Table of content - Eurocopter

Table of Content 

1 Foreword....................................................................................................................................................... 5 

2 General Characteristics............................................................................................................................... 9 

2.1 Exterior Dimensions ................................................................................................................................ 9 

2.2 Internal Dimensions............................................................................................................................... 10 

2.3 Possible Cabin Arrangement................................................................................................................. 11 

2.4 Weight ................................................................................................................................................... 11 

2.5 Fuel Capacities...................................................................................................................................... 11 

2.6 Engines: 2 Turbomeca Turbine Engines - ARRIEL 1E2 ....................................................................... 12 

2.7 Main Transmission ................................................................................................................................ 12 

2.8 Typical IFR Antenna Layout .................................................................................................................. 12 

3 Baseline Aircraft Definition....................................................................................................................... 13 

4 Recommended Mission Configurations .................................................................................................. 15 

4.1 Recommended EMS Configuration....................................................................................................... 16 

4.1.1 Mission Parameter................................................................................................................................................................ 16 

4.1.2 Basic Mission Configuration ................................................................................................................................................. 16 

4.1.3 Further Available Equipment ................................................................................................................................................ 20 

4.1.4 Avionics Layout..................................................................................................................................................................... 21 

4.1.5 Performance Data................................................................................................................................................................. 21 

4.1.6 Typical Cabin Layout ............................................................................................................................................................ 23 

4.1.7 Further Available EMS Equipment........................................................................................................................................ 23 

4.2 Recommended Offshore Configuration................................................................................................. 24 





4.3 Recommended Police / Parapublic Configuration................................................................................. 30 




4.3.4 Avionics Layout..................................................................................................................................................................... 34 


4.3.6 Further Available Police / Parapublic Equipment.................................................................................................................. 36 

4.4 Recommended Corporate Transport Configuration (Stylence ® ) ........................................................... 37 





4.4.5 Typical Cabin Layout ............................................................................................................................................................ 42 

4.4.6 Exclusive VIP Cabin Solutions.............................................................................................................................................. 44 

4.5 Recommended Utility Configuration...................................................................................................... 45 





145.10.101.01 E Page 1 of 86 

The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. 

This document is property of EUROCOPTER ® , no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER ® and its contents shall not be disclosed. ©EUROCOPTER 2010

Table of Content 

5 Further Product Information ..................................................................................................................... 51 

5.1 Avionics Solutions ................................................................................................................................. 51 

5.1.1 Single/Dual Pilot IFR ............................................................................................................................................................ 51 

5.1.2 Single/Dual Pilot IFR with Dual FMS/NMS ........................................................................................................................... 52 

5.2 General Optional Equipment ................................................................................................................. 53 

5.3 NVG Solutions and Certification ............................................................................................................ 59 

6 Main Performance ...................................................................................................................................... 61 

7 Support Information................................................................................................................................... 75 

7.1 Assets.................................................................................................................................................... 75 

7.2 Inspection Program ............................................................................................................................... 75 

7.3 Main Components ................................................................................................................................. 77 

7.4 EUROCOPTER Deutschland GmbH ® Maintenance Support Programs ............................................... 78 

7.4.1 Classical Support.................................................................................................................................................................. 78 

7.4.2 Standard Exchange .............................................................................................................................................................. 78 

7.4.3 Repair with Guaranteed TAT................................................................................................................................................ 78 

7.4.4 Guaranteed DMC ................................................................................................................................................................. 78 

7.4.5 Unscheduled Maintenance Insurance Plan (UMIP).............................................................................................................. 79 

7.4.6 Parts By the Hour (PBH) ...................................................................................................................................................... 79 

7.5 Engine Maintenance Program ............................................................................................................... 79 

7.5.1 Standard Coverage: „Classic” SBH ® .................................................................................................................................... 79 

7.5.2 Customized Coverage: SBH ® „Mission”............................................................................................................................... 79 

7.5.3 Turbomeca Internet Web Site - TOOLS ............................................................................................................................... 80 

7.5.4 Time Between Major Overhauls ........................................................................................................................................... 80 

7.5.5 Life-Limited Parts (LLP)........................................................................................................................................................ 80 

7.6 Training.................................................................................................................................................. 81 

7.7 Technical Publications........................................................................................................................... 81 

7.8 T.I.P.I. (Technical Information Publication on Internet) ......................................................................... 82 

7.8.1 Description............................................................................................................................................................................ 82 

7.8.2 Main Features....................................................................................................................................................................... 82 

8 List of Abbreviations ................................................................................................................................. 83 

Page 2 of 86 145.10.101.01 E 



Technical Data 

Manufacturer´s notes - ATTENTION! 

EUROCOPTER ® s policy is one of on-going product enhancement which means that alterations in 

definition, pictures, weights, dimensions or performance may be made at any time without notice 

being included in those documents that have been issued. 

This document cannot thus be taken as an offer or serve as an appendix to a contract without a 

prior check as to its validity and prior written agreement of EUROCOPTER ® . 

The operational or certification regulations, as defined by the local authorities, can make compulsory 

the installation of some of the equipment or recommended solutions, listed in this document. 

This list does not claim to cover the whole of the worldwide operational requirements nor the 

equipment not specifically related to the helicopter (for example: life jacket) or necessary for particular 

missions (for example: supplemental oxygen). The operator is responsible for ascertaining 

with his local authorities that the planned configuration of the helicopter complies with regulatory 

requirements for the area(s) of operations and the type(s) of mission(s) considered. 

EUROCOPTER ® , its logo, M‘ARMS ® and Stylence ® are trade marks of the EUROCOPTER ® 

group. 




Blank 






1 Foreword 

Figure 1.1: Example of the EC145 

The EC145, certified under the name BK117 C-2, is a twin-engine, multi-purpose helicopter of the 3-4 

ton class with up to 12 seats for pilot/s and passengers. It combines EUROCOPTER DEUTSCHLAND 

GMBH ® s latest developments, like advanced cockpit design, avionics and sophisticated electrical system 

with the rugged and proven design elements of the BK117, as for example the rotor system. The 

EC145's hingeless rotor system with its monolithic titanium hub ('System Bölkow') is proven all over 

the world. Furthermore, the rotor blades have been improved with respect to higher performance and 

lower noise and vibration levels. The use of the variable rotor speed and torque matching system 

(VARTOMS), known from the predecessor model BK117 C-1 has been extended. Besides ameliorating 

flying comfort, this makes the EC145 the quietest helicopter in its class bringing it to 6.7 EPN dB 

below ICAO limits. 

In addition to environmental and economical aspects, the rotor system together with high TBO gearbox 

and airframe components grant for low maintenance costs and on the other hand, high in-service-time 

of the helicopter due to low scheduled maintenance required. 

The EC145 is equipped with two powerful and reliable Turbomeca Arriel 1E2 engines which, in combination 

with its lifting system, provide outstanding performance and vital power reserves even in oneengine-inoperative 

(OEI) scenarios. Twin-engine reliability is complemented by a fully separated fuel 

system, a tandem hydraulic system, dual electrical system and redundant lubrication for the main 

transmission. Further positive safety aspects of the EC145 are design elements like energy absorbing 

fuselage and seats, as well as crash resistant fuel cells. The EC145 allows Cat. A operation up to the 

level of performance class 1 and performance class 2 according to JAR-OPS 3. 

A wide range of optional equipment, like emergency floats, rescue hoist, SX16 search light, cargo 

hook, plus many more is available for the EC145 and can be fitted simultaneously in most cases. Together 

with its most versatile cabin layout (utility, comfort, corporate, ...), the EC145 is ready to take up 

all sorts of missions, for example survey, transport, EMS, public service, to name a few. 





Compared to other helicopters in its class, the EC145 offers a significantly larger cabin, featuring: 

• Excellent outside vision for pilot/s, crew and/or passengers 

• Roomy cabin with no partitions or protrusions, no center post, no door post 

• Unrivalled side loading (no door posts) and rear loading capability 

• Flat floor all over the cabin area 

Figure 1.2: View from rear into the empty cabin 





The EC145 offers a choice of modern state-of-the-art glass cockpit solutions comprising primary flight 

displays (PFD) and NAV displays (ND) as well as a central panel display system (CPDS). All LCD 

screens are well arranged on the instrument panel, easy to read even if viewed from an angle and feature 

perfect readability in any light conditions. A NVG layout is available as an option. The unique color 

coding, warning and information concept helps the pilot/s to collect all relevant parameters while suppressing 

presentation of non-relevant information. Additionally, EUROCOPTER DEUTSCHLAND 

GMBH ® s unique first limit indicator (FLI) considerably simplifies engine and torque monitoring. Being 

relieved from extensive instrument scan without missing vital information, pilots can dedicate more of 

their attention to the mission. 

Figure 1.3: Typical instrument panel 

Latest news / highlights 

• The new engine Inlet Barrier Filter (IBF) is now EASA certified and available with updated configuration 

items. It can be proposed for helicopters operating in sandy or polluted environment to protect 

the engine. 

• The HF-9000 system is now certified and can be proposed for helicopters where long distance communication 

is required. 

• Further Stylence ® interiors satisfy customers' high comfort demands; various layouts and colors can 

be offered. 

• A special device (comprising an audio input and an IC amplifier IC 3100 stereo) is available to connect 

an external music source and enjoy this music in stereo quality with respective headsets. 

• The IRIDIUM satellite phone and tracking system from SkyConnect is available for worldwide telephone 

communication. 

• Further refined VIP interior solutions can be offered. 

• EASA certification for the new high density seating interior with up to 10 seats in the cabin was granted 

late December 2009. Various seating arrangements can be offered. 




