Dornier 228 Multirole (MR) Facts & Figures

Transcription

1 Dornier 228 Multirole (MR) Facts & Figures

2 Overview Specifications Page 20 Performance Page 22 Missions Page 4 Contents Page 48 Operations Support Page 46 Sensors and Mission Systems Page 36 2 Facts & Figures

3 Certification Basis Page 23 Construction and Fuselage Page 24 Main Wing Page 26 Engines and Propellers Page 28 Glass Cockpit Page 30 Facts & Figures 3

4 Missions Mission Challenges The Dornier 228 is the platform of choice for special mission operations taking place between low level and 10,000 ft. Military and government law enforcement organisations operate the Dornier 228 worldwide for maritime patrol (pollution control, search and rescue, border control, fishery patrol), research flights, surveillance and reconnaissance, and light transport operations (cargo, paratrooper, passenger, medevac). Maritime Patrol A challenging environment Discharge and spill of oil from ships, especially tankers Increased demand in Search and Rescue (SAR) High economic damages caused by piracy (4.9 to 8.3 billion US$ in 2010) Continuously increasing illegal immigration due to political and social instability Enforcement of international Individual Fishing Quotas (IFQs) Environmental & Pollution Control SAR Law Enforcement/Border Control FIsheries Monitoring 4 Facts & Figures

5 Light Transport A challenging environment Increase demand in MedEvac operations A wide range of runway surfaces (remote airstrips) Famine Providing food to people in hard-to-access regions An increasing number of global catastrophes Disease control Water scarcity Cargo Paratrooper Passenger MedEvac Facts & Figures 5

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7 Missions Multirole Platform The Dornier 228 is the most advanced aircraft in its class, offering unsurpassed effectiveness and efficiency with superb versatility. This is why authorities all over the world count on it when it comes to demanding special missions of various kinds. Key features are the long range, high utilization rates and high payload and all this at impressively low operational costs. With the aircraft s state-of-the-art technology, pilots are able to maintain superior situational awareness throughout the most demanding missions. No other plane in this category combines safety and efficiency to the level offered by the Dornier 228. Best platform in its class Operational advantages Speed performance: high speed cruise and range of operating speeds Endurance: up to 10 hours loitering Range: well in excess of 1000 Nm with a significant payload Productivity and flexibility: largest payload/range envelope Economic advantages Lowest fuel consumption per Nm Lowest operating cost per Nm Mission advantages Equipment installation flexibility large square cabin cross-section UNIVERSAL military grade avionics Payload advantages PAX space/seating comfort in individual seats Cargo transportation volume and loading Cargo/PAX versatility Quick swap cargo door Facts & Figures 7

8 Missions Mission Match All Around the World Central Command for Maritime Emergencies Germany The Dornier 228 is used as a mission aircraft for pollution control in the North and Baltic Sea on a daily basis. For this task the aircraft fulfills all requirements for low level flights and long endurance over sea. Hans-Werner Monsees, Head of CCME, Cuxhaven Finnish Border Guard The aircraft s performance and mission equipment enables us to provide reliable, accurate and real time maritime situational awareness to maintaining border and maritime security, and fighting against illegal immigration as well as maritime pollution. Colonel Antti Pesari, Commander, Air Patrol Squadron, Finnish Border Guard Royal Thai Navy The Dornier 228 complies with our squadron slogan All Day, all Night, all Purpose as we are convinced by its capabilities and easy maintenance. And it is economical to operate. Every day it is a pleasure to work and fly with it. CDR Sanit Kongpetch, Commander of Squadron101, Wing1, Naval Air Division, Royal Thai Fleet 8 Facts & Figures

9 Italian Army Aviation Owing to their versatility and their STOL capability the Dornier 228 have been employed for different tasks (passenger transport, cargo) in different environments, including the training of the Italian Army paratroopers unit. Lieutenant Colonel Stefano Lagorio, Commander 28 Gr. Sq. AV. ES. Tucano Lufttransport AS Norway Our Dornier 228 has been specially equipped for passenger transport in the arctic climate of Svalbard. It has already proven that it was the right choice for operations under such harsh conditions. Stig Naesh, Managing Director, Lufttransport AS, Longyearbyen, Svalbard, Norway DLR Research Flight Facility Atmospheric science and earth observation are the main activities of the DLR research flight facility in Oberpfaffenhofen. The Dornier 228 has been specifically chosen for operations using radar, multispectral and camera instrumentations. Dr. Monika Krautstrunk, Head of Research Flight Facility Oberpfaffenhofen Facts & Figures 9

