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A flexible and versatile special mission
surveillance platform
DORNIER 228 NEW GENERATION
David A Jones General Manager RUAG Aviation Malaysia September 2013
Aviation Defence Space Technology Ammotec
The RUAG Group
12.09.2013 RUAG Aviation 2 |
7’800 employees
Turnover of ~US$2bn
Operations: Switzerland, Germany, Austria, Hungary, Sweden, Australia, Malaysia
Headquarters: Berne/Switzerland
12.09.2013 RUAG Aviation 3
RUAG Aviation – providing total solutions
Aircraft and Component MRO
Program Management and
Upgrades
Engineering
• Maintenance / System
• Fatigue
• Design
Prototyping / Testing / Qualification
Configuration Management
Supply Chain Management
Publications and Training
Ground Support Systems
RUAG – Extensive MRO Capability
Avionics overhaul Cockpit upgrades Starter Generators
Rescue Hoists Turbine Engines Accessory overhaul
Established calibration capability
Establish starter generator capability
Focus on civil light fixed wing and rotary wing
markets
Government – Police, Fire Service, Coastguard
Other civil rotary wing and fixed wing operators
Military organisations
Develop additional services to meet market need
Offer line support for rescue hoists, spares and tooling
Other component support services under review
Support Dornier Do228NG in region
RUAG Aviation Malaysia
12.09.2013 │RUAG Aviation│ 5
Dornier 228 New Generation
State-of-the-art
Glass Cockpit
Honeywell TPE331-10 Up to 7,000 hrs TBO, FAA STC
New 5-bladed Propeller MT-Propeller
RUAG Aviation 6 |
> 300 other improvements
Dornier 228 New Generation – Prepared for the future!
• Mission Performance
Cover maximum possible area in the minimum of time
Extended endurance (>9 hours). Extended range. High max cruise speed (240 KTAS)
• Maneuverability/Flexibility
Ability to monitor targets with pilot confidence
Low stall speed (67 KTAS). Full aileron control even at high AOA. Higher propeller braking for faster controlled descents
• Engine and Field Performance
Able to perform across differing terrains
Take off from unpaved airfields. Engine flat rated to ISA+30°C/86°F at sea level.
• Efficiency
Aerodynamic, with low fuel burn
Generates high lift with 30% lower drag. Fuel burn less than 200kg / search hour) with lowest CO2 emission in its class
• Cockpit and Communication
Fully integrated cockpit
Important features for a surveillance platform
7 | RUAG Aviation
• Visibility
Full and unobstructed view for pilots and operators
• Reliability
Greater than 99% operational reliability
• Direct Maintenance Cost
Low maintenance manhours per flight hour, high engine TBO
• Ease of integration of Mission Systems
Unpressurised fuselage, good ground clearance, optimal fuselage cross section
• Flight Safety State of the art systems (MMS, TAWS overlay, TCAS, Digital Autopilot…). Instantaneous engine power
response for safer STOL operation
Important features for a surveillance platform
8 | RUAG Aviation
• Renowned short-field performance
• Renowned hot and high performance
• Unprepared airfields
• Excellent handling.