Blank 






2 General Characteristics 

2.1 Exterior Dimensions 

3.45 m 

11.32 ft 

Approx. 3.10 m 

10.17 ft 

11.00 m 

36,09 ft 

1 m 

3.28 ft 

0.93 m 

3.05 ft 

Figure 2.1: Exterior dimensions 

13.03 m/42.65 ft 

Rotors Running 

6.19 m 

20.31 ft 

1.73 m 

5.68 ft 

2.40 m 

7.87 ft 

10.2 m/33.5 ft 

0.75 m 

2.46 ft 

0.45 m 

1.48 ft 

1.96 m 

6.43 ft 



This document is property of EUROCOPTER ® , no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER ® and its contents shall not be disclosed. ©EUROCOPTER 2010 

1.30 m 

4.27 ft 

3.26 m/10.7 ft 

2.00 m/6.56 ft 

3.96 m/12.99 ft 

3.20 m/10.24 ft 

2.9 m/9.51 ft

2.2 Internal Dimensions 

Figure 2.2: Internal dimensions 

Cabin & baggage compartment 

(Baggage compartment with 8 seats installed) 

Floor area Volume 

4.72 m² 

0.84 m² 

50.77 ft² 

9.07 ft² 

6.04. m³ 

1.32 m³ 


213.15 ft³ 

46.72 ft³ 

Copilot 0.72 m² 7.73 ft 0.80 m³ 28.25 ft³ 

Pilot (not shaded) 1.09 m² 11.80 ft² 1.24 m³ 43.76 ft³ 

Total (undivided) 5.43 m² 58.50 ft² 6.84 m³ 241.40 ft³ 

Total (incl. pilot station) 6.52 m² 70.30 ft² 8.08 m³ 285.16 ft³ 





2.3 Possible Cabin Arrangement 

Seats & equipment as option 

Passenger transport 1 or 2 pilots + up to 8 passengers in club seating configuration (energy 

absorbing individual seats) + 1.32 m³ baggage / freight 

High density seating 1 or 2 pilots + up to 10 passengers in high-density seating configuration 

(energy absorbing individual troop seats) 

EMS / Casualty evacuation 1 or 2 pilots + up to 2 stretcher patients + up to 3 HEMS crew 

2.4 Weight 

kg lb 

• Empty weight, wet (in standard aircraft configuration) 1,792 3,951 

• Useful load (for standard aircraft configuration) 1,793 3,953 

• Pilot 80 176 

• Payload and/or fuel 1,713 3,777 

• Maximum take-off weight 3,585 7,903 

• Maximum take-off weight with external load 3,585 7,903 

• Sling load (single hook) 1,500 3,307 

NOTE: margin ± 1.5% 

2.5 Fuel Capacities 

Usable fuel Unusable fuel 

lb kg l lb kg 

• Main tank 1307.8 593.2 741.5 7.3 3.3 

• Supply tank (left) 104.1 47.2 59.0 6.6 3.0 

• Supply tank (right) 118.2 53.6 67.0 6.6 3.0 

• Total 1530.0 694.0 867.5 20.5 9.3 

NOTE: Tolerance of fuel figures: ± 2% Fuel density used is 0.8 kg / liter 




2.6 Engines: 2 Turbomeca Turbine Engines - ARRIEL 1E2 

NOTE: Thermodynamic limits per engine at SL, ISA 

2.7 Main Transmission 

Main transmission ratings 

2.8 Typical IFR Antenna Layout 


Engine ratings kW ch shp 

• One Engine Inoperative (OEI), 2.5 min power 574 780 770 

• One Engine Inoperative (OEI), MCP 550 748 738 

• Take-Off Power (TOP) 550 748 738 

• Maximum Continuous Power (MCP) 516 701 692 

Single engine operation kW ch shp 

• 2.5 min OEI-power 1 x 551 1 x 750 1 x 739 

• Maximum continuous OEI-power 1 x 404 1 x 550 1 x 542 

Twin engine operation kW ch shp 

• Take-Off Power (TOP) 2 x 388 2 x 528 2 x 520 

• Maximum Continuous Power (MCP) 2 x 316 2 x 430 2 x 424 

Figure 2.3: Typical IFR antenna layout 

a.If national regulations require an ADF 

1 ELT antenna 

2 GPS 1 antenna 

3 VOR / ILS antenna 

4 VHF / AM antenna 

5 GPS 2 antenna 

6 VHF AM 2 antenna 

7 Transponder antenna 

8 Marker antenna 

9 Radar altimenter antennas 

10 ADF antenna a 

11 DME antenna 





3 Baseline Aircraft Definition 

GENERAL 

• Energy absorbing fuselage 

• Tail boom with fixed horizontal stabilizer and two endplates 

• Upper deck with fittings for main gearbox, engines, hydraulic 

and cooling system 

• Cowlings for main transmission and engines 

• Skid-type landing gear with skid protectors, capable of taking 

ground-handling wheels 

COCKPIT, CABIN AND CARGO COMPARTMENT 

• One-level cabin and cargo compartment floor with integrated 

rails 

• Glazed canopy 

• Two hinged cockpit doors with sliding window 

• Map case in pilot´s door 

• Two wide passenger sliding doors 

• Two rear hinged clam-shell doors 

• Longitudinally adjustable energy absorbing pilot and 

copilot seats with head rest and 4-point safety belts with 

automaticlocking system; seat color grey or blue 

• Cabin boarding grips (LH and RH) 

• Interior paneling with integrated basic sound insulation 

• Flight controls (pilot side) 

• Engine twist grip controls at pilot´s collective pitch lever 

• Long boarding steps, LH and RH 

• Cold weather kit 

• Built-in maintenance steps and grips 

• Interior painting according to RAL7047 (telegrey 4) 

• Exterior painting (single color) 

• Instrument panel with extension on pilot´s side and glare 

shield 

• Ram-air for cockpit 

• Electrical ventilating system for cockpit 

• Headset holder in the cockpit, rotatable 

• Portable fire extinguisher 

• Stowage net for first aid kit at the LH rear clam-shell door 

• First aid kit a 

• Flash light (torch) 

• 4 mobile tie-down rings 

• Slant panel 

• Center console 

• Windscreen wiper for pilot and copilot 

• Door open warning 

a.First aid kit complies with German regulation rules 1. DV LuftBO paragraph 5(2). Type of operation, procedures or regulations 

may require a different/specific first aid kit. 

BASIC INSTRUMENTATION 

CENTRAL PANEL 

• Central Panel Display System (CPDS) consisting of two 

LCD displays 

• Cautions and Advisories Display (CAD) with digital indication 

of: 

• Caution and advisory information 

• Fuel quantitiy indication 

• Vehicle and Engine Multifunction Display (VEMD) with 

digital indication of: 

• Engine parameters (engine oil pressure, engine oil 

temperature) 

• FLI (First Limit Indicator) for TQ, TOT, ΔrN1 as analogue 

display 

• Main gear box parameters (oil pressure, oil temperature) 

• Dual amperemeter for generator; ampere meter for 

battery 

• Dual voltmeter 

• Outside Air Temperature (OAT) 

• Mast moment indication 

• Back-up conventional instruments (2”) 

•Clock 

• Stand-by-horizon 

• Triple (rotor and engines) RPM-indicator 

• Warning unit 

• Engine fire warning with fuel emergency shut-off 

• Warning lights 

• Aural warning (for each warning, rotor RPM, fire warning) 

• Fire extinguishing system warning 

• Master caution light 

• Main switch panel 

• DC power control 

• VARTOMS control 

• Start switches 

• Magnetic compass 

AIR DATA 

• Dual pitot static system (electrically heated pitot tube and 

static port) 

• 2 ADC MEGHAS sensors 

STANDARD INSTRUMENTS (SINGLE PILOT) a 

• Air speed indicator (3”) 

• Vertical speed indicator (3”) 

• Encoding altimeter (3”) 

• Artificial horizon (4”) 

• Gyro magnetic heading with horizontal situation ind. (3”) 

a.If glass cockpit instrumentation is chosen as optional equipment, these standard instruments are deleted (function included in 

MEGHAS) and an altimeter (2”) and an airspeed indicator (2”) as back-up instruments are added. 




POWER PLANT 

• Two TURBOMECA ARRIEL 1E2 turbine engines, complete 

with starting, fuel supply and control systems 

• Crash resistant fuel system 

• Two independent oil cooling and lubrication systems of 

the engines 

TRANSMISSION SYSTEM 

• Main transmission including an independent redundant 

lubrication system and monitoring sensors 

• Rotor brake system 

ROTOR AND FLIGHT CONTROLS 

• Hingeless main rotor (System Bölkow) with 4 glass and 

carbon fiber reinforced blades with erosion protection strip 

• Semi-rigid tail rotor with 2 twisted glass fiber reinforced 

blades of new technology with erosion protection strip 

• Basic provisions for an easy integration of a balancing 

system 

ELECTRICAL INSTALLATION 

• Power generation system: 

• Two starter/generators (2 x 200 A, 28 VDC) 

• Nickel-Cadmium battery, (24 V, 27 Ah), rear installation 

• External power connector (STANAG 3302) 

• Power distribution system: 

• Two primary busbars 

• Two essential busbars 

• Two shedding busbars 

• Two non-essential busbars (50 A) - for optional equipment 

only 

• Battery bus 

• One utility receptacle in cargo compartment (28VDC, 

15A) 

GROUND HANDLING KITa • Two ground-handling wheels 

• Basic aircraft covers (short time) 

• Oil drain hoses 

• Keys for cockpit doors, cabin doors, baggage compartment 

doors and tank flap (one-key system) 

a.Weight not included in the standard helicopter empty weight 

DOCUMENTATION (in English) 

One Flight Manual a 

One Pilots-Checklist, revision service for five years b 

• One Logbook b (only paper, CD-ROM on demand) 

• One Historical Record b (only paper, CD-ROM on demand) 

