity make Kamov Ка-32А11BC a unique machine, unrivaled for precise construction operations and fire fightingHigh life time of main units, competitive price and reliable after-sales support provide for extremely low flight hour costs and the lowest target task fulfillment cost among helicopters in its class.*Kamov Ка-32А11М offers easy maintenance and can be operated off-base for longer times at considerable distances from the main base.

Maintenance

The experience obtained in the course of operation of Ka-32 Family helicopters under extreme conditions has enabled on-condition operation of the helicopter and most of its systems. A combination of reliable and thorough structure of the helicopter, modern avionics and special equipment, as well as appropriate procedures of maintenance assure easy and convenient support of helicopter airworthiness as required by leading operators.

* As computed by “The Aircraft Cost Evaluator” of Conklin & de Decker KA32A11BC.A051F.TD00.00-P Revision A



MAIN PERFORMANCE PARAMETERS

Weights

Max take-off weight (with cargo in compartment) 11 000 kg 24 250 lb

Max take-off weight (with cargo on external load sling) 12 700 kg 28 000 lb

Empty weight for standard package 6800 kg 14991 lb

Max payload weight (in the cockpit) 3700 kg 8160 lb

Max payload weight (on external load sling) 5000 kg 11023 lb

Performance in flight

Max airspeed 260 km/h 140 kts

Cruising speed 230 km/h 124 kts

Max vertical speed 15 m/s 2952 ft/min

Max vertical speed for OEI (OEI 2.5 min) 2 m/s 393 ft/min

Hover ceiling IGE 4100 m 13451 ft

Hover ceiling OGE 3600 m 11811 ft

Max flight range with extra fuel tanks (H = 1000) 870 km 470 nm

Max flight time with extra fuel tanks ( H = 1000) 4ч 56 мин

Crew

Pilots 1 / 2

Passengers 13

Power plant (2 × ТВ3-117ВМА (TV3-117VMA))

Take-off power (5 min) 2 × 1618 kWt 2 × 2200 shp

Maximum continuous power 2 × 1250 kWt 2 × 1700 shp

OEI maximum short-time power (2.5 min) 2 × 1765 kWt 2 × 2400 shp

Fuel system capacity

Main fuel tanks 2450 l 647 USgal

Extra fuel tanks 1000 l 264 USgal



OVERALL DIMENSIONSOverall dimensions

Length 11,30 m 441,8 in

Length (with blades folded) 12.22 m 481,1 in

Height 5.4 m 215 in

Main rotor diameter 15.9 m 625,4 in

Cargo compartment

Length 4.52 m 167,3 in

Height 1.32 m 52 in

Width 1.45 м 57 in

Volume 7.30 cubic meters 257 cu ft


119.2” (3.03 m)441.8” (11.3 m)

55.4”(1.41 m)

138.2” (3.52 m)

215”

(5.4

5m

)

600× 900 mm

1240 mm945 mm

1450 mm

1320 mm

Emergency exit

Cargo compartment

door

1155 ×1140 mm

4525 mm

625.4” (15.9 m)


EQUIPMENT AND DESIGN FEATURES(standard configuration)

Airframe

Fuselage with tail fairing Power plant nacelle Two main landing gear struts Two nose landing gear struts Two detachable cockpit doors Cargo compartment door Emergency hatch of the cargo compartment


Helicopter configuration corresponds to the standard specification. The helicopter hasthe minimum equipment to carry out VFR. Certified by the AR IAC.