10 Missions Maritime Patrol The Dornier 228 in customized maritime patrol configuration is the most suitable and economical solution for your mission. The Dornier 228 ergonomics, outstanding field of view, and comfortable environment substantially reduce crew fatigue and workload, thus a high level of vigilance is maintained throughout low level operations and long missions. Our aerodynamic expertise and system integration experience will ensure a seamless integration of your choice of sensors and mission systems, and make the Dornier 228 as cost effective as it gets. Maritime Patrol Mission Profile 10 Facts & Figures

11 Performance features 8+ hours loitering on station with wing tanks For crew safety, no fuel tanks fitted in the cabin 223 KIAS cruise speed to the area of interest High manoeuvrability (fighter like roll rate) Less than 440 lbs total fuel burn per search hour Transport Category OEI take-off performance Bubble window Platform features Wide range of possible sensors Easy sensor installation/integration on the rectangular fuselage and flat bottom Large rectangular cabin cross-section that can accommodate all types of consoles Large roller door, openable in-flight On board toilet Air-conditioning system High ground clearance for sensor installation (0.76 m, 29 inch) 600 A of electrical power Multi-Mission Management System (MMMS) for FMS with search pattern and tactical waypoints Mission Management System duplex communication capability with operator s console Night Vision Goggle (NVG) capable cockpit (optional) Position and size of bubble window for full downward looking view (180 view) Retractable gear offering unobstructed 360 radar scan in flight High wing excellent down view Facts & Figures 11

12 Missions Maritime Patrol Maritime Patrol layout 2 Operators, 1 Observer, 1 SAR Operator 0.89 m 3 31 cuft (120 kg, 255 lb) 14.7 m cuft 1.2 m 3 42 cuft (150 kg, 330 lb) Wx Radar SLAR Operator Console PBE Operator Seat Cabin Heater FLIR First Aid Kit Pax Seat (moveable) Fire Extinguisher Life Raft FWD Baggage Compartment PBE Data Master Unit SLAR Pax Seat (moveable) Ladder Operator Console Operator Cabin Seat Heater Roller Door AFT Baggage Compartment Oil Spill Sampling Buoy Maritime Patrol layout 1 Operator, 8 Passenger Seats, Toilet 0.89 m 3 31 cuft (120 kg, 255 lb) 14.7 m cuft 1.2 m 3 42 cuft (150 kg, 330 lb) Wx Radar Lavatory FWD Baggage Compartment Aft facing Pax Seats Not be used during takeoff and landing Operator Console Operator Seat AFT Baggage Compartment Emergency Exits Baggage compartment Cabin 12 Facts & Figures

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14 Missions Light Transport The Dornier 228 is «flying flexibility». The aircraft can be quickly re-configured from passenger to cargo transportation layout with minimum personnel. Aircraft & performance features Renown short-field performance Renown hot and high performance Unprepared airfield operations Simple single point refueling in 10 min Pax/cargo door swap in 15 seconds Pax to cargo configuration change in about 1h by one person Cargo door Pax door Unprepared airfield operation, Nigeria Tensing-Hillary Airport (9100 ft), Lukla, Nepal 14 Facts & Figures

15 PAX A high standard of passenger comfort is the primary consideration in the Dornier 228 design. The standard cabin consists of 19 individual passenger seats with 30-in pitch and offers airline standard passenger comfort in single seat configuration. Its rectangular cross-section is the ideal shape for utility applications and provides passengers with ample space at shoulder height, extra passenger headroom and cargo storage. Passengers enter through a passenger door with built-in steps on the LH side of the rear fuselage. An 18 seats layout, with a toilet located aft of the cabin, is also available. PAX layout 19 passenger seats 0.89 m 3 31 cuft (120 kg, 255 lb) 14.7 m cuft 2.6 m 3 92 cuft (210 kg, 460 lb) FWD Baggage Compartment AFT Baggage Compartment PAX layout 18 passenger seats, toilet 0.89 m 3 31 cuft (120 kg, 255 lb) 14.7 m cuft 1.2 m 3 42 cuft (150 kg, 330 lb) FWD Baggage Compartment AFT Baggage Compartment Emergency Exits Baggage compartment Cabin Facts & Figures 15

16 Missions Light Transport Cargo Seats can be quickly removed to convert the cabin for cargo transportation; to ease loading the normal passenger door can be opened sideways, which together with the adjacent door, creates a massive opening for bulky or heavy cargo. Parcels and crates of all sorts can be distributed quickly and easily inside the cabin by means of the integrated roller system. While smaller and lighter cargo items can be secured with nets, bulky and heavier cargo stacked on pallets can be locked on the seat rails. The rectangular cabin with its 23 ft of usable length significantly eases the transportation of bulky cargo or longer goods. Whatever your cargo may be, a total of 2 tons (512 cu ft) can be transported Payload [kg] Max Cruise Speed Long Range Speed Range [NM] Cargo layout Wx Radar 0.89 m 3 31 cuft (120 kg, 255 lb) 14.7 m cuft 2.6 m 3 92 cuft (210 kg, 460 lb) FWD Baggage Compartment AFT Baggage Compartment Emergency Exits Baggage compartment Cabin 16 Facts & Figures