• One CD-ROM a b incl. AMM c , SDS c , WDM c , IPC, MSM 

• One add. Master Servicing Manual (MSM) a b on paper 

• One Service Bulletin Catalogue (SB) a b per contract, on 

paper 

a.Revision service included as long as the aircraft is operational 

b.Weight not included in the standard helicopter empty weight 

c.Customized documentation 


• Fire detection and extinguishing system 

• VARTOMS (Variable Rotor speed and Torque Matching 

System) 

• Overspeed control 

• Cycle counter 

• Tail rotor transmission and intermediate transmission with 

splash lubrication, magnetic plug and oil level sight gauge 

• Dual hydraulic boost system for cyclic and collective blade 

control of the main rotor 

• Single hydraulic boost system for yaw control 

• Stability Augmentation System (SAS) for tail rotor 

• Main and tail rotors tip painting (yellow) 

• Lighting: 

• Anti-collision warning light (red flashing) 

• Fixed landing light (250 W) 

• Three position lights (red, green, white) 

• Adjustable instrument lighting 

• One utility light in the cockpit 

• Lights in the cabin and cargo compartment 

• Boarding illumination 

• Emergency lights 

• Radio: 

• Two radio master switch 

• Battery key 

• Lifting points 

• Compass compensation key 

• Fuel drain device 

• One List of Applicable Publications (LOAP) a b , on paper 

• One Avionics Manual (for avionics installed by EURO- 

COPTER Deutschland GmbH®) b c (on paper) 

• One CD-ROM ECMM (Electronic Component Maintenance 

Manuals) for vendor manuals 

• Engine Documentation b , furnished by supplier, including: 

• Maintenance Manual 

• Illustrated Parts Catalogue (IPC) 





4 Recommended Mission Configurations 

The following mission configurations are recommended for the EC145. The created packages should 

be regarded as a first proposal for customers to evaluate the suitability of the EC145 for their operational 

fields. The shown packages comprise a list of mandatory and necessary options and they can be 

complemented by further items from the chapter "Further Available Equipment". 

The given configurations show a maximum level of compliancy with the detachable parts of the various 

options. 

The following recommended mission configurations are available: 

• EMS 

• Offshore 

• Police / Parapublic 

• Stylence ® 

• Utility 

The configurations show possible and practicable definitions coming from other experienced customer's 

demands. They provide a great adaptation to missions and are not orientated on keeping them 

significantly light to promote extraordinary range or endurance values. 

Please note that EMS and Offshore configurations include equipment requested by JAR-OPS 3 

Amendment 5. They do not cover oxygen equipment and equipment required for over water operation. 

As the national operating rules may differ from the JAR-OPS 3 Amendment 5, the operator has to contact 

his national authority to assure that the planned equipment configuration is acceptable for the intended 

kind of operation. 

Performance calculation 

All performance mission calculations data used in this document is for information purpose only and 

EUROCOPTER DEUTSCHLAND GMBH ® takes no responsibility for the correctness of this information 

as far as the applicability to the receiving party’s individual case is concerned. The present use of 

the named data shall not be construed as expressly or impliedly granting the receiving party any rights 

nor be deemed to constitute any kind of obligation or commitment of EUROCOPTER DEUTSCHLAND 

GMBH ® . 

Further individual configurations 

In chapter 5 the reader will find a list of all available optional equipment suitable for the EC145. He may 

choose further items and add them to his favorite configuration. Please note that there are various 

items which may be ordered for one helicopter, but their installation at the same time would not be possible 

completely or only partly; even a mixture of such items could make sense in specific mission configurations. 

A detailed discussion is highly recommended in order to adapt the EC145 to the customer's 

wishes and needs and to avoid misunderstandings which could lead to unsatisfactory configurations. 

Any modification and/or complement of the proposed mission configuration must be done with the assistance 

of a EUROCOPTER Deutschland GmbH® sales representative. 

Additionally tactical radios, broadcast, thermal imaging and video surveillance equipment, FLIR systems 

and operator consoles as well as NVG equipment can be offered on request. 

VIP interiors can be offered tailored to individual needs and tastes resulting from geographical operation 

and/or personal preferences. 




4.1 Recommended EMS Configuration 


This configuration is fitted with EMS equipment for general rescue operation and can be upgraded to 

special missions a customer may have. 

The shown helicopter configuration is prepared for an inter-hospital transport of one stretcher patient, 

a flight crew of two, and a medical crew of two. The helicopter is fitted with the respective items for IFR 

operation and fulfils JAR-OPS 3 Amendment 5 requirements of Germany. As the national operating 

rules may differ from the JAR-OPS 3 Amendment 5, the operator has to contact its national authority 

to assure that the planned equipment configuration is acceptable for the intended kind of operation. 

The helicopter can also be used for primary EMS missions and transport up to two patients on stretchers 

with two medical persons. 

4.1.1 Mission Parameter 

• Pilot Single / Dual pilot operation 

• VFR / IFR IFR 

• Day / Night Night 

•Cat A Yes 

• JAR-OPS 3 Yes 

• Instrumentation Glass cockpit AV PACK DP IFR G430W 

• MTOW 3585 kg 

4.1.2 Basic Mission Configuration 

Baseline aircraft 

Pilots 1 or 2 

Medics 2 

Patient 1 

Qty DocRef ComRef Title Weight 

[kg] 

Weight 

[lb] 

1 00-10011-A B0000-001-00 EC145 Baseline Aircraft 145.10.100.01 E 1,792.0 3,951.4 

Subtotal: 1,792.0 3,951.4 

1.5% Weight margin: 26.9 59.3 

Subtotal (incl. margin): 1,818.9 4,010.6 





General equipment 


[kg] 

Mission equipment 

Weight 

[lb] 

1 05-37018-B B6701-001-00 Copilot flight controls 6.5 14.3 

1 05-38011-C B3111-001-03 7” copilot instrument panel with glare shield 1.5 3.3 

1 05-39009-B B2514-003-01 Map case in copilot door 0.5 1.1 

1 05-41005-C B2104-100-00 Bleed air heating system 13.2 29.1 

1 05-43008-A B2576-003-00 Ventilation for avionics compartment 0.7 1.5 

1 05-61005-B B2433-002-00 Battery, type ”Saft”, ULM, 40Ah, 24V, 

instead of standard battery 

6.2 13.7 

1 05-68002-B B3343-003-00 Additional electrical unit 1.5 3.3 

1 05-02020-C B1111-002-00 Enhanced exterior painting instead of standard painting 2.0 4.4 

1 05-02029-B B1112-001-00 High visibility paint for main rotor blades 0.0 0.0 

1 05-22005-B B7924-002-00 Fuzz burner for tail rotor and intermediate gearbox 0.1 0.2 

1 05-22015-B B6343-001-00 Fuzz burner for main transmission 0.1 0.2 

1 05-22018-A B7924-001-00 Fuzz burner for engines 1.1 2.4 

1 05-22024-A B7114-008-00 Heat protection for engine cowling LH 0.4 0.9 

1 05-23007-B B7165-002-00 Engine compressor wash kit 1.7 3.7 

1 05-24019-B B6344-006-00 Vector Mast Moment System (VMMS) 0.3 0.7 

1 05-31032-B B5213-001-11 Sliding door fastener, intermediate and max. position, LH 0.4 0.9 

1 05-31034-B B5633-001-10 Window in clam-shell door, LH 0.3 0.7 

1 05-31034-B B5633-001-20 Window in clam-shell door, RH 0.3 0.7 

1 05-39010-B B3111-001-10 Map case on instrument panel glare shield 0.6 1.3 

1 05-39011-C B3113-005-20 Illuminated chart holder, pilot side 1.1 2.4 

1 05-41005-C B2104-100-01 Performance improvement kit for bleed air hearting system 3.9 8.6 

1 05-67015-B B8522-001-00 Additional electrical interface for mission equipment 0.8 1.8 

1 05-68001-B B3113-011-00 Additional circuit breaker panel 5.2 11.5 


[kg] 

Weight 

[lb] 

1 06-41015-B B3342-001-00 LED Anti-Collision Light (instead of standard version) 1.0 2.2 

1 06-45026-B B3343-006-00 Landing and search light, 400/200 W 4.5 9.9 

1 06-65005-C B2625-003-00 2nd portable fire extinguisher 2.6 5.7 

1 06-67045-C B2563-801-06 ELT C406-N HM (Artex) + NAV option 3.9 8.6 

1 06-40001-B B3349-001-00 Tail flood lights for tail rotor and clam-shell doors 1.4 3.1 

1 06-46004-B B3344-001-10 Strobe lights 0.7 1.5 

1 06-71007-B B2524-003-10 Separation curtain for cockpit / cabin, fixed provisions 0.1 0.2 

1 06-71007-B B2524-003-20 Separation curtain for cockpit / cabin, detachable parts 1.1 2.4 




Interior layout 

Avionics 



[kg] 

Weight 

[lb] 

1 07-00017-C B2581-002-20 Comfort improvement kit 24.1 53.1 

1 07-15014-B B2512-003-10 Height adjustable pilot seat instead of standard pilot seat 1.8 4.0 

1 07-15014-B B2512-003-20 Height adjustable copilot seat instead of standard copilot seat 1.8 4.0 

1 07-75020-B B2514-300-00 Attachment rails in cabin ceiling 4.6 10.1 

1 07-90016-B B2524-008-11 Multi-purpose fittings in cabin, LH 3.1 6.8 

1 07-90016-B B2524-008-12 Multi purpose fittings in cabin, RH 3.1 6.8 


[kg] 

1 08-00036-A B2300-005-02 AV PACK DP IFR G430Wa 1 08-16054-F B2341-190-01 Audio/Comm. control system 2x ACU 6100, 

pilot+copilot, and REU 6100 (Becker) 

Weight 

[lb] 