Three windows of cargo compartment Hatch in the fuselage nose for electronic

equipment installation Hatch in the tail boom for electronic

equipment installation Hatch in the fuselage bottom for optional

equipment installation

Power plant and fuel system

Two engines ТВ3-117ВМА (TV3-117VMA) series 2 Auxiliary power plant АИ-9 (AI-9) Two independent fuel systems with cross-feed valve

Dynamic system

Main rotor mast Set of upper main rotor blades (3 blades) Set of lower main rotor blades (3 blades)

Oil system of engines and gearbox Fire fighting system of the power plant Vibration measuring system

Gearbox ВР-252 (VR-252) Vibration dampers and blades of

lower main rotor

Helicopter systems

Control system for helicopter with steering wheel system

Hydraulics (normal pressure – 80 kgf/cm²)

Heating and ventilation Anti-ice system

Lighting

Two search-and-rescue lights Two signal flash beacon

Strobe light Set of navigation lights

EQUIPMENT AND DESIGN FEATURES (standard configuration)

General data in this document are for information only. For details of specifications and operation limitations, please refer to operations manual and other official documents.

Power supply

Power sources:● two generators (200/115 V, 400 Hz, 40 kVA)● converter (27/115 V, 400 Hz, 1000 VA)● converter (27/36 V, 400 Hz, 800 VA)● converter (27/36 V, 400 Hz, 25 VA)● two storage battery (24 V, 25 Ah)

Primary power supply system:● two independent electrical systems,

operating in parallel (200В/115 V, 400 Hz)

Secondary power supply system:● 36 V, 400 Hz three-phase AC generation system● 27 V DC generation system

Emergency power supply system:● Emergency power supply system (~115 V, 400 Hz)● Emergency power supply system (~36 V, 400 Hz)● Emergency power supply system (27 V)

Navigation equipment

Compass system Torque switch

Automatic direction finder

Avionics

Instrument decks and panels in the cockpit Integrated flight control system (ПКВ) ATC transponder Limiting signal system Radio altimeter Airspeed transmitter

Magnetic compass Two rate-of-climb indicators Two gyro horizons Two altimeters Electromechanical altimeter Aircraft clock

Cockpit equipment

Pilot seat with restrain system One pocket for flight maps

First aid kit Portable fire extinguisher

Communication equipment

HF radio Two VHF radios ( main and standby) Intercommunication equipment

Cockpit voice recorder incorporated in joint audio and flight data recorder system

ELT

Single package of operation facilities Spare parts kit Instruments and tools for ground servicing Operation and maintenance publications



HELICOPTER CONFIGURING

Ка-32А11ВСBaseline configuration (ВС)

Package options О1

Ка-32А11ВСConfiguration С2

Ка-32А11ВСConfiguration С1

Package options О2

Ка-32А11ВСCustomer configuration

corresponds to the EASA Certificate

EASA certificate is necessary EASA certificate isn’t necessary

+

=

Options list OL1 Options list OL2

Ка-32А11ВСCustomer configuration

Baseline configuration ВС – Helicopter configuration corresponds to the Standard specification.The helicopter has the minimum equipment to carry out VFR. Certified by AR IAC.

Package options О1 – A fixed set of options that allows to bring the helicopter Baseline configuration BC to theConfiguration C1.

Configuration С1 – Helicopter certified by EASA, AR IAC, as well as the aviation authorities of Canada, Chile, Mexico, Taiwan, China, Japan; equipped with an analog avionics set

Package options О2 – A fixed set of options that allows to bring the helicopter Baseline configuration BC to theConfiguration C2.

Configuration С2 – Helicopter certified by AR IAC, as well as the aviation authorities of China; equipped with a digital avionics set.

Options list OL1– options from the OL1 list certified by EASA , AR IAC, as well as the aviation authorities of Canada, Chile, Mexico, Taiwan, China, Japan. Option from the OL1 list can be used to configure the helicopter (EASA certificateis necessary) according to customer requirements.

Options list OL2 – options from the OL2 list certified by AR IAC, as well as the aviation authorities of China. Option from the OL1 list can be used to configure the helicopter (EASA certificate isn’t necessary) according to customer requirements.

▼ On request of the Customer and in agreement with the developer, on the helicopter C1 configuration can be installed options from OL2 options list, thus the helicopter with the specified options won't correspond to EASA certificate.

