aw119kx general presentation decembre 2014 - estado mayor conjunto.pdf
TRANSCRIPT
-
1
AW119Kx
Base erea IV Brigada
Mendoza - 2-3-de Diciembre de 2014
-
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
Value Propositions
-
3
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
AW119 Koala Development
-
AW119Koala
AW119Ke
AW119Kx
Product Evolution AW119 AW119Kx
-
Sales (as of Noviembre 2014)
more than 240 aircraft (order & options) in 33 countries by 104 customers
-
Fleet leader:
Tri-State Care Flight
SN 14032 5700 FH
Fleet & Sales Data
15%
7%
10%
21%13%
34%
EMS/SAR
Military
Govern. & Law Enf.
Utility
Offshore
Corp/Vip
24%
13%
13%19%
31%
Europe
Asia & Australasia
Africa
C. & S. America
North America
By areas
By applications
-
Leading Safety Features
Fully Articulated Titanium Rotor &
Composite Main Rotor Blades
High Visibility Reinforced
Windshield
Large Unobstructed Cabin for
Higher Flexibility
Dual Hydraulic System
Redundant Electrical System
Redundant Fuel System
1002 SHP P&W Single Turbine Engine
30 Minute Run-dry Transmission
-
Main Features
WEIGHT SUMMARY
Maximum Take Off Weight (internal load) 2850 kg Maximum Take Off Weight (external load) 3150 kg Basic Empty Weight 1455 kg
VOLUMES PILOT & PAX CABIN 4.96 m3
BAGGAGE COMPARTMENT 0.95 m3
1 Pilot +7 pax SEATING
MINIMUM CREW: ONE PILOT PASSENGERS: SEVEN
-
9
Safety by design
Cocoon type crash protective airframe High inertia rotor blades for safe autorotation
Transmission
dry run
capability:
30 min
Windshield bird strike protection
Redundancy of
main systems
-
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
HYDRAULIC SYSTEM ELECTRICAL SYSTEM
FUEL SYSTEM AUTOMATIC STABILIZATION
SYSTEM
Safety Redundancy of Main Systems
-
11
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
-
Take Off Power 1002 shp
Max Continuous Power 872 shp
ENGINE with EEC (Electronic Engine Control)
Take Off Power (5min) 917 shp
Max Continuous Power 900 shp
Run Dry Capability 30 min
TRANSMISSION
AGUSTAWESTLAND
PRATT & WHITNEY PT6B-37A
Engine & Transmission Ratings
-
13
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 (*) 5 h 20 min
(*) with 688 kg of usable fuel (no reserve) @ 5000 ft
-
14
Stability and yaw control
Lateral wind up to 40 kts
High controllability assuring safe operational conditions
-
15
Modular Fuel system
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
Modular design
-
16
Configuration:
SAR/Surveillance
1 Litter
2 Litters
Training
Passenger
Transport
Litter
Copilot
Pilot
Hoist
Operator
Seat
Hoist
Instructor
Seat
Fuel
Tanks
Medical
Attendants
Seats
Six Pax
Seats
Operational Flexibility
-
17
0,95
3,45
1,51
0
1
2
3
4
5
6
AW119Ke
m3 Cockpit
Cabin
Baggage compartment
Internal Volume
Baggage compartment
Maximum load: 150 kg
High comfort for passengers in the cabin
Baggage compartment separated from cabin & easily accessible
5,91
-
18
1/2 pilots + 6/7 passengers
1/2 pilots + 1 stretcher + 4/5 passengers
1/2 pilots + 2 stretcher + 2/3 passengers
Convertible Interior
High flexibility
-
19
Space and Comfort
Unique Single Engine with separate cabin
Corporate/VIP interior
-
20
EMS Interior
1 or 2 longitudinal litters with no intrusion into the cockpit
2 attendants + 2 patients as the larger twin engine h/c
-
21
New Glass Cockpit
Ergonomic cockpit with improved situational awareness and reduced pilot workload
MFD PFD
ICS control
panel (pilot)
ICS control
panel (co-pilot)
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.