17 MedEvac The ambulance equipment has been designed to cover different mission aspects. The complete equipment is sectionalized in separate specific modules, which enable quick change, if required, to support the multi purpose operation of the Dornier 228. In accordance with MedEvac hygienic requirements, the cabin roof and walls of the Dornier 228 are covered with a polycarbonate lining with a washable surface and can be easily sanitised. The cabin floor is covered with a special washable, anti-skid coating to protect the aircraft s lower structure against contamination by fluids. The cabin can be equipped with various combinations of forward and side facing seats and double stretcher as well as intensive care stations. The ambulance transport layout may be easily combined with trooper and paratrooper transport layouts. MedEvac layout 0.89 m 3 31 cuft (120 kg, 255 lb) 14.7 m cuft 1.2 m 3 42 cuft (150 kg, 330 lb) Wx Radar 4 Sideways facing folding Seats Not to be used during takeoff and landing Forwards facing PAX Seats Used during takeoff and landing Lavatory FWD Baggage Compartment Stretcher Stretcher AFT Baggage Compartment Emergency Exits Baggage compartment Cabin Facts & Figures 17

18 Missions Light Transport Paratrooper In this configuration 21 paratroopers and 1 jumpmaster can be transported (limited to 19 parachutists when operated under civil registration). The paratrooper version is easily changeable to the trooper version by removing the anchor line cable and jump master equipment. The paratrooper version is characterized by the following equipment: Side facing, lightweight fold-up troop seats Roller door with ladder Anchor line cable Side wall protection Paratrooper layout (21 Paratroopers, 1 Jumpmaster) 0.89 m 3 31 cuft (120 kg, 255 lb) 14.7 m cuft 2.6 m 3 92 cuft (210 kg, 460 lb) Wx Radar Ladder Stowage Anchorline Cable FWD Baggage Compartment AFT Baggage Compartment Troopers Lightweight Seat Roller Door Emergency Exits Baggage compartment Cabin 18 Facts & Figures

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20 Aircraft Specifications Dimensions 2.54 m (8 ft 4 inch) 3,30 m (10 ft 10 inch) m (55 ft 8 inch) 1.17 m (4 ft 2 inch) 4.86 m (15 ft 11 inch) m (54 ft 4 inch) 6.29 m (20 ft 8 inch) 1.32 m (4 ft 4 inch) 7.08 m (23 ft 6 inch) 1.85 m (6 ft 1 inch) 5ft 1 in 1,55 m 0.89 m 3 31 cuft (120 kg, 255 Ib) 14.7 m cuft 2.6 m 3 92 cuft (210 kg, 460 Ib) Baggage Compartment Cabin 12 in 0,35 53 in / 1,35 m 19.8 in 0,502 m 20 Facts & Figures

21 Principal dimensions Overall height 15 ft 11 in (4.86 m) Overall length 54 ft 4 in (16.56 m) Wing Span 55 ft 8 in (16.97 m) Area ft 2 (32.00 m 2 ) Aspect ratio 9.0 Taper ratio 0.7 Sweepback of leading edge inboard 0 /outboard 8 Vertical stabilizer Height 8 ft 10 in (2.70 m) Area 64.6 ft 2 (6.0 m 2 ) Aspect ratio 1.50 Taper ratio 0.46 Rudder area 16.1 ft 2 (1.5 m 2 ) Rudder deflection -24 /+24 Passenger compartment Overall length, max. 23 ft 3 in (7.08 m) Maximum width 4 ft 4 in (1.328 m) Maximum height 5 ft 1 in (1.55 m) Weights Horizontal stabilizer Span 21 ft 2 in (6.45 m) Area 89.6 ft 2 (8.33 m 2 ) Aspect ratio 5.00 Taper ratio 1.00 Elevator deflection -30 /+25 Ailerons Span 8 ft 10 in (2.69 m) Area ft 2 ( m 2 ) Deflection (Flaps 0 ) 25 up / 18 down Chord 30% Doors (height width) Cockpit door 2 ft 9 in 2 ft 2 in (0.84 m 0.65 m) Passenger airstair door 4 ft 5 in 2 ft 1 in (1.34 m 0.64 m) Passenger/cargo door 4 ft 5 in 4 ft 2 in (both door panels are open) (1.34 m 1.28 m) Baggage door (front) 3 ft 11 in 1 ft 8 in (1.2 m 0.5 m) Baggage door (rear) 2 ft 11 in 1 ft 9 in (0.89 m 0.53 m) Emergency exits (3) 2 ft 2 in 1 ft 7 in (0.67 m 0.48 m) Weights lb kg Max. take-off weight (MTOW*) 14,110 6,400 Max. landing weight 13,448 6,100 Max. zero fuel weight (MZFM) 13,095 5,940 Operating weight empty (with 2 Pilots) (OWE) 8,598 3,900 Mission equipment (incl. operator and console) 1, Max. fuel 4,156 1,885 * e.g. optional MTOW increase to 6,575 kg (14,550 lbs) possible Facts & Figures 21