+

+ +

=

==



Package options «О1»

Package options «О2»

АТА № Option designation Qty.0001-00-01 Cockpit placards and indication in English language 1

0002-00-01 Indication using Imperial system of measurement 1

0003-00-01 EASA certification set

2510-07-01 Co-pilot seat with restraint system set

6700-01-01 Secondary controls set

7550-01-01 Engine air intake foreign objects ingestion protection set

Onboard registrars BUR-1-2B and MARS-BM set

АТА № Option designation Qty.0004-00-01 Automatic flight control system with MFDs set

2310-03-03 Prima HF radio 1

2340-01-01 Digital intercom and radio management equipment 1

3120-01-01 Alternative aircraft clock 1

3340-05-01 Strobe lights set

3450-01-01 Global navigation system 1

5210-01-01 Cargo compartment RH sliding door set

7550-01-01 Engine air intake foreign objects ingestion protection set

Prima-MV UHF radio 1

SO-96 ATC transponder 1



OPTIONS LIST «OL1»

Options from the OL1 list certified by EASA , AR IAC, as well as the aviation authorities of Canada, Chile, Mexico, Taiwan, China, Japan

АТА № Option designation Qty.2120-01-01 Electrical fans for crew 3

2510-01-01 Curtains for instrument flight simulation set

2510-02-01 Sun visors set

2510-03-01 Pilot armrest 1

2510-04-01 Rear-view mirrors 2

2520-01-01 Operator seat with restraint system set

2520-02-01 Foldable seats in cargo compartment 13

2520-05-01 Cargo compartment interior panels and lighting set

2620-01-01 Portable fire extinguisher in cargo compartment 1

3040-01-01 Windshield wipers set

3270-01-02 Skis on the nose and main landing gears set

3340-01-01 Landing and taxiing lights 4

3340-02-01 Additional search and landing light 1

3510-01-01 Oxygen equipment set set

5020-01-01 Tie-down fittings set

5020-02-01 Tie-down straps set

5020-03-01 External load sling set



ПЕРЕЧЕНЬ ОПЦИЙ «OL2»

Options from the OL2 list certified by AR IAC, as well as the aviation authorities of China

