Ка-226 helicopter ka-226 helicopter program director zarschikov denis © 2011 ОАО...

Ка-226 HelicopterKa-226 helicopter Program Director

Zarschikov Denis

© 2011 ОАО «Вертолёты России». Все права защищены

Contents

Ka-226 helicopter. General Information

Helicopter operation milestones

Modifications & Development

Helicopter systems

After Sales Support

Ka-226 helicopter. General Information

Ka-226 – light multipurpose helicopter with coaxial rotor, twin «ROLLS-ROYCE» engines.

Main applications of Ka-226 «250-C20R/2» helicopter model:


Patrol, Law enforcement

EMS

Compact design

Excellent maneuverability and controllability for flights in dense urban

conditions

Take-off/landing capability in constrained conditions

Helicopter Ка-226. Main Advantages

Maximum safety in flight (Category А)

Continues take-off and safe landing in case on one engine failure

OEI flight ability in a wide temperature/altitude range independently

of gross weight

Absence of a tail rotor – safety on the ground

Helicopter Ка-226. Safe Application

Torsion type hubs No lubrication points Latent defect manifestation excluded Damage resistance Favorable operation experience

© 2011 JSC Russian Helicopters. All rights reserved

Main Rotor System

The main distinctive feature of the Ка-226Т is its fuselage modular design enabling its multifunctional operation by application of unified easily detachable modules containing mission equipment.


Modular Design

Helicopter operation milestones

- Ministry of Interior Affairs

- Federal Security Service of Russia

- «International Airport Orenburg»

- EMERCOM of Ukraine

- «Gazpromavia»

- 9 AC

- 6 AC

- 2 AC

- 1 AC

- 4 AC

The beginning of Ка-226 helicopter operation: February 2006

Number of in-operation helicopters: 22

Ka-226 helicopter operators:

Helicopter operation


Kazan(Republic of Tatarstan)

Astrahan

Nalchik

Sankt-Petersburg

Voronezh

Moscow

Operation areas


Orenburg

Krasnodar

Stavropol

Gelendgik Yoshkar-Ola

Total fleet utilisation: 6307 flight hours (June 2011)


17%

66%

14%

3%

0,15%


Since 2006 to the present time Kamov company has collected information about 205 failures of Ка-226 helicopter.

29%

9%

2,5% 5,25%

2% 2%

5%

20%

11%

5,25% 2%

7%

Helicopter system failures


№ Year

Number of failures in

flights Average FH before failure

1 2009 15 95,2

2 2010 18 126

Note: Data extractions from reports №№ 226-93-47/10 и 226-93-16/11

Helicopter Ка-226 reliability : years 2009-2010

Modifications & Development


Helicopter Ка-226ТDeliveries to civil and military Customers in the RF and world markets Main application versions – transportation/passenger, cargo, EMS, emergency

rescue, patrol, reconnaissance/surveillance, fire fighting.

Helicopter Ка-226Т,Modification of a serially produced

Ка-226 helicopter

Proposed certification : to АП-29 Requirements (IAC AR)

– 4th quarter 2012 to CS-29 Requirements (EASA)

– 4th quarter 2013


Helicopter Ка-226T

The Ka-226T can be operated in the following conditions:

IFR&VFR both day and night standard and adverse weather conditions icing conditions over vast water surface in tropical conditions within () 50C to () 50C temperature range at max wind speeds of

16 m/s at hover 18 m/s at rotor speed up18 m/s at take-off and landing5 m/s at tail wind take-off and landing from ground sites of min 4 kgf/cm2 soil density from sloped sites with lower limit () 5, upper limit () 10and lateral limit ()