7.1 15.7 

1 08-16054-F B2341-293-01 IC amplifier IC 3100-4-01 (Becker) 2.1 4.6 

1 08-22031-C B2325-092-00 Transponder (Mode S) GTX 330 (Garmin) 3.5 7.7 

1 08-25032-A B3455-004-00 Distance Measuring Equipment DME-4000 (Rockwell Collins) 2.8 6.2 

1 08-26027-C B3431-090-01 Marker beacon receiver/lights KR 21 (Honeywell) 1.0 2.2 

1 08-43026-D B3442-093-00 GPS/NAV/COM GNS 430W (Garmin), copilot, VOR/ILS interfaced 

with FCDS, GPS stand alone 

5.6 12.3 

1 08-43026-D B3442-094-00 GPS/NAV/COM GNS 430W (Garmin), pilot, interfaced with 

FCDS 

8.1 17.9 

1 08-65005-C B3161-090-09 MEGHAS - Flight Control Display System (FCDS) - 

Dual (4xSMD45) 

25.9 57.1 

1 08-99002-A B0000-151-05 AV PACK DP IFR G430W interconnection / wiring 23.9 52.7 

1 08-21016-B B3441-090-04 Radar altimeter KRA 405 B (Honeywell) 3.2 7.1 

1 08-53003-B B2212-300-00 MEGHAS sensor kit 20.7 45.6 

1 08-72002-B B2212-001-00 Automatic Flight Control System - AFCS 30.5 67.3 

1 08-81025-C B3132-001-00 M‘ARMS ® Cockpit Voice and Flight Data Recorder (CVFDR) 16.0 35.3 

1 08-12041-A B4322-090-04 Fixed provisions for tactical radio #1 

(antenna, power supply, ICS interface) 

2.0 4.4 

1 08-16054-F B2341-845-00 Audio/Comm. control system ACU 6100 (Becker), EMS 1.4 3.1 

2 08-18062-A B2333-000-02 Headset Adapter cable crew GLENAIR/U92 0.2 0.4 

6 08-18062-A B2333-001-02 Headset Adapter cable pax GLENAIR/U92 1.2 2.7 

1 08-43040-A B3442-006-00 FCDS/DAFCS interface switch (GNS430) 0.6 1.3 

1 08-46042-A B3168-093-00 Moving map EURONAV IV+ - RN6CM (EuroAvionics), 

interfaced with FCDS, basic version 

3.9 8.6 

1 08-65006-B B3443-010-00 Video Radar Unit (VRU) 4.8 10.6 

Subtotal: 266.7 587.9 

3% Weight margin: 8.0 17.6 

Subtotal (incl. margin): 274.7 605.5 

a.System installation is not approved for WAAS navigation functions (e.g. LPV, LP, LNAV/VNAV and LNAV+V approaches); so 

these functions are de-activated. From mid 2010 onwards and in USA only, WAAS LPV approaches capability will be proposed 

by AE as STC. 





Aerolite EMS package 


[kg] 

Weight 

[lb] 

1 07-70048-A AEL-40100-005-2 EMS kit Aerolite 201.3 443.8 

1 Integral floor, fixed provisions - AEL 

1 Integral floor, detachable parts - AEL 

1 Stretcher "Cirrus 2000", LH, fix provisions - AEL 

1 Stretcher "Cirrus 2000", LH, detachable parts - AEL 

1 Medical seat stationary, aft RH, fix provisions - AEL 

1 Medical seat stationary, aft RH, detachable parts - AEL 

1 Medical seat slidable & swivelling, front RH, 

fix provisions - AEL 

1 Medical seat slidable & swivelling, front RH, 

detachable parts - AEL 

1 Medical cabinet full height, front center, fix provisions - AEL 

1 Medical cabinet full height, front center, detachable parts - AEL 

1 Medical supply unit, mid LH, fixed provisions - AEL 

1 Medical supply unit, mid LH, detachable parts - AEL 

1 Power & lighting system, mid LH - AEL 

2 Infusion hook, mid LH - AEL 

1 Retainer for monitor & defibrillator Corpuls C3 - AEL 

1 Retainer for monitor & defibrillator Corpuls C3 (only monitor) - 

AEL 

1 Retainer for respirator Weinmann medumat transport - AEL 

2 Retainer for infusion system Braun Perfusor Space - AEL 

1 Retainer for suction pump Laerdal LCSU 3 - AEL 

1 Medical oxygen system 3x3,0 lt. 200 bar, window LH, 

fix provisions - AEL 

1 Medical oxygen system 3x3,0 lt. 200 bar, window LH, 

detachable parts - AEL 

2 Tie down web - AEL 

1 Installation, certification & documentation - AEL 

3 Oxygen cylinder 3.0 lt. aluminium/carbon - Luxfer 

1 Monitor & defibrillator Corpuls C3 - GS 

1 Respirator medumat transport - Weinmann 

1 Suction pump LCSU 3 - Laerdal 

2 Infusion system perfusor space - Braun 

1 Blood glucose meter Omnitest Plus - Braun 

1 Respiration backpack incl. contents - Weinmann 

1 Emergency backpack incl. DIN13232-N contents - Weinmann 

1 Cervical collar set Perfit ACE & Mini Perfit ACE - Ambu 

1 Vacuum mattress - Tyromont 

1 Rescue bag with internal belt system - Tyromont 

Subtotal: 201.3 443.8 



Total: 2,300.9 5,073.3 




GSE 

4.1.3 Further Available Equipment 

NOTE: Weight is not included in the configuration above 



[kg] 

1 08-80000-A B3132-001-30 CVFDR read out kita a.Recommended 1 per customer if CVFDR is selected (PGS software included) 


[kg] 

Weight 

[lb] 

0.0 0.0 

Weight 

[lb] 

1 05-21016-B B8541-001-10 Wire strike protection system, fixed provisions 3.8 8.4 

1 05-21016-B B8541-001-20 Wire strike protection system, detachable parts 7.9 17.4 

1 05-37019-B B6721-001-00 Pedal cover for copilot flight controls 0.3 0.7 

1 06-11024-B B3274-001-10 Settling protectors, fixed provisions 0.1 0.2 

1 06-11024-B B3274-001-20 Settling protectors, detachable parts 8.1 17.9 

1 06-21019-D B8512-001-10 External hoist, LH, fixed provisionsa 12.4 27.3 

1 06-21019-D B8512-001-20 External hoist (without hook), detachable parts 62.9 138.7 

1 06-21019-D B8512-001-21 External hoist hook and standard damper 3.6 7.9 

1 08-31044-A B2571-002-00 Color weather radar RDR 2000, radar radome 0.9 2.0 

1 08-31044-A B3443-005-10 Color weather radar RDR 2000, installation provisions 

(electrical and mechanical) 

1.7 3.7 

1 08-31044-A B3443-005-21 Color weather radar RDR 2000, vendor parts (Honeywell) 

incl. control CP466 

1 08-15511-C B2315-040-00 IRIDIUM satellite communication and tracking system (Sky 

Connect), satellite transceiver unit 


Connect), cockpit dial panel 


Connect), event switch panel 

a.12.4 kg in combination with emergency floats; 9.8 kg without emergency floats 

b.1.7 kg in combination with CVFDR; 7.6 kg without CVFDR 

c.Recommended 1 per fleet customer (> 3 H/C) if CVFDR is selected 

5.8 12.8 

4.2 9.7 

1.2 2.7 

0.4 0.9 

1 08-18023-B B2315-001-10 Headset H 10-76 (David Clark), low impedance 0.6 1.3 

1 08-24027-A B3452-002-00 ADF system DFS-43A (Chelton/Wulfsberg) 8.6 19.0 

1 08-24027-A B3452-093-30 ADF control unit CDF-552 (Chelton) 1.4 3.1 

1 08-35020-E B2327-001-01 Traffic Advisory System TAS 9900BX with interface to GNS430 7.1 15.7 

1 08-83008-B B3171-001-00 M‘ARMS ® Usage Monitoring System (UMS) b 

1.7 3.8 

1 08-80001-A B3132-001-04 MFDAU tool kit c 

0.0 0.0 





4.1.4 Avionics Layout 

Figure 4.1: AV PACK DP IFR G430W 

4.1.5 Performance Data 

Weight breakdown (with max. fuel): 

• Equipped empty weight EMS configuration (incl. engine oil, unusable 

fuel and weight margin of ± 1.5%) 

1 SMD45 (copilot) PFD: 

Primary Flight Display 

2 SMD45 (pilot) PFD: 


3 SMD45 (pilot) ND: 

Navigation Display 

4 GPS/NAV/COM (pilot) 

GNS430W (Garmin) 

5 GPS/NAV/COM (copilot) 

GNS430W (Garmin) 

6 Transponder GTX 330 (Garmin) 

7 ICPs: MEGHAS 

Instrument Control Panels 

8 RCU: MEGHAS 

Reconfiguration Control Unit 

9 Audio/Comm. control unit 

ACU6100 (copilot) 

10 Audio/Comm. control unit 

ACU6100 (pilot) 

11 Autopilot control unit 

12 SMD45 (copilot) ND: 


13 Marker beacon receiver/light 

kg lb 

2,301 5,073 

• 2 Pilots (2 x 85 kg) 170 375 

• 2 medical crew (2 x 85 kg) 170 375 

• 1 stretcher patient (1 x 85 kg) 85 187 

• Reserve fuel 93 205 

• Contingency fuel 55 121 

• Trip fuel = max. fuel 546 1,203 

• Mission take-off weight 3,420 7,540 




Mission profile: 

• Take-off in SL (3,585 kg) 

• Climb flight AEO-MCP from SL to 7,000ft with VY , mean 65KIAS 

• Level flight in 7,000ft with VBR , mean 113KIAS 

• Descent from 7,000ft to SL with R/D of -1,000fpm, mean 80KIAS 

• Landing in SL 

• Contingency: 10% 

• Reserve: 30 minutes in 1,500ft at VY (65KIAS) 

Relevant flight data: 

• The calculated max. range (with max. fuel) is 313nm (579km) 

• Climb: 6nm 

• Level: 297nm 

• Descent: 10nm 

The corresponding flight time (incl. climb/descent phase) is approx. 2 hour 35 minutes. 