FLIR image displayed on MFD
-
Electronic
Standby Instrument
System
Garmin G1000H Glass Cockpit
Caution,
Warning
switches
-
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
Primary Flight Display
-
24
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
FMS - FLIGHT PLANNING
-
25
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
Synthetic Vision
-
26
TAWS Terrain Awareness Warning System
Provides a map of terrain and sounds an audible
warning if the airplane approaches too close to terrain or
a structure
HTAWS & HITS
HITS Highway In The Sky
Displays the desired navigation route in 3D using a series
of skyway boxes
-
27
Digital moving map
Provides real-time flight information on the map that illustrates the position
and direction of the aircraft
Digital Moving Map
-
28
New Nose Equipment Layout
New
New
New
New
New
-
29
Optional equipment
Electrical rescue hoist
204 kg (450 lbs)
50 m Cable
Cargo hook (1400 kg) Emergency floats
Dual cargo hook (1400 kg/500 kg)
-
Fire Fighting Equipment
Operational Strengths:
Greatest water volume capacity
High altitude performance
Wide temperature range
Belly tank: 1200 l Bambi Bucket: 910 l
-
31
Rear view mirrors
Electrically adjustable and electrically heated mirror Fixed rear view mirror
The pilot monitors the sling load during flight
-
32
Crew doors windows
High visibility doors Bubble window (on the RH cockpit door)
Better visibility on sling load during operations
-
33
Configuration 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
INTERIOR
Bleed air heater
Primer finished cabin walls
UTILITY CONVERTIBLE INTERIOR
Soundproofing
Painted liners
Seats covered with leatherette
3 aft facing seats (central bench) with individually foldable black panels
3 fwd facing seats (aft bench) with individually foldable black panels
Provision for locking system for stretcher on back panel seats, aft and central bench
3-point shoulder harness with inertial reels and black coloured safety belts for all
passenger seats
Reading lights, advisory lights
Cabin loudspeakers
Rubber carpet
PAINTING
AgustaWestland painting scheme, metallic colours from Company selection
AVIONIC EQUIPMENT
Active Noise Reduction (ANR) headset (Qty 3)
ELT C406-N HM Artex
Radio altimeter FreeFlight RA-4500
UTILITY EQUIPMENT
188 USgal fuel system
Bubble Windows
External hoist (450 lb) provision
External hoist (450 lb) removable
Search Light Spectrolab SX-5 Starburst
Wire strike protection system
Estimated Equipped Empty Weight: 1737 kg 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.
BASIC AIRCRAFT
AVIONIC PACKAGE
Two GDU-1040 10.4 display units providing a Primary Flight Display (PFD) and a Multifunction Display (MFD) and integrating:
Radio tuning controls Flight Management System (FMS) Synthetic Vision System
Two GIA-63H Integrated Avionics Units (IAU) comprising: COM 1&2 NAV 1&2 GPS 1&2
GTX-33H Mode-S Transponder with Extended Squitter (ES) capability Digital Audio Control System (DACS) NAT with two cockpit panels Magnetic Compass indicator L3 Avionics System ESI-2000 Electronic Standby Indicator Engine Hour meter STANDARD EQUIPMENT
28 Ah battery (in lieu of 22 Ah battery)
Active Noise Reduction (ANR) headsets (pilot and co-pilot)
Baggage compartment lights
Crew open door actuators
First aid kit
Fuel drain electrical valves
Portable fire extinguisher
Quick disconnecting chip detectors
Shoulder harness with inertial reels (pilot and co-pilot)
Tail boom strake
ADDITIONAL AVIONIC EQUIPMENT
AC power supply system (2 inverters)
AFCS 3-axis duplex SP-711 Honeywell
-
34
SAR Mission analysis
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.
0
50
100
150
200
250
0 50 100 150 200 250
Sear
ch t
ime
ove
r ar
ea
- m
in
Radius to search area - nm
Mission Weights
Max Gross Weight: 2850 kg
EEW: 1737 kg
Pilot: 85 kg
2 Operators: 85 kg (each)
Rescued person: 85 kg
Fuel Reserve: 40 kg
Flight Assumptions
Temperature: ISA+20C Cruise Altitude: 6000 ft
Loitering: 4000 ft
5 min HOGE for rescuing: 4000 ft
Fuel reserve: 20 min @ 70 kts
Max Range Cruise Speed: 120 kts
-
35
Operational Flexibility
VIP CORPORATE
OFFSHORE
EMS
SAR
AERIAL WORK
LAW ENFORCEMENT
PAX TRANSPORT
-
36
Customer Service and Support
-
37
Regional Offices FSRs
Supply Centers
Service Stations
Headquarter
Back Offices
R&O Centers
24/7 FLEET
OPERATIONS
CENTRE
CUSTOMER SERVICE HEADQUARTER
CUSTOMER SUPPORT &
SERVICES
Innovative Web Services
AW CUSTOMER SUPPORT - LONATE
(ITALY)
AW PHILADELPHIA PHILADELPHIA (USA)
AW DO BRASIL SAO PAOLO (BRAZIL)
AAS LIEGE (BELGIUM)
AW MALAYSIA KUALA LUMPUR (MALAYSIA)
MIDDLE EAST ABU DHABI / DUBAI (UAE)
AW Customer Support & Services
-
38
3 years warranty
2 inspection programs
High overhaul intervals
Customer Service: 24 hr/365 days
Support and Maintenance
-
39
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
Main Components TBO
-
40
More Space Than Any Other Light Single Exceptional Flexibility Superior Performance High Productivity Great Reliability
THE A119 KOALA OFFERS:
Conclusion
-
41