• Proven reliability
• Efficient and productive
• High payload transport
• Only aircraft in production in its
performance class (FAR23 commuter <
19.000lbs)
12.09.2013 RUAG Aviation 9 |
Dornier 228 New Generation Versatile multirole aircraft
Tensing-Hillary Airport (9100 ft) Lukla, Nepal
Unprepared airfield operation, Nigeria
12.09.2013 RUAG Aviation 10 |
Dornier 228 New Generation Mission Endurance
Distance Airfield to Search Area (NM)
Searc
h T
ime (
Ho
urs
)
0 100 200 300 400 500 600 700 800 900
9
8
7
6
5
4
3
2
1
0
Distance Airfield to Search Area (NM)
0 100 200 300 400 500 600 700 800 900
1000
900
800
700
600
500
400
300
200
100
0
Searc
h A
rea 1
000 N
M3
Transit to Search Area
•Field Elevation 250 ft Delta ISA 0°C
•Climb with Best Climb Rate to FL 100
•Max Range Cruise Speed
•Wind 0 Kts, Descent Max Range
Search in the Area
• Delta ISA 0°C
• Search Altitude 4000 ft
• Max Endurance Speed
• Sensor Range (both sides) 40 NM
Transit back from Search Area
• Delta ISA 0°C
• Climb with Best Climb Rate to FL 100
• Max Range Cruise Speed
• Wind 0 Kts, Field Elevation 250 ft
MTOW 6675 kg
OWE 3900 kg
Mis. E. 600 kg
Fuel 2250 kg
0
250
500
750
1000
1250
1500
1750
2000
2250
0 100 200 300 400 500 600 700 800 900 1000 1100 1200 1300 1400
Range (NM)
Pa
ylo
ad
(kg
)
Dornier 228 New Generation DHC6-400
Payload (kg)/Range (NM) – 100% Load Factor (LF), max Range
19 Pax with 93 kg each
(100% LF)
312 120
Payload –Range
Dornier 228 New Generation
Versatility Quick change troop layout
12.09.2013 RUAG Aviation 12 |
Fwd Baggage Compartment
Aft Baggage Compartment
Troopers Lightweight Seat
Roller Door
WX Radar
Ladder Stowage Anchorline Cable
Emergency Exits
Special Operations Platform Multirole layout – 2 Operators, 1 Observer, 1 SAR Operator
12.09.2013 RUAG Aviation 13 |
FWD Baggage Compartment
ATF Baggage Compartment
WX Radar
PBE
Data Master Unit
SLAR
Pax Seat (moveable)
Ladder
Operator Console
Operator Seat
VIS Line Scanner
MWR
Cabin Heater
Roller Door
Oil Spill Sampling Buoy
Pax Seat (moveable)
First Aid Kit Fire Extinguisher
Life
Raft
EO/IR Cabin Heater
Operator Console
Operator Seat
PBE SLAR
Emergency Exits
Special Operations Platform Multirole layout – 1 Operator, 8 Passenger Seats, Toilet
12.09.2013
RUAG Aviation 14 |
FWD Baggage Compartment
ATF Baggage Compartment
WX Radar
Aft facing Pax Seats
Operator Console
Operator Seat
Lavatory
Emergency Exits
Versatility Quick change MedEvac layout (up to 6 double stretchers)
Up to 3 quick change Double Stretchers:
•4 side-facing seats
•3 Pax seats
12.09.2013 RUAG Aviation 15 |
Fwd Baggage Compartment
Aft Baggage Compartment
WX Radar
Stretcher Stretcher
4 Sideways facing folding Seats
Forwards facing PAX Seats Lavatory
Emergency Exits
EO/IR Pointer MWR
IR/UV Scanner
SLAR Antenna
Surveillance Radar
VIS Scanner
Data link
• LOS Data Links
• BLOS Data Links
• TVDL
• ARC-210, ARC-231
• IFF
• P-25 Radios
• ASE
Avionics Systems
• 2nd FMS
• NVG Compatibility
• Mission Display
• Encrypted Comms
• TACAN
Mission Systems
• General Atomics
• SELEX
• ForceX
• Avalex
• MEDUSA
Sensors and Mission Systems
Special Operations Platform
High ground clearance for sensor installation (0.76m)
High wing - excellent down view through bubble window
Electronic library of (land) targets
Moving Target Identification (MTI)
Data recording and data link
Detection/Highlighting of man-made objects
Sensor Management and cross cue capability
Mission Management System (MMS)
Primary Sensor: Synthetic Aperture Radar (SAR)
Secondary Sensor: EO/IR
Other Equipment: Tactical Radio/Nav Aids, NGV
Compatibility, Search Light, Laser
Illuminator
12.09.2013 RUAG Aviation 17 |
Police ISR Requirements
EO / IR Search Radar
• Side Looking Airborne Radar (SLAR)
• 360° Surveillance / Search radar (SAR)
• Forward Looking Infrared (FLIR)
• Electro-Optical / Infrared Camera (EO / IR)
• VIS Line scanner
• UV / IR Scanner equipment
• Video camera
• Laser illuminator, Search light
• MWR microwave radiometer
• Direct / Indirect data links
• AIS Airborne/ELR Receiver
• SatCom
• Tactical radio and navigation aids (e.g.