Planned Take-Off Weight (TOW) versus range: 

Figure 4.2: Planned TOW vs. range - EMS 






4.1.6 Typical Cabin Layout 

The two photos show a typical EMS cabin layout from Aerolite. 

Figure 4.3: Typical cabin layout - Aerolite 

4.1.7 Further Available EMS Equipment 

Other EMS configurations for medevac, primary and secondary EMS missions as well as for multirole 

missions can be proposed on request. 

• Stretchers and loading devices 

• Incubator transportation systems 

• Cabinets 

• Medical crew seats 

• Special floors 

• Retainers for medical apparatuses 

• Attachment points for equipment 

• Additional stowage options in cabin and cargo compartment 

• Oxygen systems 

• Suction systems 

• Special electrical systems 

• Special lighting systems 

• EMS Ground Power Unit connector 




4.2 Recommended Offshore Configuration 


This configuration is created for passenger transport missions with two pilots and six passengers from 

onshore bases to oil rig platforms. The helicopter is fitted with the respective items for IFR operation 

and fulfils JAR-OPS 3 Amendment 5 requirements of Germany. As the national operating rule may differ 

from the JAR-OPS 3 Amendment 5, the operator has to contact his national authority to assure that 

the planned equipment configuration is acceptable for the intended kind of operation. 

It is the operator's responsibility to still add needed survival equipment like life vests, life raft(s), etc. to 

fulfill his national/local operational requirements which are not known by EUROCOPTER DEUTSCH- 

LAND GMBH ® . 





•Cat A Yes 

• JAR-OPS 3 Yes 





Pilots 1 or 2 


[kg] 




Pax 6 

Weight 

[lb] 


Subtotal: 1,792.0 3,951.4 


Subtotal (incl. margin): 1,818.9 4,010.6




[kg] 



Weight 

[lb] 






1 05-61005-B B2433-002-00 Battery, type ”Saft”, ULM, 40AH, 24V 


6.2 13.7 










1 05-39011-C B3113-005-20 Illuminated chart holder, pilot side 1.1 2.4 

1 05-62011-B B2420-004-00 AC system 1.5 3.3 

1 05-93009-B B8544-001-10 Lashing points - 60 kts 1.3 2.9 


[kg] 

Weight 

[lb] 



1 06-67049-A B2563-812-00 Automatic Deployable ELT (ADELT) 9.0 19.8 

1 06-61017-C B3215-001-10 Emergency floats, fixed provisions 16.7 36.8 

1 06-61017-C B3215-001-20 Emergency floats, detachable parts 50.7 111.8 

1 06-65005-D B2625-003-00 2nd portable fire extinguisher 2.6 5.7 

1 06-66002-B B3353-015-00 Helicopter Emergency Egress Lighting (HEEL) 5.5 12.1 

1 06-69006-B B2341-006-61 Voice Alert Generator (NAT 611-014) 0.5 1.1 


[kg] 

1 07-27003-C B2523-002-10 Passenger seating, 3 club seats 

(front row, facing against flight direction) 

1 07-27003-C B2523-002-30 Passenger seating, 3 club seats 

(rear row, facing in flight direction 

Weight 

[lb] 

33.8 74.5 

33.2 73.2 

1 07-50032-B B5212-001-30 Jettisonable cabin doors 0.0 0.0 

1 07-50033-B B5212-001-00 Jettisonable cockpit doors 0.6 1.3 




Avionics 

GSE 



[kg] 

1 08-00036-A B2300-005-02 AV PACK DP IFR G430Wa 1 08-16054-F B2341-190-01 Audio/Comm. control system 2x ACU 6100, 

pilot+copilot, and REU 6100 (Becker) 

Weight 

[lb] 

7.1 15.7 





1 08-43026-D B3442-093-00 GPS/NAV/COM GNS 430W (Garmin), copilot, 

VOR/ILS interfaced with FCDS, GPS stand alone 

5.6 12.3 


FCDS 

8.1 17.9 



25.9 57.1 








1 08-31037-B B2571-001-00 Radar radome (for RDR 1600) 4.8 10.6 

1 08-31037-B B3443-004-00 Search and rescue weather radar RDR 1600 (Telephonics) 16.6 36.6 


1 08-53005-B B3424-000-00 AHRS Free Steering Mode 0.6 1.3 


1 08-83008-A B3171-001-00 M‘ARMS ® Usage Monitoring System (UMS) b 

1.7 3.8 

Subtotal: 378.7 834.9 



Total: 2,208.9 4,869.7 



by AE as STC. 

b.1.7 kg in combination with CVFDR; 7.6 kg without CVFDR 


[kg] 

1 08-80000-A B3132-001-30 CVFDR read out kit a 

a.Recommended 1 per customer if CVFDR is selected (PGS software included) 

Weight 

[lb] 

0.0 0.0 








[kg] 

Weight 

[lb] 

1 05-31046-A B5632-002-00 Push-out cabin windows 3.2 7.1 

1 05-42022-B B2105-001-00 Air conditioning/cooling system - Metro (STC) 51.3 113.1 

1 05-31032-B B5213-001-21 Sliding door fastener, intermediate and max. position, RH 0.4 0.9 

1 05-41005-C B2104-100-01 Performance improvement kit for bleed air heating system 3.9 8.6 

1 05-92015-C B6611-001-10 Main rotor blade folding, basic kit 0.3 0.7 

1 05-92015-C B6611-001-20 Main rotor blade folding, fixed provisions for ground handling kit 0.5 1.1 

1 05-92015-C B6611-001-30 Main rotor blade folding, ground handling kita 0.0 0.0 

1 06-21019-D B8512-001-11 External hoist, RH, fixed provisionsb 13.5 29.8 



1 06-21019-D B8512-001-22 External hoist hook damper floating device 0.4 0.9 

1 06-21020-B B8512-002-12 External hoist observation light, RH, fixed provisions 0.6 1.3 

1 06-21020-B B8512-002-20 External hoist observation light, detachable parts 0.8 1.8 

1 06-26012-B B8511-002-10 Cargo hook mirrors, fixed provisions 0.5 1.1 

1 06-26012-B B8511-002-20 Cargo hook mirrors, detachable parts 3.8 8.4 

1 06-26012-B B8511-002-21 Cover for cargo hook mirrors 0.4 0.9 

1 06-27028-B B8511-005-10 Cargo hook system, fixed provisions 9.3 20.5 

1 06-27028-B B8511-005-20 Cargo hook system, detachable parts 9.0 19.8 

1 07-27009-C B2522-000-09 High-density seating, 8 seats, 3 FWD / 3 LH / 2 RH - 

BAE Systems (STC) 

99.5 219.4 



109.2 240.7 

1 07-27009-C B2522-000-12 High-density seating, 10 seats, 3 FWD / 2 LH / 2 RH / 3 AFT - 


a.GSE (15.0 kg) 

b.13.5 kg in combination with emergency floats; 10.8 kg without emergency floats 

c.Installation on special 10” instrument panel at pilot side 

d.Recommended 1 per fleet customer (> 3 H/C) if CVFDR is selected 

123.5 272.3 

1 07-30019-B B2581-001-00 Soundproofing kit 6.0 13.2 

1 07-60019-B B2552-001-00 Variable tie-down net 3.3 7.3 

1 07-75020-B B2514-300-00 Attachment rails in cabin ceiling 4.6 10.1 


1 07-90016-B B2524-008-12 Multi-purpose fittings in cabin, RH 3.1 6.8 



4.2 9.3 



1.2 2.7 



0.4 0.9 

1 08-18023-C B2315-001-10 Headset H 10-76 (David Clark), low impedance 0.6 1.3 

1 08-17041-A B2331-001-00 Cabin loudspeaker 2.2 4.9 

1 08-17043-A B2332-001-00 Passenger address system DP4100 (Becker) 1.6 3.5 

1 08-35028-B B3446-000-00 Enhanced Ground Proximity Warning System (EGPWS) 

MK XXI (Honeywell) c 

5.3 11.7 

1 08-80001-A B3132-001-04 MFDAU tool kit d 

0.0 0.0 





Weight breakdown (with 6 passengers): 

• Equipped empty weight Offshore configuration (incl. engine oil, unusable 




The calculated max radius of action (with 6 passengers) is 126 nm (233 km). 


kg lb 

2,208 4,868 

• 2 Pilots (2 x 85 kg) 170 375 

• 6 passengers (6 x 95 kg) 570 1,257 



• Trip fuel 508 1,120 


• Take-off in SL (max. 3,585 kg) 

• Climb flight AEO-MCP from SL to 3.000ft with VY , mean 65KIAS 


• Descent from 3,000ft to SL with R/D of -1000fpm, mean 80KIAS 

• Landing and takeoff (with same number of PAX) in SL 


• Level flight in 3,000 with VBR , mean 117KIAS 

• Descent from 3,000ft to SL with R/D of -1000fpm, mean 80KIAS 



• Reserve: 20 minutes in 1,500ft at VBR , mean 119KIAS 





Payload versus Radius Of Action (ROA): 

Figure 4.4: Payload versus ROA - Offshore 




4.3 Recommended Police / Parapublic Configuration 


The shown configuration can be used for different tasks a police force may have (search and rescue, 

transport of intervention groups or high ranking people). The mission calculation is for a quick reaction 

team with two pilots and six specialists who can use both the rescue hoist and the rope down device 

to leave the helicopter in an intervention mission. For missions during night, the search light SX16 can 

illuminate the scene on ground with white light and IR light. 