22 Aircraft Performance With its Transport Category OEI field performance, control and engine responsiveness and wide range of operational speeds (74 to 223 KIAS), the Dornier 228 ensures safe margins throughout the entire mission envelope. Range of take-off distance ft at MTOW, ISA, SL ft at MTOW, ISA+10 C, 2000 ft elevation ft at MTOW, ISA+20 C, 4000 ft elevation Accelerate stop distance range ft at MTOW, ISA at SL ft at MTOW, ISA+10 C at 2000 ft elevation ft at MTOW, ISA+20 C at 4000 ft elevation Range of unfactored landing distance ft at MLW, ISA at SL ft at MLW, ISA+10 C at 2000 ft elevation ft atmlw, ISA+20 C at 4000 ft elevation Climb at ISA, SL conditions normal 1570 ft/min single engine 400 ft/min Speed max. cruise 223 KIAS minimum control 74 KIAS 22 Facts & Figures

23 Certification Basis The Dornier 228 is the only 3rd-generation aircraft in its class. It has been purposely designed to match the FAR23/CS23 commuter category airworthiness standard, which assigns safety margin equivalents to transport category aircraft. Its advanced design provides the Dornier 228 with unmatched performance, payload capacity, operational flexibility and efficiency. The Dornier 228 success is proven by the over four million hours flown to date. Based on continuous improvements and innovations, the Dornier 228 offers a high level of safety, even in its standard version, and is one of the most reliable aircraft in the world with its perfect mix of a mature design and innovative technologies. Due to its advanced aerodynamics, the Dornier 228 is able to match or exceed the STOL performance of competing aircraft at the same payload, all while cruising up to 50 kts faster. Facts & Figures 23

24 Aircraft Construction and Fuselage The structure of the fuselage is a conventional alloy construction (non-pressurized fuselage). The structure of the wing is new technology. While a conventional wing has a main and a secondary spar, ribs and stringers and sheet metal skin rivited together the Dornier 228 wing structure is a box formed from four integrally milled alloy panels. Leading edge is conventional alloy sheet metal with ribs and stringers, trailing edge and Fowler Flaps are made from Kevlar. Empenage is conventional alloy construction Aerodynamic cowlings (e.g. landing gear) are Kevlar Conventional frame/stringer/sheet metal construction with 4 seat rails (Douglas 1 inch) Cables and air condition tubing installed Emergency exits (front right and centre left) Electronic racks 24 Facts & Figures

25 Key advantages Square cross-section and volume Allow for large operator console(s) and still guarantee safe egress path Floor structure offering several spot for sensors installation without a need for structural reinforcements Flat bottom and side for easy sensors integration and low fuselage interference Retractable gear allowing for unobstructed 360 radar scan Aft cargo area configurable and accessible in flight (drop-hole possible) 30 second quick change pax/cargo door Roller door, capable of in-flight operation (optional) Facts & Figures 25

26 Aircraft Main Wing Airfoil specification The outstanding wing design is the key element behind the Dornier 228 best-in-class performance. The supercritical profile Do A-5 reduces drag by up to 30%, retains good characteristics in icing conditions, and ensures roll control even in full stalls The optimised wing shape keeps secondary drag as low as possible (reduced wing vortex by triangular shape of wing tips) The box type structure and the manufacturing process ensure the highest possible accuracy over the life cycle Wings of excellence: the Wing of New Technology The high performance wing of the D228 was developed by Dornier as part of the Wing of New Technology for General Aviation Aircraft programme funded by the German Federal Ministry of Education and Research. The objective of this program was to improve the performance and efficiency of general aviation aircraft at speeds of up to 250 KTAS. The Dornier 228 wing stems directly from this research program, the most radical evolutions being: Supercritical profile designed specifically for this aircraft (50% laminar flow) Trapezoidal wing with raked wing tips for enhanced pressure distribution and reduced vortex drag Integral milled wing panel for structural performance and reduced parasite drag Performance with the Wing of New Technology was increased by more than 25% overall. Another reason for the better performance is the Fowler Flaps, which ensure an improved take-off and landing performance. Finally, the triangular wing tips ensure a reduction in induced drag and gentle stalling characteristics. Cruise Improvement Climb Improvement Climb Cruise Lift Drag Do A-5 NACA GA (W)-1 26 Facts & Figures