TACAN, Encrypted Communication)
• Mission management systems
12.09.2013 RUAG Aviation 18 |
Special Operations Platform Sensors and Mission Systems
360° Search Radar
SAR imagery
360° scan or sector scan. Primary sensor for
all search task (except oil spill search)
Max range 200 NM
Small target (periscope, small boats,
life rafts), high sea state range ~ 60 NM
Pulse compression
Moving Target Indication (MTI)
Weight: 35 – 100 kg
Different Suppliers
Search/Surveillance Radar (SAR)
Special Operations Platform
EO / IR
IR / EO imagery
Up to 9 sensors, HD resolution
Typical sensor equipment
Thermal imager
Multi-spectral HD zoom camera
Multi-spectral HD spotter
Laser illuminator, laser pointer
Mission awareness positioning system
Stabilized system, auto-tracking, layover mode
System weight 40 kg to 55 kg
Different Suppliers
Electro Optical / Infrared (EO/IR)
Special Operations Platform
EO / IR
IR / EO imagery
Search Radar
SAR imagery
Cross Cueing capabilities
Workstation sensor calibration
Best identification through combination of
Long range, all weather, broad area radar surveillance (SAR)
Short range, high resolution EO/IR imagery
Cross cueing sensor software available
System weight: 70 – 150 kg
EO/IR + SAR = Optimal Sensor Package
Special Operations Platform
Special Mission Version Delivered
Customer
Air Border Patrol
Coast Guard
Indian Navy
DLR
Finnish Frontier Guard
National Carthogr. Center
Fr Aviation
German Government
Kustwacht
Royal Thai Navy
German Government
Bangladesh Navy
12.09.2013 RUAG Aviation 22 |
Country
Nigeria
India
India
Germany
Finland
Iran
UK
Germany
Netherlands
Thailand
Germany
Bangladesh
A/C
5
20
30
2
2
4
3
2
2
7
2
2
Mission
Air Border Patrol
Maritime Patrol, SAR
Maritime Patrol
Environmental Prot.
Air Border Patrol
Carthography
Fisheries Patrol
Pollution Surveillance
Maritime Patrol, SAR
Maritime Patrol, SAR
Pollution Surveillance
Maritime Patrol
Primary Sensor
FLIR, SLOS Camera
360° Radar
360° Radar
Air Data Sensors
360° Radar, SLAR, FLIR
Zeiss Analog Camera
360° Radar
SLAR, IR/UV
360° Radar, SLAR, FLIR
360° Radar
SLAR, IR/UV
360° Radar
Dornier 228 New Generation
Max. Take-off Weight
Optional (military only)
Max. Landing Weight
optional
Max. Zero Fuel Weight
Operating Weight Empty
Max. Structural Payload
Typical Payload (19 Pax) 93 kg
Fuel at max. Pax
12.09.2013 RUAG Aerospace Services GmbH 24 |
lb
14,109
14,550
13,448
14,109
13,095
8,816
4,279
3,895
1,464
kg
6,400
6,575
6,100
6,400
5,940
3,999
1,941
1,767
664
6.29 m
(20 ft 8 in) 16.56 m
(54 ft 4 in)
16.97 m
(55 ft 8 in)
3.30 m
(10 ft 10 in)
2.54 m (8 ft 4 in)
1.17 m (4 ft 2 in)
• Four (4) 8.9 inch liquid crystal HD
displays
• Navigation display with TAWS overlay,
• Special Mission Operations FMS
available
• Avionic system modifiable. Interface
between mission system and cockpit
avionic possible
• Charts and airport diagrams (optional)
• Checklist (optional)
• Moving Map (optional)
Designed for increased situational
and flight safety awareness
12.09.2013 RUAG Aviation 25 |
Dornier 228 New Generation 4-tube Universal glass cockpit