In order to take into account the variety of missions a police squadron may have, this configuration includes 

a dual flight / navigation management system (FMS/NMS) providing full range of navigation and 

flight planning features, route databases, creation/storing/modification of routes, creation of flight plan, 

performing search and rescue and holding patterns. 





•Cat A Yes 

• JAR-OPS 3 No 

• Instrumentation Glass cockpit AV PACK DP FL NMS 




Pilots 1 or 2 

Police 6 


[kg] 

Weight 

[lb] 


Subtotal: 1,792.0 3,951.4 









[kg] 



Weight 

[lb] 






1 05-61005-B B2433-003-00 Battery, type ”Saft”, ULM, 44Ah, 24V 


9.7 21.4 










1 05-31032-B B5213-001-21 Sliding door fastener, intermediate and max. position, RH 0.4 0.9 

1 05-36008-B B8532-002-30 Multifunction step LH for standard landing gear 

(instead of standard boarding step) 

3.4 7.5 


[kg] 

Weight 

[lb] 

1 06-21019-D B8512-001-10 External hoist, LH, fixed provisions 9.8 21.6 



1 06-24011-B B8534-003-12 External rope down device for 2 persons, RH, fixed provisions 2.3 5:1 

1 06-24011-B B8534-003-22 External rope down device for 2 persons, RH, detachable parts 

- ECMS (STC) 

15.2 33.5 



1 06-45027-B B3346-004-10 Search light SX16, fixed provisions 5.3 11.7 

1 06-45027-B B3346-004-20 Search light SX16, detachable parts (W/O vendor parts) a 

10.2 22.5 

1 06-45027-B B3346-004-30 Search light SX16, with infrared filter, vendor partsa 29.8 65.7 



1 06-71007-B B2524-003-20 Separation curtain for cockpit / cabin, detachable parts 1.1 2.4 

a.see chapter 4.3.6 ITAR controlled item 


[kg] 

Weight 

[lb] 

1 07-50047-A B8512-004-10 External protection for cabin frame, LH 0.3 0.7 

1 07-50047-A B8512-004-11 External protection for cabin frame, RH 0.3 0.7 




Avionics 



[kg] 

1 08-00038-A B2300-006-01 AV PACK DP IFR FL NMS 

Weight 

[lb] 

1 08-11033-A B2313-094-01 VHF AM/COM system CVC-151 (Chelton), pilot 3.3 7.3 

1 08-11033-A B2313-093-01 VHF AM/COM system CVC-151 (Chelton), copilot 3.3 7.3 

1 08-16054-F B2341-190-01 Audio/Comm. control system 2x ACU 6100, pilot+copilot, 

and REU 6100 (Becker) 

7.1 15.7 


1 08-22014-B B2325-092-06 Transponder (Mode S) MST 67A (Honeywell) 6.4 14.1 

1 08-25030-A B3455-003-00 DME CDM-451 (Chelton) 3.1 6.8 

1 08-26013-A B3432-094-00 VOR/ILS/MKR navigation system CVN-251 (Chelton), pilot 4.9 10.8 

1 08-26013-A B3432-094-01 VHF/NAV combined control unit CCN-955 (Chelton), pilot 2.1 4.6 

1 08-26013-A B3432-093-00 VOR/ILS/MKR navigation system CVN-251 (Chelton), copilot 3.2 7.1 

1 08-44028-A B3442-022-00 Flight/Navigation Management system (CMA-9000) - Dual 

(CMC Electronics) 

12.9 28.4 

1 08-44028-A B3442-004-05 GPS sensor CMA-3024 for CMA-9000 (CMC Electronics) 4.9 10.8 

1 08-65005-C B3161-090-09 MEGHAS - Flight Control Display System (FCDS) - Dual 

(4xSMD45) 

25.9 57.1 

1 08-99002-A B0000-151-06 AV PACK DP IFR FL NMS interconnection / wiring 24.7 54.5 







1 08-16054-F B2341-193-10 Audio/Comm. control system ACU 6100 (Becker), PAX/3rd station, 

cabin panel RH 

0.3 0.7 


cabin panel cutout forward #1 

0.1 0.2 


protection for cabin panel forward #1 

1 08-16054-F B2341-193-30 Audio/Comm. control system ACU 6100 (Becker), Pax/3rd station, 

cabin RH 

0.1 0.2 

1.2 2.7 

1 08-44054-A B3442-024-00 Data transfer unit (DTU) for NMS - CMA-9000 (TARGA) 1.2 2.7 

1 08-46042-A B3168-093-00 Moving map EURONAV IV+ - RN6CM (EuroAvionics), interfaced 

with FCDS, basic version 

3.9 8.6 


Subtotal: 380.3 838.4 



Total: 2,210.6 4,873.5 





GSE 


[kg] 

1 08-80000-A B3132-001-30 CVFDR read out kita a.Recommended 1 per customer if CVFRD is selected (PGS software included) 




[kg] 

Weight 

[lb] 

0.0 0.0 

Weight 

[lb] 


1 05-81034-B B2818-100-10 Internal long range fuel tank system, fixed provisions 2.3 5.1 

1 05-81034-B B2818-100-20 Internal long range fuel tank system, detachable parts 38.0 83.8 

1 06-31014-B B8531-001-00 External loudspeaker system with siren 10.2 22.5 




1 06-27030-B B8511-008-10 Dual cargo hook system, fixed provisions 7.3 16.1 

1 06-27030-B B8511-008-20 Dual cargo hook system, detachable parts 21.4 47.2 

1 06-27031-B B8511-091-10 Dual cargo weighing system, fixed provisions 0.3 0.7 

1 06-27031-B B8511-091-20 Dual cargo weighing system, detachable parts 2.6 5.7 

1 06-65005-D B2625-002-00 2nd portable fire extinguisher, high-densitiy, 10 seats BAE 2.9 6.4 

1 06-81010-B B8503-001-10 Fire extinguishing bucket attachment (Bambi Bucket), fixed 

provisions 

0.8 1.8 

1 07-40010-B B2513-220-00 Washable floor covering for cockpit, cabin and cargo compartment 

14.1 31.1 

1 07-27003-C B2523-002-00 Passenger seating, 8 club seats (standard arrangement) 90.4 199.3 

1 07-27009-C B2522-000-06 High-density seating, 6 seats, 3 LH / 3 RH - BAE Systems 

(STC) 

75.4 166.2 

1 07-27009-C B2522-000-09 High-density seating, 8 seats, 3 FWD / 3 LH / 2 RH - BAE Systems 

(STC) 



99.5 219.4 

123.5 272.3 




1 08-10022-A B2314-090-10 HF system HF-9000 (ROCKWELL COLLINS), fixed provisions 13.9 30.6 

1 08-10022-A B2314-090-20 HF system HF-9000 (ROCKWELL COLLINS), detachable 

parts 

14.3 31.5 

1 08-14034-B B4322-090-10 Tactical radio RT-5000 and C-5000 control (NVG), fixed provisions 

7.7 17.0 

1 08-14034-B B4322-090-20 Tactical radio RT-5000 and C-5000 control (NVG), detachable 

parts 







10.8 23.8 

4.2 9.3 

1.2 2.7 

0.4 0.9 

1 08-18023-C B2315-001-10 Headset H 10-76 (David Clark), low impedance 0.6 1.3 




4.3.4 Avionics Layout 



[kg] 


1 08-31044-A B2571-002-00 Color weather radar RDR 2000, radar radome 0.9 2.0 

1 08-31044-A B3443-005-10 Color weather radar RDR 2000, installation provisions (electrical 

and mechanical) 

1.7 3.7 

1 08-31044-A B3443-005-21 Color weather radar RDR 2000, vendor parts (Honeywell) incl. 

control CP466 

5.8 12.8 

1 08-35020-E B2327-001-00 Traffic Advisory System TAS 9900BX with 3” indicator (Ryan) 10.3 22.7 

1 08-65005-C B3161-090-12 MEGHAS - Flight Control Display System (FCDS) - Dual 

(2xSMD45/1xSMD68) a 

26.9 59.3 

1 08-80001-A B3132-001-04 MFDAU tool kitb 0.0 0.0 

a.Instead of MEGHAS - Flight Control Display System (FCDS) - Dual (4xSMD45) 

b.Recommended 1 per fleet customer (> 3 H/C) if CVFDR is selected 

Figure 4.5: AV PACK DP IFR FL NMS 

Weight 

[lb] 

1 SMD 45 (copilot) PFD: 


2 SMD 45 (pilot) PFD: 


3 Autopilot (AFCS) Control Unit 

(min. required equipment) 

4 Audio / Comm. Control Unit 

ACU 6100 (pilot) 

5 SMD 45 (pilot) ND: 



ACU 6100 (copilot) 

7 RCU°: MEGHAS 


8 Navigation Management 

System CMA-9000 (pilot) 

9 ICP‘s: MEGHAS 

Reconfiguration Control Panel 




System CMA-9000 (copilot) 

12 SMD 45 (copilot) ND: 


13 NAV/COM system control unit 






Weight breakdown (with 6 team members): 

• Equipped empty weight Police / Parapublic configuration (incl. engine 

oil, unusable fuel and weight margin of ± 1.5%) 



The calculated maximum radius of action (with 6 team members) is 90.5 nm (168 km). 

kg lb 

2,211 4,874 

• High-density seats, 6 seats 75 165 

• 2 Pilots (2 x 85 kg) 170 375 

• 6 team members (6 x 110 kg) 660 1,455 


• Trip fuel 395 871 




• Level flight in 3,000ft with VH , mean 120KIAS 


• Rope down phase (all team members dropped-off) in SL with HOGE, 5 minutes 


• Level flight in 3,000ft with , mean 125KIAS 







Payload versus Radius Of Action (ROA): 

Figure 4.6: Payload versus ROA - Police / Parapublic 

4.3.6 Further Available Police / Parapublic Equipment 


Optional equipment like FLIR camera system, downlink and operator work station as well as 

NVG solutions are available on request. 