27 The high wing design make the aircraft less prone to FOD and stone damage when operating on unprepared runways. The wing box, panels and root ribs are integrally milled and serve as the integrated fuel tank. While conventional sheet metal construction is used for the leading edge part, glass-fiber reinforced plastic is used for the trailing edge, outboard wing and wing tips. Do A-5 supercritical profile, more than 50% laminar flow upper panel Kevlar trailing edge front spar panel front wing box fuel tank panel rear rear spar conventional alloy leading edge lower panel Fowler Flaps Facts & Figures 27

28 Aircraft Engines and Propellers The Dornier 228 is currently the most productive, most reliable and most up-to-date aircraft in its class. And this unmatched performance has even been significantly improved by the new 5-bladed propeller in combination with the fuel-efficient TPE engine. The results are unique and outstanding mission performances and improvements over the whole flight profile. Our complete support of the Dornier 228 includes the competence required for the regular MRO, certified safety and continued support of the TPE331 engine over its entire life cycle. RUAG is your experienced partner of choice as a Honeywell Authorised Service Centre and we invest our expertise in providing full support for TPE331-5 & -10 engines, offering both line and major maintenance, as well as hot section inspection. Engine data TPE Dimensions (mm) (length width height) (in) Weight 385 lb Pressure Ratio Power 940 shp Compressor bleed (max.) 10% TBO (commercial operation min 800 h/year) 7,000 h ESFC (Equiv. Specific Fuel Consumption T/O) lb/hp-h N.T.S. Negative Torque Sensing (N.T.S.) provides automatic and instantaneous prop drag reduction Power N.T.S. 28 Facts & Figures

29 TPE331 Engine Benefits Low Specific Fuel Consumption (SFC) Efficient front-to-rear-flow turbine design Very high ram pressure recovery Low frontal area reducing drag to a minimum Instantaneous power response in all flight modes Automatic torque and ITT limiting system Automatic start sequence Simple Engine Anti-Ice System 940 SHP de-rated to 776 SHP Flat rated up to ISA + 30 C at SL Low Direct Maintenance Cost Time between overhaul up to 7,000 hours Engine Health Monitoring (optional) 5-bladed Composite Propeller Lighter propeller: Reduced stress on the engine and electrical system during start up Smaller propeller diameter: Reduced noise and increased ground clearance Retrofit ready: EASA STC A.S.02755, MT-Propeller Facts & Figures 29

30 Cockpit Glass Cockpit The cockpit is fitted with 4 large UNIVERSAL displays, featuring one Primary Flight Display (PFD) and one Multi Function Display (MFD) in front of each crew member located on the central panel, additionally an Electronic Standby Instrument System (ESIS) is installed between the two MFD. Those crystal clear, sunlight readable HD displays provide the pilots with the specific information required during each phase of the mission. Key features Four (4) 8.9 inch liquid crystal HD displays Designed for increased situational and flight safety awareness Primary Flight Display (PFD) with multiple display setting to match mission segment requirements Navigation display with TAWS overlay, Terrain cross-section analysis along flight path Multi-sensors FMS with LPV Monitor Duplex communication capability between FMS and operator s consoles Emergency ESIS with navigation capability Charts and airport diagrams (optional) Checklist (optional) Moving Map (optional) Native NVG PFD/MFD display available (not add-on filters) Obstacle cross-section view along flight path Synthetic vision (optional) 30 Facts & Figures