АТА № Option designation Qty.2120-01-01 Electrical fans for crew 3

2310-01-01 RT-5000 FLEXCOMM II wideband radio 1

2310-01-02 SRT-651 radio 1

2310-01-03 KTR908 VHF radio 1

2310-01-04 NPX138 FM radio 1

2310-03-01 KHF1050 HF radio 1

2310-03-02 HF9000 HF radio 1

2350-01-01 Additional headsets Up to 4

2350-02-01 David Clark headsets Up to 5

2430-01-01 Equipment for IFR flights 1

2510-01-01 Curtains for instrument flight simulation set

2510-02-01 Sun visors set

2510-03-01 Pilot armrest 1

2510-04-01 Rear-view mirrors 2

2510-05-01 Comfortable crew seats Up to 3

2510-06-01 Heated lower hemisphere view mirror with remote control set

2510-07-01 Co-pilot seat with restraint system set

2520-01-01 Operator seat with restraint system set

2520-02-01 Foldable seats in cargo compartment 13

2520-04-01 Passengers soft headrests set

2520-05-01 Cargo compartment interior panels and lighting set

2523-01-01 Medical patient handling platform, USA made 1

2523-02-01 Stretchers Up to 4

2523-03-01 Paramedic case 1

2523-04-01 Foldable paramedic work table 1



АТА № Option designation Qty.2523-05-01 Immobilizing mattress 1

2523-06-01 Medical pneumatic splints set

2523-07-01 Artificial lung ventilator, Drager Medical 1

2523-08-01 Defibrillator with monitor, Physio-Control 1

2523-09-01 Aspirator, Laerdal Medical 1

2560-01-01 First-aid kit in the cargo compartment 1

2560-02-01 Life rafts, Aerazur 3

2560-02-02 Life rafts, Russian made 3

2560-03-01 Life vests, Aerazur Up to 11

2560-03-02 Life vests, Russian made Up to 11

2560-04-01 Crew life belts Up to 3

2560-05-01 ME 406 ELT 1

2570-01-01 Winch cargo system 1

2570-01-02 Electric winch, Goodrich 1

2570-02-01 Strap lifting seat 1

2570-03-01 Operator safety belt 1

2570-06-01 Loudspeaker system 1

2570-07-01 Wire cutters 1

2570-08-01 Attachments for rappelling device 1

2620-01-01 Portable fire extinguisher in cargo compartment 1

2810-01-01 Auxiliary fuel tanks set

3040-01-01 Windshield wipers set

3270-01-01 Skis on the main landing gears set

3270-01-03 Skis on the nose and main landing gears set

3270-03-01 Ditching float system 1

3340-01-01 Landing and taxiing lights 4

ПЕРЕЧЕНЬ ОПЦИЙ «OL2» (Cont.)



АТА № Option designation Qty.3340-02-01 Additional search and landing light 1

3340-03-01 Winch light 1

3340-04-01 Search light 1

3410-01-01 Second radio altimeter without indicators set

3430-01-01 Navigation-landing system Up to 2

3440-01-01 Search and weather radar 1

3450-02-01 DME 2

3450-03-01 Search ADF 1

3450-04-01 Mode S ATC transponder 1

3450-04-02 Mode S ATC transponder with TIS 1

3510-01-01 Oxygen equipment set 1

5020-01-01 Tie-down fittings set

5020-02-01 Tie-down straps set

5020-03-01 External load sling 1

5030-01-01 Underslung Bambi Bucket fire fighting system 1

5030-01-02 Underslung Bambi Bucket fire fighting system with foaming agent feed 1

5030-01-03 Underslung Bambi Bucket fire fighting system with water pumping and foaming agent feed 1

5030-01-04 Simplex fire fighting system, 3000 liters capacity 1

5030-01-05 Simplex fire fighting system with foaming system, 3000 liters capacity 1

5030-03-01 Baggage compartment for bucket and special equipment transportation 1

5490-01-01 Engine air intake dust protection devices set

5630-01-01 Opening windows in cargo compartment sliding doors Up to 2

6700-01-01 Secondary controls set

KA32A11BC.A051F.TD00.00-P Revision AGeneral data in this document are for information only.

For details of specifications and operation limitations, please refer to operations manual and other official documents.

ПЕРЕЧЕНЬ ОПЦИЙ «OL2» (Cont.)