(*) Items are controlled under the provisions the US International Traffic in Arms Regulations and therefore 

require a US re-export licence. EUROCOPTER DEUTSCHLAND GMBH ® is committed to strict 

compliance with all applicable US Regulations and requires a corresponding commitment from the customer, 

too. EUROCOPTER DEUTSCHLAND GMBH ® cannot guarantee that a US ITAR licence will be 

granted. Nevertheless EUROCOPTER DEUTSCHLAND GMBH ® will perform all necessary procedures 

for obtaining such licence. Customer shall support the licence application procedure by providing 

the necessary documentation and information, particularly end-user certificates, undertakings, documents 

on the utilization of the commodities, etc. Customer shall adhere to the parameters and requirements 

of the re-export licence and US regulations. EUROCOPTER DEUTSCHLAND GMBH ® reserves 

the right to deliver the helicopter without the ITAR-controlled items should the US authorities deny or 

delay the (re-)export licence. The same is valid if the US authorities do not react at all or in cases of a 

return without action or if otherwise the absence of a required licence or provisions of US law inhibit a 

delivery in time. 





4.4 Recommended Corporate Transport Configuration (Stylence ® ) 

This configuration is created for corporate transport. The helicopter complies with IFR rules and the 

calculated mission is for a flight with a crew of one pilot, one passenger on the copilot seat and 7 passengers 

in the cabin. 





• Cat A Yes 






Pilots 1 or 2 


[kg] 




Pax 7 

Weight 

[lb] 


Subtotal: 1,792.0 3,951.4 


Subtotal (incl. margin): 1,818.9 4,010.6






[kg] 

Weight 

[lb] 








6.2 13.7 


1 05-02020-C B1111-003-00 Complex exterior painting instead of standard painting 2.0 4.4 





1 05-42022-B B2105-001-00 Air conditioning/cooling system - Metro (STC) 51.3 113.1 

1 05-85007-B B7321-001-00 Fuel management system (Fuel flow meters) 1.0 2.2 


[kg] 

Weight 

[lb] 




1 06-89001-A B2631-000-00 Smoke detector 0.5 1.1 


[kg] 

Weight 

[lb] 

1 07-00017-B B2581-002-20 Comfort improvement kit 24.1 53.1 

1 07-60038-A B2513-001-00 Map cases in sliding doors LH/RH 0.7 1.5 

1 07-30019-B B2581-001-00 Soundproofing kit 6.0 13.2 

1 07-27003-C B2523-002-10 Passenger seating, 3 club seats (front row, facing against 

flight direction) 

33.8 74.5 

1 07-27003-C B2523-002-21 Passenger seating, 1 club seat (middle row, LH) 11.7 25.8 

1 07-27003-C B2523-002-22 Passenger seating, 1 club seat (middle row, RH) 11.7 25.8 

1 07-27003-C B2523-002-31 Passenger seating, 2 club seats (rear row, facing in 

flight direction 

22.1 48.8 

1 07-31001-A B2524-001-10 Separation wall Cabin Baggage Compartment, fixed provisions 2.0 4.4 

1 07-30051-A AEL-40220-004-2 EC145 Stylence ® separation wall 5.5 12.1 

1 07-80026-B AEL-40200-002-1 Standard Stylence ® package 7 seats layout 28.1 62.0 





Avionics 


[kg] 

1 08-00036-A B2300-005-02 AV PACK DP IFR G430Wa 1 08-16054-F B2341-190-01 Audio/Comm. control system 2x ACU 6100, pilot+copilot, 


GSE 

Weight 

[lb] 

7.1 15.7 







5.6 12.3 


FCDS 

8.1 17.9 



25.9 57.1 






1 08-18055-C B2341-007-00 Fixed provisions for ANR 0.5 1.1 

9 08-18057-A B2315-002-11 Headset AHX34-04 ANR LEMO 28 VDC (Bose), 

low impedance 

2.7 6.0 

2 08-18062-A B2333-000-04 Headset adapter cable crew GLENAIR/LEMO ANR 0.2 0.4 

7 08-18062-A B2333-001-04 Headset adapter cable pax GLENAIR/LEMO ANR 1.4 3.1 


1 08-46042-A B3168-093-00 Moving map EURONAV IV+ - RN6CM (EuroAvionics), interfaced 

with FCDS, basic version 

3.9 8.6 


Subtotal: 406.1 895.3 



Total: 2,237.2 4,932.8 



by AE as STC. 


[kg] 

1 08-80000-A B3132-001-30 CVFDR read out kita a.Recommended 1 per customer if CVFDR is selected (PGS software included) 

Weight 

[lb] 

0.0 0.0 






To comply with JAR-OPS 3 operation rules: 



[kg] 

Weight 

[lb] 

1 05-41005-C B2104-100-01 Performance improvement kit for bleed air heating system 3.9 8.6 

1 05-93009-B B8544-001-10 Lashing points - 60 ktsa 1 05-93010-A B8544-002-00 Lashing points - 100 kts a 

a.NSF (no simultaneous fitment) 

b.Instead of standard version 

c.Installation on special 10” instrument panel at pilot side 

d.Recommended 1 fleet customer (> 3 H/C) if CVFDR is selected 

1.3 2.9 

4.5 9.9 

1 06-46004-B B3344-001-10 Strobe lights 0.7 1.5 


1 07-50032-B B5212-001-30 Jettisonable sliding doors 0.0 0.0 

1 07-50033-B B5212-001-00 Jettisonable cockpit doors 0.6 1.3 


1 07-81083-A AEL-40230-002-2 Stylence ® 8 th pax seat 11.9 26.2 

1 07-83018-A AEL-40220-003-2 Stylence ® curtain between cockpit and cabin 1.1 2.4 

1 07-85018-A AEL-40240-002-2 Stylence ® rear cabinet 16.0 35.3 

1 08-17078-A B2341-009-00 Audio input 0.1 0.2 

1 07-91034-A B2582-000-00 Special interior painting 0.0 0.0 

1 08-15031-B B2319-001-10 Fixed provisions for GSM phone (antenna, 28VDC, interfacing 

to ICS) 

0.8 0.8 







4.2 9.3 

1.2 2.7 

0.4 0.9 

1 08-16056-A B2341-393-01 IC amplifier IC 3100 STEREOb 2.3 5.1 


1 08-24027-A B3452-093-30 ADF control unit CDF-552 (Chelton) 1.4 3.1 

1 08-35020-E B2327-001-01 Traffic Advisory System TAS 9900BX 

with interface to GNS430 

7.1 15.7 

1 08-35028-B B3446-000-00 Enhanced Ground Proximity Warning System (EGPWS) MK 

XXI (Honeywell) c 

1 08-80001-A B3132-001-04 MFDAU tool kit d 


[kg] 

5.3 11.7 

0.0 0.0 

Weight 

[lb] 

1 05-39011-B B3113-005-20 Illuminated chart holder, pilot side 1.1 2.4 

1 06-65005-D B2625-003-00 2 nd portable fire extinguisher 2.6 5.7 

The offered equipment package is derived from the conditions stated in JAR-OPS 3 Amendment 5. 

This package does not cover oxygen equipment and equipment required for over water operations. As 

the national operating rules may differ from the JAR-OPS 3 Amendment 5, the operator shall contact 

himself his national authority to assure that the planned equipment configuration is acceptable for the 

intended kind of operation. 






Weight breakdown (with 8 passengers): 

• Equipped empty weight Stylence ® configuration (incl. engine oil, unusable 




The corresponding flight time (incl. climb/descent phase) is approx. 2 hours 13 minutes. 

kg lb 

2,237 4,932 

• 1 Pilot (1 x 85 kg) 85 187 

• 8 passengers (8 x 85 kg) 680 1,499 



• Trip fuel 481 1,060 









• The calculated max. range (with 8 passengers) is 266nm (492km) 


• Level: 249nm 





Payload versus range: 

Figure 4.7: Payload versus range - Stylence ® 

4.4.5 Typical Cabin Layout 

Figure 4.8: Typical cabin layout - Stylence ® 






Features 

• Carbon fibre look for air outlet plates 

• Armrests upholstered with leather 

• Leather upholstery for integrated door cases 

• Special painted sliding doors harmonized with interior trim 

• Stylence seat upholstery with leather, partly perforated areas 

• Map pocket in backside of the seats 

• Visible aluminium structure of seat 

• Control covers matched with Stylence leather 

• Carpet with leather trimming 

The available Stylence ® color lines are listed as following: 

DocRef ComRef Color Line Definition Color 

07-80026-A AEL-40290-001-2 Aubergine Leather: Coloris 5840 

Carpet: 6/707 

Interior paint: RAL 1015 

07-80026-A AEL-40290-002-2 Brick Leather: Coloris 710 

Carpet: 6/403 


07-80026-A AEL-40290-002-3 Camel Leather: Coloris 720 

Carpet: 6/403 


07-80026-A AEL-40290-002-4 Chocolate Leather: Chocolate 6985 

Carpet: 6/205 


07-80026-A AEL-40290-002-5 Graphite Leather: Coloris 703 

Carpet: 6/403 


07-80026-A AEL-40290-002-6 Marine Leather: Coloris 708 

Carpet: 6/308 





4.4.6 Exclusive VIP Cabin Solutions 

The following exclusive VIP cabin solutions are available on customer request. 

Figure 4.9: Typical interior details - Stylence 

Features: 

• Predefined high quality materials 

• Predefined front and/or rear cabinet 

• 4 VIP seats covered with leather 

• Pilot and copilot (if installed) seats covered with leather 

• Belts and buckles harmonized with the color of the leather 

• Metallic (various „finish”) air outlets, reading lights and handles 

• Separation wall between cabin and cargo compartment covered with leather 

• Interior covered with leather 

• Hand tufted carpet (long pile) 

• In-flight entertainment system (DVD, IPod, etc. ...) 