31 NG-SAMM USE FLAP POSITION 1 OR UP IF FROST, ICE, SLUSH, MUD OR STRUCTURAL DAMAGE IS SUSPECTED ON THE HORIZONTAL STABILIZER. INCREASE V REFBY 15 KIAS MINIMUM FUEL T.O.: 200 LBS EACH FEEDER TANK OPEARATIONAL LIMITS THE MARKINGS AND PLACARDS INSTALLED IN THIS AIRPLANE CONTAIN OPERATING LIMITATIONS WHICH MUST BE COMPLIED WITH WHEN OPER- ATING THIS AIRPLANE IN THE COMMUTER CAT- EGORY. OTHER OPERATING LIMITATIONS WHICH MUST BE COMPLIED WITH WHEN OPERATING THIS AIRPLANE IN THIS CATEGORY ARE CONTAINED IN THE PILOTS OPERATING HANDBOOK AND LBA APPROVED AIPLANE FLIGHT MANUAL. MAX. DESIGN MANEUVERING SPEED 150 KIAS MAX. LOADING GEAR OPERATING SPEED 160 KIAS THIS AIRPLANE IS APPROVED FOR VFR, IFR, DAY AND NIGHT OPERATIONS. FLIGHTS UNDER KNOWN ICING CONDITIONS ARE APPROVED IF ICE PROTECTION EQUIPMENT IS INSTALLED. ALTERNATE SOURCE STATIC PRESSURE SELECTOR VALVE TEST MASTER MASTER CAUTION WARNING RESET RESET OFF MAX EGT LIMITS C ENGINE START 770 C MAXIMUM REVERSE 565 C 100% 96% RPM OAT RPM WITH ICE BUILD-UP ON THE WINGS RSD AND STALL WARNING ARE UNRELIABLE UNIVERSAL TEST ANTI LRN SKID OFF TFC TERR EXT WX UNIVERSAL CRS HDG CRS POWER MAX P O FI GI REVERSE AIL-TRIM LAMP TEST LH RH BYPASS ON TEST AVIONICS MSTR ON THE SYNCHROPHASER MUST BE OFF FOR T.O. SINGLE ENGINE OPERATION, AND LANDINGS. NWS P AR K BR SYNCHRO PHASER ON OFF FIRE EXT. TEST LH SELECT HYDRAULIC MAN ON NORM OFF RA/DA NOSE LEFT RIGHT LDG GEAR UP FIRE PULL DN LCK REL TFC TERR WX OFF VHF1 HOT ON OFF FDS/ AP ON OFF STBY BATT ON TURN FOR SHOT ENGINE SPEED HIGH L O W S H FEATHER UP 1 2 ON OFF TST MSS MSTR ON FLAPS OFF DN MUTE HORH TEST UNIVERSAL TRQ LIMIT TEST TEST ON ON OFF OFF UP 1 2 ON UNIVERSAL SPEED N G FIRE PULL TURN FOR SHOT TEST BLEEDAIR AIRCOND CKP-HEAT ON ON HIGH ON ON N O R M OFF OFF RAM OFF OFF AIR LH RH I AUTO MAN HOT OFF I COLD C AUTO TEMP MAN SELECT MODE CONTR COLD ALERT FT/M HOT DATA NAV VNAV DTO LIST PREV FUEL FPL PERF TUNE MENU NEXT CAUTION: DO NOT OPERATE ANY BRAKE DURING TOWING FIRE EXT. TEST RH UNIVERSAL RA/DA TFC TERR WX EMER EMER ACTV BRT PREV NEXT EMER EMER ACTV BRT PREV NEXT TOP PRE SET TOP PRE SET BACK 0 MSG ON/OFF DIM ENTER XTUNE DETAIL XTUNE DETAIL ID DME HOLD ID DME HOLD TFC NO ACROBATIC MANEUVERS, INCLUDING SPINS, APPROVED FLAP OVRD TERR EXT WX E R M E E L R P E G. U A L L S D L E N G TEST MASTER WARNING RESET MASTER CAUTION RESET Main Instrument Panel DORNIER SLOW FAST STALL PFD Pilot MFD 1 MFD 2 PFD Copilot C D P K E N P M E U S M 4 TI AT A I R 5 NG-SAMM ELT Control Panel 2. Pilot and Co-pilot PFD Control Unit 3. Pilot and Co-pilot MFD and WXR Control Unit 4. DF Control and Display Unit 5. Air Conditioning Control Panel 6. Landing Gear Lever W ER C R U IS E 7. Pilot and Co-pilot Clock 8. Pilot and Co-pilot Master Warning Master Caution Annunciator / Buttons A B C D E F G Pilot and Co-pilot NAV and Annunciator Panel H I J K L M N O P Q R S T U V W X Y Z 10. Engine Fire Handles 11. Emergency ESIS U T O FF PHASE NG-SAMM Facts & Figures 31 NG-SAMM

32 Cockpit Avionics Navigation and Pitot Static Systems UNIVERSAL UNS-1Ew Flight Management System (FMS) Multi-Mission Management System Software upgrade (optional) Dual Revue Thommen Air Data Computer Dual Northrop Grumman Litef Attitude Heading Reference System Rockwell Collins Radar Altimeter Rockwell Collins Distance Measuring Equipment Dual Rockwell Collins VHF Navigation System ACSS Transponder System Honeywell Weather Radar (optional) Universal Avionics Terrain Awareness and Warning System Class A (TAWS, optional) ACSS Airborne Collision Avoidance System (TCAS, optional) Flight Director/Autopilot (optional) L3-Com Airborne TACAN System (optional) Indicating Systems Universal Avionics Electronic Flight Instrument System L-3 Com Avionics Electronic Standby Instrument Systems Dual AEE Analog-Digital Converting System (EIU) AEE Central Advisory and Warning System Recording Systems L3-Com Solid State Flight Data Recorder with Flight Data Aquisition Unit (optional) L3-Com Solid State Cockpit Voice Recorder (optional) Emergency Equipment Emergency Locator Transmitter 32 Facts & Figures TAWS A unique 3-D perspective view provides the optimum level of situational awareness.