PERFORMANCE

Payload/Range


MSA. Pressure altitude 500 mFuel reserve for 20 min. flight

nm

RANGE, km

0 50 100 150 200 250400

500

600

700

800

900

900

10001100

1200

1300

140015001600

1700

18001900

0 20 40 60 80 100 120 140

1100010000 9000 8000

0 50 100 150 200 250400

500

600

700

800

900

1100010000 9000 8000

900

1000

11001200

13001400

15001600

17001800

1900

0 20 40 60 80 100 120 140

Minimal flight fuel consumption

Fuel

con

sum

ptio

n, k

g/h

Flight speed, km/h

IASKnots

lb/h

Fuel

con

sum

ptio

n, k

g/h

lb/h

Flight speed, km/h

Knots

H = 0 H = 1000 m

Gross weight, kg

Maximum range

Gross weight, kg

Maximum range

Maximum duration

Maximum duration

Payload at theexternal sling

Payload inside.Main fuel tanks full

Payload inside.Main and auxiliaryfuel tanks fullP

aylo

ad, k

g

Pay

load

, lbx

1000


PERFORMANCE


-50 -40 -30 -20 -10 0 10 20 30 40 50 600

500

1000

1500

2000

2500

3000

3500

4000

4500

5000

0

2000

4000

6000

8000

10000

12000

14000

16000

900010000110001200012600

-50 -40 -30 -20 -10 0 10 20 30 40 50 60

0

500

1000

1500

2000

2500

3000

3500

4000

4500

5000

0

2000

4000

6000

8000

10000

12000

14000

16000

900010000110001200012600

0 50 100 150 200 250 300 350

0

1

2

3

4

5

60 40 80 120 160

Hover ceiling IGETakeoff Power

IAS IAS +30 °С IAS +30 °СIAS

Hover ceiling OGETakeoff Power

TEMPERATURE, °C TEMPERATURE, °C

ft

Pre

ssur

e A

ltitu

de, m

ft

Pre

ssur

e A

ltitu

de, m

Gross weight, kg Gross

weight, kg

Hovering 1 min IGEClimbing H = 500 m, economic speedFlight to search area, best en-route speed Glide, economic speedLoitering in search area, economic speedHovering OGE, 30 minutes. Evacuation of 10 personsClimbing H = 500 m, economic speedFlight from search area, best en-route speedHovering 1 min IGEFuel reserve for 20 min at economic speed

Loite

ring

time,

h

Radius of distance, km

nm

Maximum time required for SAR operation

Full filling of main tanksFull filling of main and

extra fuel tanks

KA32A11ВС.A051F.TD00.00-P Revision A

APPLICATIONS

TRANSPORTATION AND CONSTRUCTION


With maximum lifting capacity (5000 kg) for external load sling in its class and advantages of coaxial rotor system, Kamov Ка-32А11BCoffers the best performance of external load transportation and,especially, precise building and assembly jobs. Resistance to variable wind loads, enhanced stability and simplepiloting assure operations both in open areas and in dense building of the city. Helicopter parameters can entirely change the concept of helicopter efficiency for construction in mountain areas, so that even an average rated pilot can perform this kind of mission.

RECOMMENDED HELICOPTER CONFIGURATION FORTRANSPORTATION AND CONSTRUCTIONConfiguration described by the "Standard Specification KA-32A11BC» № KA32A11BC.A051F.SS00.00RU and supplemented by the following options list.

324.TAC (E)EASA certificate is necessary

0001-00-01 Cockpit placards and indication in English language

0002-00-01 Indication using Imperial system of measurement

0003-00-01 EASA certification

2120-01-01 Electrical fans for crew

2350-01-01 Additional headsets

2510-01-01 Curtains for instrument flight simulation

2510-02-01 Sun visors

2510-03-01 Pilot armrest

2510-04-01 Rear-view mirrors

2510-02-01 Co-pilot seat with restraint system

2520-01-01 Operator seat with restraint system

3040-01-01 Windshield wipers

3270-01-03 Skis on the nose and main landing gears

3340-01-01 Landing and taxiing lights

3340-02-01 Additional search and landing light

3510-01-01 Oxygen equipment set

5020-01-01 Tie-down fittings

5020-02-01 Tie-down straps

5020-03-01 External load sling

6700-01-01 Secondary controls

7550-01-01 Engine air intake foreign objects ingestion protection

324.TACEASA certificate isn’t necessary

0004-00-01 Automatic flight control system with MFDs


2310-03-03 Prima HF radio

2340-01-01 Digital intercom and radio management equipment


2430-01-01 Equipment for IFR flights





2510-06-01 Heated lower hemisphere view mirror with remote control







3450-01-01 Global navigation system

3450-04-03 SO-96 ATC transponder

3450-05-01 Satellite navigation system BMS





5210-01-01 Cargo compartment RH sliding door




APPLICATIONS

MEDEVAC


When equipped with medical instruments (medical module with the removable stretchers, oxygen equipment, defibrillator, cardiograph, extra lights and electrical equipment) Kamov Ка-32А11BC helicopteris excellent for medical evacuation, both at long range from a hospital, and at dense building of a city. The helicopter can carry up to 4 standard stretchers having a patient securing system. Wide sliding doors from left and right side (optional) of the cargo compartment afford to waste no time during the evacuation. Coaxial rotor system enhances the helicopter stability in turbulence, makes the transportation of patients safer and provides for morecomfortable work of medics.


