AW119Kx General Presentation Decembre 2014 - Estado Mayor Conjunto.pdf

AW119Kx Base Àerea IV Brigada Mendoza - 2-3-de Diciembre de 2014

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Value Propositions

AW119Kx Offers: 

More Room Than Any Other Light Single Turbine Helicopter



High Level of Performance



Great Safety, “fail safe” design and redundancy of main systems



Modern Avionics



High Flexibility



Competive Acquisition & Maintenance Costs

AW119 Koala Development 2000

2005

2010

Derived from the AW109Power and incorporating features typical of a light twin helicopter the A119Koala has benefitted from continuous improvement in capabilities, performance and technologies to meet the evolving Customer requirements 3

Product Evolution AW119 – AW119Kx

AW119Kx

AW119Koala

AW119Ke

Sales (as of Noviembre 2014)

more than

240 aircraft (order & options)

in 33 countries by 104 customers

Fleet & Sales Data By areas Europe

24%

31%

Asia & Australasia 13% 19%

Africa C. & S. America

13%

North America

By applications EMS/SAR

15% 34%

7%

Military Govern. & Law Enf.

10%

Utility 13%

21%

Offshore Corp/Vip

Fleet leader: Tri-State Care Flight SN 14032 – 5700 FH

Leading Safety Features Fully Articulated Titanium Rotor & Composite Main Rotor Blades

1002 SHP P&W Single Turbine Engine 30 Minute Run-dry Transmission High Visibility Reinforced Windshield

Dual Hydraulic System Redundant Electrical System Redundant Fuel System Large Unobstructed Cabin for Higher Flexibility

Main Features WEIGHT SUMMARY Maximum Take Off Weight (internal load) 2850 kg Maximum Take Off Weight (external load) 3150 kg Basic Empty Weight

 1

1455 kg

SEATING MINIMUM CREW: PASSENGERS:

ONE PILOT SEVEN

VOLUMES PILOT & PAX CABIN 4.96 m3 BAGGAGE COMPARTMENT 0.95 m3

Pilot +7 pax

Safety by design High inertia rotor blades for safe autorotation

“Cocoon type” crash protective airframe

Windshield bird strike protection

Transmission dry run capability: 30 min

Redundancy of main systems

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Safety – Redundancy of Main Systems HYDRAULIC SYSTEM

ELECTRICAL SYSTEM

Redundancy Of All Main Systems:

 Hydraulic System  Fuel System  Electrical System  Automatic Stabilization System:  2 Modes Of Operations  SAS  Att Hold

 High Level Of Safety In Case Of Failure

FUEL SYSTEM

AUTOMATIC STABILIZATION SYSTEM

Main and Tail Rotor

MAIN ROTOR

Fully articulated titanium rotor hub with composite blades and elastomeric bearings For smooth and stable control response in all flight conditions including autorotation Reduced maintenance

TAIL ROTOR

Steel rotor hub with composite blades High lateral lateral controllability

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Engine & Transmission Ratings

ENGINE with EEC (Electronic Engine Control) PRATT & WHITNEY PT6B-37A

Take Off Power Max Continuous Power

1002 shp 872 shp

TRANSMISSION AGUSTAWESTLAND

Take Off Power (5min) Max Continuous Power

917 900

shp shp

Run Dry Capability

30

min

Performance (ISA, SL, MTOW) VNE

281 km/h

152 kts

Max Cruise Speed

257 km/h

139 kts

HIGE

3352 m

11000 ft

HOGE

2225 m

7300 ft

Service Ceiling

4572 m

15000 ft

Max Range (*)

954 km

515 nm

Max Endurance (*)

(*) with 688 kg of usable fuel (no reserve) @ 5000 ft

5 h 20 min

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Stability and yaw control Lateral wind up to 40 kts

High controllability assuring safe operational conditions 14

Modular Fuel system Modular design 3-CELL: 484 kg - 605 l 4-CELL: 568 kg - 711 l 5-CELL: 696 kg - 870 l

No reduction of useful volumes in cabin and in baggage compartment 15

Operational Flexibility Hoist Operator Seat

Configuration:

Copilot

SAR/Surveillance Litter

Hoist

Pilot

1 Litter Medical Attendants Seats

2 Litters

Training

Passenger Transport

Instructor Seat

Fuel Tanks

Six Pax Seats 16

Internal Volume Baggage compartment 6 5

5,91 1,51

4

m3 3

Cockpit 3,45

2

Cabin

Maximum load: 150 kg

Baggage compartment

1 0,95

0 AW119Ke

 High comfort for passengers in the cabin

 Baggage compartment separated from cabin & easily accessible 17

Convertible Interior 1/2 pilots + 6/7 passengers

1/2 pilots + 1 stretcher + 4/5 passengers 1/2 pilots + 2 stretcher + 2/3 passengers

High flexibility

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Corporate/VIP interior

Space and Comfort Unique “Single Engine ” with separate cabin 19

EMS Interior

1 or 2 longitudinal litters with no intrusion into the cockpit 2 attendants + 2 patients as the larger twin engine h/c

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New Glass Cockpit The AW119Ke is offered with one of the most modern and integrated glass cockpit today available in the market, similar to the ones installed on larger and heavier helicopters. The AW119Ke VFR avionic package consists of the Garmin G1000H integrated flight deck system, civil certified FAA. Engine information are integrated in the G1000H avionic suite. The AW119Ke avionic suite allows also IFR training. PFD

MFD

FLIR image displayed on MFD

ICS control panel (co-pilot) ICS control panel (pilot)

Ergonomic cockpit with improved situational awareness and reduced pilot workload 21

Garmin G1000H Glass Cockpit

Caution, Warning switches

Electronic Standby Instrument System

Primary Flight Display PFD displays:  Airspeed  Attitude  Altitude  Heading  Slip/skid indicators  360° HSI  COM 1/2 Communication frequencies  VOR/LOC 1/2 NAV frequencies  Clock 

XPDR current status

FMS - FLIGHT PLANNING The system can create and store up to 1,000 user-defined waypoints Flight planning on the system consists of building a flight plan by entering waypoints one at a time, adding waypoints along airways, and inserting departures, airways, arrivals, or approaches Up to 99 flight plans with up to 99 waypoints each can be created and stored in memory Flight plans can be imported from a SD Card or exported to a SD Card from the Stored Flight Plan Page Waypoints can be added to the active flight plan or any stored flight plan

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Synthetic Vision

SVS – 3D Synthetic Vision System Provides realistic, real-time 3D virtual reality view of the helicopter attitude and flight

trajectory and the outside world in any weather conditions

CLEAR SKY

CLOUDS / FOG

NIGHT

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HTAWS & HITS

TAWS – Terrain Awareness Warning System

HITS – Highway In The Sky

Provides a map of terrain and sounds an audible

Displays the desired navigation route in 3D using a series

warning if the airplane approaches too close to terrain or

of skyway boxes

a structure

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Digital Moving Map Digital moving map Provides real-time flight information on the map that illustrates the position and direction of the aircraft

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New Nose Equipment Layout

New

New New New

New

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Optional equipment

Cargo hook (1400 kg)

Emergency floats

Dual cargo hook (1400 kg/500 kg)

Electrical rescue hoist 204 kg (450 lbs) 50 m Cable

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Fire Fighting Equipment

Belly tank: 1200 l Operational Strengths: – Greatest water volume capacity – High altitude performance – Wide temperature range

Bambi Bucket: 910 l

Rear view mirrors Electrically adjustable and electrically heated mirror Fixed rear view mirror

The pilot monitors the sling load during flight 31

Crew doors windows Bubble window (on the RH cockpit door)