33 Communication Systems Dual Rockwell Collins VHF Communication System two independent VHF COM transceivers and antennas Digital Becker Avionics Intercommunication System two audio control units installed in the center pedestal and one remote electronic unit provides communication between pilot, co-pilot, operator and observers and monitoring of all COM and NAV radio equipment. Dual Universal Avionics Radio Control Units RCU two radio control units installed in the center pedestal primary means of control for all onboard radios without a dedicated control unit Rockwell Collins V/UHF Communications System (optional) accommodates full range of ECCM (el. counter-countermeasures) waveforms Marine Band Radio (optional) Maritime VHF transceiver to provide the MPA with maritime communication in the VHF FM band and on the Distress and Safety Channel (DSC) HF Communication System (optional) long range communication and data transmission inverted-v antenna between top of fuselage tail section and vertical stabilizer SELCAL Decoder (optional) allows an aircraft crew to be notified of incoming communications even when the aircraft s radio has been muted SATCOM (optional) provides secure video, data, voice and IP Facts & Figures 33

34 Cockpit Multi-Missions Management System (MMMS) Search Pattern The MMMS generates and steers the aircraft through the following six pattern types: Rising Ladder The Rising Ladder search pattern consists of an alternating series of parallel legs adjoined with flyover waypoints. Race Track The Race Track pattern consists of two parallel legs. Expanding Square The Expanding Square search pattern consists of a series of legs flow with conventional turn anticipation. 34 Facts & Figures

35 Sector Search The Sector Search pattern resembles a cloverleaf and consists of a series of legs which pass through a centre waypoint. Orbit The Orbit search pattern consists of flying a constant radius circle in a predefined direction around a point. Border Patrol The Border Patrol pattern consists of flying a track between pilot-defined waypoints, or stored route, with course reversal at the final waypoints. Facts & Figures 35

36 Sensors and Mission Systems Overview MMS and Operator Console MWR UV/IR Scanner SAR/DF 36 Facts & Figures

37 MMMS AIS VIS Line Scanner Search/Surveillance Radar SLAR EO/IR Facts & Figures 37

38 Sensors and Mission Systems Mission adaptable Side Looking Airborne Radar (SLAR) Perpendicular beams (090/270) High resolution wave returns = sea clutter (if sea clutter is visible oil spills can be detected) Changes in waves are clearly visible (oil covered water, ship waves) Oil spill area can be measured All weather, day & night High sea state Range right and left 20/40 Nm Measurement of layer thickness not possible SLAR Primary sensor for detection of oil spills Search/Surveillance Radar 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: kg ( lbs) Different suppliers 38 Facts & Figures

39 SAR Direction Finder (SAR/DF) The SAR Direction Finder combines a communication direction finder and a SAR (Search and Rescue) direction finder, thus allowing to track all coastal and maritime radio stations. The SAR Direction Finder allows the bearing of radio signals on different frequency bands as well as their traditional emergency frequencies in the VHF and UHF range, the common calling up channel 16 in the maritime radio band and the widely used Cospas-Sarsat emergency signal. Automatic Identification System (AIS) Monitoring of Surface Traffic; keeps track of AIS equipped vessels and their destinations. Maritime Surveillance/Coast Guard Patrol; together with a radar system, aircraft can find vessels without AIS or faulty AIS parameters. Search and Rescue (SAR); helps locate vessels in distress and communicate help is on the way Mission Control and Coordination; in SAR and military operations involving several helicopters and vessels Facts & Figures 39

40 Sensors and Mission Systems Electro Optical / Infrared (EO/IR) 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: kg ( lbs) Different suppliers EO/IR + SAR = Optimal Sensor Package 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: kg ( lbs) 40 Facts & Figures

41 Visible (VIS) Line Scanner This passive sensor in the visible wave length range is used as an auxiliary tool for various applications. In maritime surveillance: it can detect oil spills, chemical plumes and biogenic slicks (daylight only) Weight: 17 kg (37 lbs) Optimare VIS Scanner Facts & Figures 41

42 Sensors and Mission Systems Ultraviolet / Infrared (UV/IR) Scanner Ultraviolet scanner makes different reflections of water and oil spill visible (daylight only) Infrared scanner makes different surface temperature of water and oil spill (less emissivity) visible (day and night) System weight: 29 kg (64 lbs) Both sensors allow measurements of oil spill thickness > 0.01 µm Optimare UV/IR Scanner 42 Facts & Figures

43 Microwave Radiometer (MWR) This passive sensor measures oil spill thickness > 0.05 mm and < 3 mm by measuring microwave reflection and emission (all weather, day and night). System weight: 115 kg (253 lbs) Optimare Microwave Radiometer Facts & Figures 43