324.MEDEASA certificate isn’t necessary

0001-00-01 Cockpit placards and indication in English language0002-00-01 Indication using Imperial system of measurement0004-00-01 Automatic flight control system with MFDs2120-01-01 Electrical fans for crew2310-03-03 Prima HF radio2340-01-01 Digital intercom and radio management equipment2350-01-01 Additional headsets2430-01-01 Equipment for IFR flights2510-01-01 Curtains for instrument flight simulation2510-02-01 Sun visors2510-03-01 Pilot armrest2510-04-01 Rear-view mirrors2510-05-01 Comfortable crew seats2510-07-01 Co-pilot seat with restraint system2520-02-01 Foldable seats in cargo compartment2520-05-01 Cargo compartment interior panels and lighting2523-01-01 Medical patient handling platform, USA made2523-02-01 Stretchers2523-03-01 Paramedic case2523-04-01 Foldable paramedic work table2523-05-01 Immobilizing mattress2523-06-01 Medical pneumatic splints2523-07-01 Artificial lung ventilator, Drager Medical2523-08-01 Defibrillator with monitor, Physio-Control2523-09-01 Aspirator, Laerdal Medical2560-01-01 First-aid kit in the cargo compartment2560-03-01 Life vests, Aerazur2560-05-01 ME 406 ELT2620-01-01 Portable fire extinguisher in cargo compartment2810-01-01 Auxiliary fuel tanks3040-01-01 Windshield wipers3120-01-01 Alternative aircraft clock3270-01-03 Skis on the nose and main landing gears3340-01-01 Landing and taxiing lights3340-02-01 Additional search and landing light3340-05-01 Strobe lights3410-01-01 Second radio altimeter without indicators3430-01-01 Navigation-landing system3450-01-01 Global navigation system3450-02-01 DME3450-04-01 Mode S ATC transponder3510-01-01 Oxygen equipment set5210-01-01 Cargo compartment RH sliding door5630-01-01 Opening windows in cargo compartment sliding doors6700-01-01 Secondary controls7550-01-01 Engine air intake foreign objects ingestion protection

Общие данные, содержащиеся в настоящем документе приведены исключительно в информационных целях.Для использования характеристик и эксплуатационных ограничений должна быть использована информация из эксплуатационных и иных официальных документов.


324.SAREASA certificate isn’t necessary













2510-05-01 Comfortable crew seats



2520-02-01 Foldable seats in cargo compartment

2520-04-01 Passengers soft headrests

2520-05-01 Cargo compartment interior panels and lighting

2560-01-01 First-aid kit in the cargo compartment

2560-02-01 Life rafts, Aerazur

2560-03-01 Life vests, Aerazur

2560-04-01 Crew life belts

2560-05-01 ME 406 ELT

2570-01-02 Electric winch, Goodrich

2570-02-01 Strap lifting seat

2570-03-01 Operator safety belt

2570-06-01 Loudspeaker system

2570-08-01 Attachments for rappelling device

2620-01-01 Portable fire extinguisher in cargo compartment

2810-01-01 Auxiliary fuel tanks


3120-01-01 Alternative aircraft clock


3270-03-01 Ditching float system



3340-03-01 Winch light

3340-04-01 Search light

3340-05-01 Strobe lights

3430-01-01 Navigation-landing system

3440-01-01 Search and weather radar


3450-02-01 DME

3450-03-01 Search ADF

3450-04-02 Mode S ATC transponder



5630-01-01 Opening windows in cargo compartment sliding doors



Kamov Ка-32А11BC is an irreplaceable rescue helicopter for mountain areas difficult to access, many kilometers sea surface and impassable forest-covered heights. A wide spectrum of optional equipment affords urgent evacuation of disabled persons, and take rescue teams with specialized equipment to emergency situations areas. The helicopter is fit for search-and rescue in adverse weather, day and night, at sea and in icing condition, practically in every climate and geographic zones. Kamov Ка-32А11BC can take-off and land at prepared and non-prepared sites, so persons to be saved can reach it easily. When landing is impossible, an electrically driven hoist can safely lift and evacuate injured persons.