Avionics
• EFIS: 2 each PFD’s and MFD’s
• FMS
• ESIS
• TAWS*, TCAS*
• Weather Radar*
• Autopilot*
• HF Radio*
• MMS *
* optional
Dornier 228 New Generation
Engine
Performance
Cabin
12.09.2013 RUAG Aerospace Services GmbH 26 |
671 m
793 m
747 m
450 m
1,870 ft/min
440 ft/min
444 km/h
833 km
7.08 m
1.55 m
2,200 ft
2,600 ft
2,450 ft
1,480 ft
240 KTAS
450 NM
23.23 ft
5.09 ft
Garrett TPE 331-10GP-511D 2 x 776 SHP
(flat rated to ISA + 15°C/59°F) Cruise Fuel Flow 252 lb/h/engine
Take-off Run (1-engine)*
Take-off Distance (1-engine)*
Acc. Stop Distance*
Landing Distance**
Climb, 2 engines*
Climb, 1 engine*
Max. Cruise Speed (10,000 ft)*
Range (Max. Cruise Speed)***
Length
Height
* Max. Take-off Weight, ISA, Sea Level ** Max. Landing Weight, ISA, Sea Level
*** 19 Pax, 85 kg/187 lbs each, 45 min hold, ISA, 10,000 ft; alternate 100 nm
Market potential
Description
Baseline ISR
1.Higher growth
2.Lower growth rate
3.Competition
4.Downside scenario
Baseline Commuter
2.1 Shrinking market
2.2 Competition
12.09.2013 RUAG Aerospace Services GmbH 27 |
Generic market
997
1108
790
997
790
500
275
500
Dornier 228NG Share
19.8% = 197
19.8% = 219
19.8% = 156
16.6% = 166
16.6% = 131
21% = 105
21% = 58
18% = 92
Probability
High
Medium
Medium
Medium
Low
High
Low
Medium
Mean Time Between In-Flight Shutdown
(MTBIFSD)
12.09.2013 RUAG Aerospace Services GmbH 28 |
Dornier 228 New Generation Honeywell TPE331 – Reliability
MT
BIF
SD
rate
per
1,0
00 h
our
0.0200
0.0150
0.0100
0.0050
0.0000
Jan-0
9
Feb-0
9
Mar-
09
Apr-
09
May-
09
Jun-0
9
Jul-09
Aug-0
9
Sep-0
9
Oct-
09
Nov-0
9
Dec-0
9
Jan-1
0
Feb-1
0
Mar-
10
Apr-
10
May-
10
Jun-1
0
Jul-10
Aug-1
0
Sep-1
0
Oct-
10
Nov-1
0
Dec-1
0
Goal = .01 events per 1.000 fleet hours (ie. 100.000 hours MTBIFSD)
MTBIFSD rate = 0.0 (> 658.578 hours) MT
BIF
SD
rate
per
1,0
00 h
our
0.0200
0.0150
0.0100
0.0050
0.0000
Jan-0
9
Feb-0
9
Mar-
09
Apr-
09
May-
09
Jun-0
9
Jul-09
Aug-0
9
Sep-0
9
Oct-
09
Nov-0
9
Dec-0
9
Jan-1
0
Feb-1
0
Mar-
10
Apr-
10
May-
10
Jun-1
0
Jul-10
Aug-1
0
Sep-1
0
Oct-
10
Nov-1
0
Dec-1
0
Goal = .01 events per 1.000 fleet hours (ie. 100.000 hours MTBIFSD)
MTBF rate = 0.14 (> 73.175 hours)
Mean Time Between Failure
(MTBF)
www.ruag.com
P.O. BOX 1253
82231 Wessling
Germany
© RUAG Aerospace Services GmbH 2012
ALL RIGHTS RESERVED
This document and all information contained herein is the sole property of RUAG Aerospace Services GmbH.
No intellectual property rights are granted by the delivery of this document or disclosure of its content.
This document shall not be reproduced or disclosed to a third party without the express prior written consent
of RUAG Aerospace Services GmbH.
This document and its content shall not be used for any other purpose other than for which it is supplied.
The statements made herein do not constitute an offer. They are based on the assumptions shown and are expressed in good faith.
Where the supporting grounds for these statements are not shown,
RUAG Aerospace Services GmbH will be pleased to explain the basis thereof.
Printed in Germany