44 Sensors and Mission Systems Mission Management System The Mission Management System is one of the most important elements of any Maritime Patrol Aircraft and the true brain of the platform where all the sensors data are fused together and analysed in real time. As an independent system provider, RUAG is able to flexibly cater to customer requests, integrate the requested Mission Management System and console into the Dornier 228 and work together with the system and sensor providers. Key features Software and sensors form a unified presentation to the operator. Sensor data, maps and reports are presented in pre-assigned windows. All data is recorded digitally, allowing the operator to simultaneously operate a number of sensors and at the same time access stored data to work on the mission report without stress or risk of making errors. All sensor data, images, targets, etc. are annotated using navigation data from a single source, so that each piece of information becomes an integrated part of a Geographic Information System (GIS) on board the aircraft. Operator s Console Forward Looking Design The operator console provides the Human Machine Interface (HMI) between the operator and the mission sensors. 44 Facts & Figures

45 Key features The operator can choose the sensors on the console in order to carry out an analysis on the colour monitor. The aircraft s navigation system automatically includes the current flight data (position, course, time, etc.) in the images that appear on the monitor. The displayed screen shown at the operator console is handed over to the cockpit crew and can be selected by the cockpit crew to be imaged on the copilot MFD The sensors selected are saved on the hard drive integrated in the system and can be analysed in an instant. What s more, this data can also be saved on a portable hard drive, which allows for additional analyses to be carried out on the ground, sensor images to be printed out and data to be transferred to another computer. Displays can be remotely controlled via a serial link Secondary LCD / CDU Phone Radio Control Primary LCDs Joystick Keyboard Work Surface Console Radar Control Panel FLIR HCU ICS Control Panel Trackball FLIR Control Panel Laser Fire Control Circuit Breakers Push-to-talk Lights (generic solution) Facts & Figures 45

46 Operations Support Life Cycle Support As manufacturer of the Dornier 228 RUAG also offers comprehensive support services, ensuring that the aircraft can be operated safely, economically and in accordance with the customer s requirements at any time. RUAG s international, customer support services comprise technical support and supply of spare parts, documentation, field service and training. In addition, RUAG offers operators of special versions and small fleets of the Dornier 228 its Total Aircraft Care service, which provides full technical support and guaranteed availability for a fixed price per flight hour. Technical support Material support MRO services Training Modification/ upgrades Fleet management Technical documentation Service contracts, power-bythe-hour Field service Flight operations support 46 Facts & Figures

47 Technical and Operational Support Between 1982 and 2002, well over 200 Dornier 228s were built in Oberpfaffenhofen and were marketed worldwide. About 150 machines are still in service today, and many of these are serviced by RUAG. As holders of the type certificate of the Dornier 228 and licences EASA 21G, EASA 21J, EASA 145 and FAR 145, we offer comprehensive servicing for the Dornier 228 fleet operating worldwide. The scope of our services is as follows: Technical support beyond the basic documentation, e.g. with Service Problem Report (SPR) and Repair Approval Sheet (RAS) for complex repairs Modifications e.g. customer-specific mission equipment, engine and avionic upgrades The whole range of maintenance work (Line & Base) including engine inspections Complete and partial painting in our state-of-the-art paint shop Service contracts, Power-by-the-Hour contracts Fleet management in line with CAMO Training for pilots and maintenance staff Spare parts support 24-hour AOG Hotlines Technical Support Tel.: Fax: Material Support Tel.: Fax: Facts & Figures 47

48 Contents 2 Content Overview 4 Missions 4 Mission Challenges 7 Multirole Platform 8 Mission Match All Around the World 10 Maritime Patrol 14 Light Transport 15 PAX 16 Cargo 17 MedEvac 18 Paratrooper 20 Aircraft 20 Specifications 22 Performance 23 Certification Basis 24 Construction and Fuselage 26 Main Wing 28 Engines and Propellers 30 Cockpit 30 Glass Cockpit 32 Avionics 33 Communication Systems 34 Multi-Missions Management System (MMMS) 48 Facts & Figures

49 36 Sensors and Mission Systems 36 Overview 38 Mission adaptable 38 Side Looking Airborne Radar (SLAR) 38 Search/Surveillance Radar 39 SAR Direction Finder (SAR/DF) 39 Automatic Identification System (AIS) 40 Electro Optical / Infrared (EO/IR) 40 EO/IR + SAR = Optimal Sensor Package 41 Visible (VIS) Line Scanner 42 Ultraviolet / Infrared (UV/IR) Scanner 43 Microwave Radiometer (MWR) 44 Mission Management System 44 Operator s Console Forward Looking Design 46 Operations Support 46 Life Cycle Support 47 Technical and Operational Support 48 Contents Facts & Figures 49

50 50 Facts & Figures

51 Facts & Figures 51

52 RUAG Aerospace Services GmbH RUAG Aviation P.O. Box 1253 Special Airfield Oberpfaffenhofen Wessling Germany Phone