APPLICATIONS

SEARCH-AND-RESCUE



Simplex

Bambi-Bucket

324.FFW (E)EASA certificate is necessary










2510-06-01 Heated lower hemisphere view mirror with remote control









5030-01-01 Underslung Bambi Bucket fire fighting system



324.FFWEASA certificate isn’t necessary




2310-01-05 Prima-MV UHF radio











2570-07-01 Wire cutters





3410-01-01 Navigation-landing system

3430-01-01 Search and weather radar


3450-02-01 DME

3450-03-01 Search ADF

3450-04-03 SO-96 ATC transponder

3450-05-01 Satellite navigation system BMS


5030-01-04 Simplex fire fighting system, 3000 liters capacity

5030-02-01 "Water Cannon" fire fighting system






This helicopter is most efficient when used for fire fighting at high floors and roofs of tall buildings, fire at oil-filling tankers and tanks, at fuel, chemical and oil-refining plants, fire in oil and gas production areas, large postemergency fire of grounded aircrafts, accidents and catastrophes of trains, sea and river ships, for making protective belts around forestry fire and solid foam belts at aerodrome runway in case of aircraft emergency landing. For fire fighting, the helicopter uses “Bambi-Bucket” or “Simplex” system and a water foam gun.

APPLICATIONS

FIRE FIGHTING


Water foam tank capacity 4996 lWater withdrawal time 50 sWater basin depth ≤0.5 m

Depending on the distance

between the seat of fire and the water withdrawal point, the

helicopter can bring and pour

the following approximate amount of water:

Distance to water basin,

km

Amount of

water, tons

0.5 50

3 36

5 28


324.SPT (Е)EASA certificate is necessary
























324.SPTEASA certificate isn’t necessary








2510-05-01 Comfortable crew seats




2520-04-01 Passengers soft headrests



2560-02-01 Life rafts, Aerazur

2560-03-01 Life vests, Aerazur

2560-04-01 Crew life belts


2810-01-01 Auxiliary fuel tanks


3270-03-01 Ditching float system







APPLICATIONS

SERVICE PASSENGER TRANSPORTATION

For service passenger transportation, 13 foldable seats with restraint system may be installed in the cargo compartment of Kamov Ka-32A11BC. To make flight more comfortable soft headrests and furnish of interior panels may be provided in cargo compartment.The helicopter is equipped with life vests and group rescue equipment -life rafts for overwater missions. Thus the helicopter is equipped with the ditching float system.




OPERATING CONDITIONS

Kamov Ка-32А11BC operates in any climate:

–50 °С / +45 °С outside air temperature Up to 100 % relative air humidity At the aerodromes and ground sites with

minimum soil density of 4 kgf/cm² (56 lb/sqin) and slopes up to 6°

For take-off and landing, Kamov Ка-32А11BC needs a site of at least 40×40 meters(132×132 ft), including safety zones along the perimeter.

For operations on soft ground (density up to 2.5 kgf/cm² (36.7 lb/sq in) the helicopter may be equipped with skids.

PERCEIVABLE NOISE

Кamov Ка-32А11BC meets the requirements of the Aviation Rules, Part 36, and the international standard for Environmental Protection (ICAO Annex 16, chapter 8).

MTOW Kamov Ка-32А11BC noise:


Stage of flight Noise,EPNdB

Requirement, EPNdB

Take-off 93.5 100.4

Cruising in a level flight 99.4 99.4

Approach for landing 96.8 101.4


LIFE TIME AND SERVICE LIFE

Performance history of Kamov Ka-32 Family helicopters and research accomplished by Kamov Company made it possible to assign longer life time to Kamov Ka-32A11BC and its major components featuring limited life time.