High visibility doors

Better visibility on sling load during operations 32

ADDITIONAL EQUIPMENT Baggage compartment extensions (1.9 m) Dual controls Fuel cap with key-lock Reinforced windshields (pilot and co-pilot) Rotor Brake Sliders on cockpit doors windows Windshield wipers (pilot/copilot) with wiper switch on cyclic grip BASIC AIRCRAFT INTERIOR AVIONIC PACKAGE Bleed air heater •Two GDU-1040 10.4” display units providing a Primary Flight Display Primer finished cabin walls (PFD) and a Multifunction Display (MFD) and integrating: UTILITY CONVERTIBLE INTERIOR Radio tuning controls Soundproofing Flight Management System (FMS) Painted liners Synthetic Vision System Seats covered with leatherette •Two GIA-63H Integrated Avionics Units (IAU) comprising: 3 aft facing seats (central bench) with individually foldable black panels COM 1&2 3 fwd facing seats (aft bench) with individually foldable black panels NAV 1&2 Provision for locking system for stretcher on back panel seats, aft and central bench GPS 1&2 3-point shoulder harness with inertial reels and black coloured safety belts for all •GTX-33H Mode-S Transponder with Extended Squitter (ES) capability passenger seats •Digital Audio Control System (DACS) NAT with two cockpit panels Reading lights, advisory lights •Magnetic Compass indicator Cabin loudspeakers •L3 Avionics System ESI-2000 Electronic Standby Indicator Rubber carpet •Engine Hour meter PAINTING STANDARD EQUIPMENT AgustaWestland painting scheme, metallic colours from Company selection 28 Ah battery (in lieu of 22 Ah battery) AVIONIC EQUIPMENT Active Noise Reduction (ANR) headsets (pilot and co-pilot) Active Noise Reduction (ANR) headset (Qty 3) Baggage compartment lights ELT C406-N HM Artex Crew open door actuators Radio altimeter FreeFlight RA-4500 First aid kit UTILITY EQUIPMENT Fuel drain electrical valves 188 USgal fuel system Portable fire extinguisher Bubble Windows Quick disconnecting chip detectors External hoist (450 lb) provision Shoulder harness with inertial reels (pilot and co-pilot) External hoist (450 lb) removable Tail boom strake Search Light Spectrolab SX-5 Starburst ADDITIONAL AVIONIC EQUIPMENT Wire strike protection system AC power supply system (2 inverters) Estimated Equipped Empty Weight: 1737 kg AFCS 3-axis duplex SP-711 Honeywell

Configuration

±2% tolerance

Data contained in this presentation are preliminary and represent AgustaWestland best estimation. Data is subject to change without notice and is not to be used for operational purposes nor constitute a contractual commitment.

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SAR Mission analysis 250

Search time over area - min

200

150

100

Mission Weights Max Gross Weight: EEW: Pilot: 2 Operators: Rescued person: Fuel Reserve:

2850 kg 1737 kg 85 kg 85 kg (each) 85 kg 40 kg

Flight Assumptions Temperature: Cruise Altitude: Loitering: 5 min HOGE for rescuing: Fuel reserve: Max Range Cruise Speed:

ISA+20°C 6000 ft 4000 ft 4000 ft 20 min @ 70 kts 120 kts

50

0 0

50

100

150

200

250

Radius to search area - nm

 1 hr:55 min of searching time 100 nm far from base Data contained in this presentation are preliminary and represent AgustaWestland best estimation. Data is subject to change without notice and is not to be used for operational purposes nor constitute a contractual commitment.

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Operational Flexibility

OFFSHORE

LAW ENFORCEMENT AERIAL WORK

PAX TRANSPORT

EMS SAR VIP CORPORATE

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Customer Service and Support

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AW Customer Support & Services FSRs

Regional Offices

AW CUSTOMER SUPPORT - LONATE (ITALY) AW PHILADELPHIA – PHILADELPHIA (USA) AW DO BRASIL – SAO PAOLO (BRAZIL)

HEADQUARTER CUSTOMER SUPPORT & SERVICES

CUSTOMER SERVICE

Supply Centers

24/7 FLEET OPERATIONS CENTRE

Headquarter Back Offices

AAS – LIEGE (BELGIUM) AW MALAYSIA – KUALA LUMPUR (MALAYSIA) MIDDLE EAST – ABU DHABI / DUBAI (UAE) Innovative Web Services

R&O Centers

Service Stations

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Support and Maintenance

3 years warranty 2 inspection programs High overhaul intervals Customer Service: 24 hr/365 days

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Main Components TBO

High Operational availability thanks to high limits TBOs of the main components Time Between Overhaul (TBO) Main transmission assembly

4800 FH

Tail rotor gearbox assembly

4800 FH

Main rotor servo actuator assembly

1800 FH

Tail rotor servo actuator assembly

1800 FH

Engine

3000 FH 39

Conclusion

THE A119 KOALA OFFERS: More Space Than Any Other Light Single Exceptional Flexibility Superior Performance

High Productivity Great Reliability

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