6 to max altitude 7000 m


Helicopter Ка-226Т. Operating conditions

Perfomance Ка-226 Ка-226Т

Max take-off/landing weight 3400 kg 3600 кг

Maximum flight weight масса 3600 kg 3800 кг

OEW 2230 kg 2000 кг

Max internal load weight in transportation cabin 1100 kg 1200 кг

Max external load weight at the sling 1300 kg 1500 кг

Hover ceiling OGE 2600 м 4100 м

Service ceiling 5500 м 5700 м

Max non-exceeded speed 210 km/h 250 km/h

Max cruising speed 190 km/h 220 km/h

Crew 1 pilot 1 pilot

Passenger 7 pax 7 pax


Flight performance

Nos DescriptionTime to overhaul

hrs/yearsService life limit

hrs/years

1 Fuselage none 18000 / 30

2 Engine 3000 / - Not limited

3 Gear box 2000 / - 6000/30

4 Main rotor mast 3000 / - 6000 / 30

5 Main rotor blades 3000 / - 6000 / 30

6 Dual actuator unit 3000 / - 6000 / 30


Ка-226Т. SERVICE LIFE LIMITS OF MAIN COMPONENTS

Helicopter systems


Main gear ВР-226Н

«Turbomeca» Arrius 2G1 Engines

AERAZUR anticrash fuel system

Dual actuator unit КАУ-165М

Windscreen mitigates the consequences of a birdstrike

Integrated Flight & Navigation System.


Ка-226Т Main Modifications & Development

Power ratings, hp.Contingency 705Tale-off 580Max continuous 580

Output shaft speed, rpm 6 000Fuel consumption, kg/hp per hour

at take-off rating 0,260At max continuous rating 0,283

Engine installation weight, kg 118


Arrius 2G1 Engine

Modern piloting and navigational equipment

Integrated navigational system

Autopilot

Several variants of equipment configuration are available providing for VFR

and IFR flights for one and two pilots

© 2011 ОАО «Вертолёты России». Все права защищены© 2011 JSC Russian Helicopters. All rights reserved

Integrated Flight & Navigation System

Fuel tank volume 920 LSingle point pressure fuelling provided

Auxilliary tanks can be installed and connected

1.Front fuel tanks2.Fuel quantity

transmitters3.Pumps4.Drain output5.Aft fuel tank6.Overflow pipes7.Tank attachments8.Filler ports9.Residue drain

cocks


AERAZUR anticrash fuel system

Crashworthy crew and passenger seats from Fisher+Entwicklunger GmbH & Co KG are certified to JTSO-C127a standard and comply with the FAR-27/29 requirements, endure longitudinal load 18.4 g and vertical load to 30 g. Crew seats can be adjusted to individual pilot parameters both vertically and horizontally.


Crashworthy crew and passenger seats

Skies allow to operate the helicopter from sites of soil density below 4 kgf/cm2


Optional equipment Skies

Attachment points are provided on the helicopter to install hoisting devices like an ЛПГ-300 or a Goodrich winch of up to 300 kg capacity


Optional equipment Winch

External sling can be used to transport loads weighing to 1500 kg on the helicopter with its transportation cabin module installed or not installed


Optional EquipmentExternal Load Sling

Attachment points are available on the helicopter to mount an inlet particle used separator to clean the air supplied to the engines of dust, sand and foreign objects during taxiing, take off and landing at sandy airfields or

dusty sites. 95 % air purification is provided.


PALL IPS

Aircraft diagnostic system monitors operation and performs diagnostics of engines and main gear box condition and main rotor balance status in flight

and on the ground in order to reveal potentially dangerous defects


Aircraft diagnostic system. БСДВ-226

Skies allow to operate the helicopter from sites of soil density below 4 kgf/cm2


Optional equipment. Skies


EMS

Universal platform with oxygen bottle Removable stretcher (1 pc) Support for infusions Oxygen control panel, the wall for medical equipment installation


Easily cleaned cabin

paneling

Operation lights in

transportation cabin

for sliding and aft

doors

Auxiliary technical

systems

Medical equipment

Dry wash stand

Medical personnel seats (2 pcs)

Hydro insulating floor cover

EMS


Thank you

Ка-226 helicopter ka-226 helicopter program director zarschikov denis © 2011 ОАО...

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