Kamov continues research aimed at extension of life time and service life of components with limited life time and plans further enhancement to helicopter life time to achieve higher operational economic efficiency of Kamov Ка-32А11BC helicopters.

Assigned life time of Kamov Ка-32А11BC components

Life time,flight hrs

Calendar life, years

Helicopter as a whole 32,000 30

ТВ3-117ВМА (TV3-117VMA) series 2 engine 4,500 Not limited

АИ-9 (AI-9) APU Accordingmanufacturer

logbook

Not limited

ВР-252 (VR-252) gearbox 2,000 Not limited

Main rotor mast 6,000* Not limited

Blades 3,000 20

*Provided the repair or maintenance work by the developer or the developer authorized service center every 1000+200 hours, but not less frequently than every 8 years

TBO and service life of Kamov Ка-32А11BC components

Life time, flight hrs

Calendar life, years

Helicopter as a whole Not limited Not limited

ТВ3-117ВМА (TV3-117VMA) series 2 engine 1,500 10

АИ-9 (AI-9) APU Accordingmanufacturer

logbook

10

ВР-252 (VR-252) gearbox 500** 8

Main rotor mast 1,000 8

Blades – operation w/o scheduled repairs**Approval for exploitation more than 500 hours (increase intervals up to 1,000 hours of use) is produced every 250 hours based on the assessment of technical condition of the developer (manufacturer) component at the expense of the Customer.




MAINTENANCE AND OVERHAUL

The system of maintenance established for Ка-32А11BC includes the following steps: level “О”, level “I”and level “D”.

Level “О” includes:• routine maintenance;• storage maintenance;• equipment diagnostics and replacement of failed blocks (if any).

Level “О” can be performed directly at the helicopter base. Routine maintenance represents a system of preliminary operations, inspections and testing of helicopter to provide for serviceability, readiness and application in accordance with its configuration in the intervals between periodic maintenance sessions.

Routine maintenance includes: • pre-flight preparation;• turn-around procedures;• post-flight procedures.

Total time of routine maintenance procedures: • pre-flight preparation: not less than 25 min;• turn-around preparation: not less than 20…25 min;• post-flight preparation: not less than 25…30 min.

Full filling of fuel tanks lasts no longer than 11 minutes for single-point pressure fuelling and no longer than 22 minutes for fuelling through tank filling necks.

Storage maintenance should be performed when the helicopter has not been flown for over 15 days. On a temporarily closed-down helicopter, storage maintenance should be performed every 15 and 30 days of parking. The helicopter, however, must be preserved when it is planned to be grounded for longer than 30 days.

Labor intensiveness of level “0” equals:• 1.22 man-hour / flight hour for on-line maintenance; • 0.4 man-hour / flight hour for storage.



Level “I” includes:• periodic maintenance (schedule maintenance) of the helicopter;• repair of helicopter blocks and units by replacement of failed parts and modules.

Periodic maintenance of Ка-32А11BC, its systems and units include 25,50,100,300,600 hour schedule works.

Schedule maintenance of ТВЗ-117ВМА (TV3-117VMA) series 2 engines should be performed every 100, 200,300, 500,1500 and 2000 flight hours.

Level “D” includes reconditioning overhaul of the components having fixed TBO, and reconditioning of the components to be operated on-condition.

Level “D” repair can be performed either by specialized service centers or by manufacturing companies.

Full list, periods and scope of maintenance can be found in the Operation Manual of Ка-32А11BC.

MAINTENANCE AND OVERHAUL


Kamov Public Joint Stock CompanyRussia, 140007, Moskow region,Lyubertsy, 8 Marta st., 8аe-mail: [email protected]: www.kamov.ruphone: +7 (495) 994-4800fax: +7 (495) 700-3071

General data in this document are for information only. For specifications and operation limitations, please refer to operational manuals and other official documents.

www.kamov.ru


Technical Data Ka-32A11BC Rev. A (eng.) · 2019. 12. 31. · Kamov Ka-32A11BC is a multifunctional...

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