4.5 Recommended Utility Configuration 

This configuration is intentionally created for external and internal load transport missions. The helicopter 

is kept relatively light to offer a high payload. The calculated mission is for internal cargo transport 

with one pilot only. 




• Day / Nigth Night 

• Cat A Yes 



• MTOW 3,585 kg 



Pilots 1 or 2 


[kg] 

Weight 

[lb] 


Subtotal: 1,792.0 3,951.4 










[kg] 

Weight 

[lb] 








6.2 13.7 










[kg] 

Weight 

[lb] 





1 06-27028-B B8511-005-10 Cargo hook system, fixed provisions 9.3 20.5 

1 06-27028-B B8511-005-20 Cargo hook system, detachable parts 9.0 19.8 


1 06-81010-B B8503-001-10 Fire extinguishing bucket attachment (Bambi Bucket), 

fixed provisions 

0.8 1.8 





Avionics 


[kg] 

1 08-00036-A B2300-005-02 AV PACK DP IFR G430Wa 1 08-16054-F B2341-190-01 Audio/Comm. control system 2x ACU 6100, pilot+copilot, 


Weight 

[lb] 

7.1 15.7 







5.6 12.3 


FCDS 

8.1 17.9 



25.9 57.1 








Subtotal: 207.1 456.5 



Total: 2,032.2 4,480.8 



by AE as STC. 








[kg] 

Weight 

[lb] 


1 05-42022-A B2105-001-00 Air conditioning/cooling system - Metro (STC) 51.3 113.1 

1 05-81034-B B2818-100-10 Internal long range fuel tank system, fixed provisions 2.3 5.1 

1 05-81034-B B2818-100-20 Internal long range fuel tank system, detachable parts 38.0 83.8 

1 06-11023-B B3272-001-20 Snow skids 22.4 49.4 

1 06-11024-B B3274-001-10 Settling protectors, fixed provisions 0.1 0.2 

1 06-11024-B B3274-001-20 Settling protectors, detachable parts 8.1 17.9 

1 06-21019-D B8512-001-10 External hoist, LH, fixed provisions 9.8 21.6 

1 06-21019-D B8512-001-20 External hoist (without hook), detachable parts 

(incl. 1 week winch operator training) 

62.9 138.7 


1 06-21019-D B8512-001-22 External hoist hook damper floating device 0.4 0.9 

1 06-21020-B B8512-002-11 External hoist observation light, LH, fixed provisions 0.6 1.3 

1 06-21020-B B8512-002-20 External hoist observation light, detachable parts 0.8 1.8 

1 06-21030-A B8510-001-00 Cable deflector protection on floats landing gear 1.2 2.7 


1 06-27029-A B8511-003-10 Cargo hook weighing system, fixed provisions 0.4 0.9 

1 06-27029-A B8511-003-20 Cargo hook weighing system, detachable parts 1.8 4.0 

1 06-61017-C B3215-001-10 Emergency floats, fixed provisions 16.7 36.8 

1 06-61017-C B3215-001-20 Emergency floats, detachable parts 50.7 111.8 

1 06-65005-D B2625-003-00 2nd portable fire extinguisher 2.6 5.7 

1 06-65005-D B2625-002-00 2nd portable fire extinguisher (high-density seating, 10 BAE 

seats) 

2.9 6.4 

1 07-27003-C B2523-002-00 Passenger seating, 8 club seats (standard arrangement) 90.4 199.3 



99.5 219.4 



109.2 240.7 



1 07-40010-B B2513-220-00 Washable floor covering for cockpit, cabin and 

cargo compartment 

123.5 272.3 

14.1 31.1 

1 07-50037-B B5205-008-00 Spoiler position for cockpit doors 1.0 2.2 

1 07-50047-A B8512-004-10 External protection for cabin frame, LH 0.3 0.7 


1 07-74055-A AAT-40120-007-2 Stretcher „Rescue” foldable for helicopter floor, LH / RH - AAT 18.7 41.2 

1 07-74056-A AEL-40120-006-1 Stretcher „Cirrus 1000” foldable, LH/RH, fix provisions - AEL 1.0 2.2 

1 07-74056-A AEL-40120-006-2 Stretcher „Cirrus 1000” foldable, LH/RH, detachable parts - 

AEL 

14.5 32.0 



1 08-10022-A B2314-090-10 HF system HF-9000 (ROCKWELL COLLINS), fixed provisions 13.9 30.6 

1 08-10022-A B2314-090-20 HF system HF-9000 (ROCKWELL COLLINS), 

detachable parts 

14.3 31.5 

1 08-12041-A B4322-090-04 Fixed provisions for tactical radio #1 (antenna, power supply, 

ICS interface) 

2.0 4.4 






[kg] 

1 08-18023-B B2315-001-10 Headset H 10-76 (David Clark), low impedance 0.6 1.3 

1 08-81025-C B3132-001-00 M’ARMS ® Cockpit Voice and Flight Data Recorder (CVFDR) 16.0 35.3 

1 08-80000-A B3132-001-30 CVFDR read out kit a 

0.0 0.0 

1 08-80001-A B3132-001-40 MFDAU took kitb 0.0 0.0 

a.Recommended 1 per customer if CVFDR is selected (PGS software included) 

b.Recommended 1 per fleet customer (>3 H/C) if CVFDR is selected 


Weight breakdown (with payload and maximum fuel): 

• Equipped empty weight Utility configuration (incl. engine oil, unusable 




The corresponding flight time (incl. climb/descent phase) is approx. 2 hour 50 minutes. 

Weight 

[lb] 

kg lb 

2,032 4,480 

• 1 Pilots (1 x 85 kg) 85 187 

• Payload 774 1,706 


• Trip fuel = max. fuel 616 1,358 








• The calculated max. range (with payload and maximum fuel) is 339.5nm (629km) 


• Level: 322.5nm 





Payload versus range 

Figure 4.10: Payload versus range - Utility 






5 Further Product Information 

5.1 Avionics Solutions 

5.1.1 Single/Dual Pilot IFR 

Figure 5.1: AV PACK DP IFR G430 

Contents of AV PACK DP IFR G430W 







4 GPS / NAV / COM (pilot) 

GNS 430W (Garmin) 

5 GPS / NAV / COM (copilot) 

GNS 430W (Garmin) 

6 Transponder GTX 330 (Garmin) 

7 ICPs: MEGHAS 

Instrument Control Panels 

8 RCU: MEGHAS 

Reconfiguratin Control Unit 

9 Audio / Comm. control unit 

ACU6100 (copilot) 

10 Audio / Comm. control unit 

ACU6100 (pilot) 

11 Autopilot control unit 



13 Marker beacon receiver / lights 


[kg] 

1 08-00036-A B2300-005-02 AV Pack DP IFR G430Wa , consisting of: 

Audio/Comm. Control system 2 x ACU 6100, pilot and copilot, 

and Remote Electronic Unit REU 6100 (Becker) 

IC amplifier IC 3100-4-01 (Becker) 

Transponder (Mode S) GTX 330 (Garmin) 

Distance Measuring Equipment DME-4000 (Rockwell Collins) 

Marker Beacon receiver / lights KR 21 (Honeywell) 

GPS/NAV/COM GNS 430W (Garmin), pilot, interfaced with 

FCDS 

GPS/NAV/COM GNS 430W (Garmin), copilot, VOR/ILS interfaced 


MEGHAS - Flight Control Display System (FCDS) Dual 

(4xSMD45) 

AV PACK DP IFR G430 interconnection / wiring 

Weight 

[lb] 

80.0 176.4 



by AE as STC. 




5.1.2 Single/Dual Pilot IFR with Dual FMS/NMS 

Figure 5.2: AV PACK DP IFR FL NMS 

Contents of AV PACK DP IFR FL NMS 






3 Autopilot (AFCS) control unit 

(min. required equipment) 


ACU 6100 (pilot) 




ACU 6100 (copilot) 

7 RCU°: MEGHAS 



System CMA-9000 (pilot) 






System CMA-9000 (copilot) 



13 NAV / COM system control unit 


[kg] 

Weight 

[lb] 

1 08-00038-A B2300-006-01 AV PACK DP IFR FL NMS, consisting of: 103.9 229.1 

VHF AM/COM system CVC-151 (Chelton), pilot 

VHF AM/COM system CVC-151 (Chelton), copilot 

Audio/Comm. Control system 2 x ACU 6100, pilot and copilot, 

and Remote Electronic Unit REU 6100 (Becker) 

IC amplifier IC 3100-4-01 (Becker) 

Transponder (Mode S) MST 67A (Honey well) 

DME CDM-451 (Chelton) 

VOR/ILS/MKR navigation system CVN-251 (Chelton), pilot 

VHF/NAV combined control unit CCN-955 (Chelton), pilot, fixed 

provisions and detachable parts 

VOR/ILS/MKR navigation system CVN-251 (Chelton), copilot 

Flight/Navigation Management System (CMA-9000) a - Dual 

(CMC Electronics) 

GPS sensor CMA-3024 for CMA-9000 (CMC Electronics) 

MEGHAS - Flight Control Display System (FCDS) Dual 

(4xSMD45) 

AV PACK DP IFR FL NMS interconnection / wiring 

a.VHF AM/COM, VHF NAV and ATC transponder are controlled via CMA-9000 





5.2 General Optional Equipment 

The following list presents the available optional equipment which may be added to customize the recommended 

configurations or to build specific configurations. For further mission adaptation specific 

items are also available on request. Please take into account that there may be incompatibilities 

between various optional equipment items. Any modification and/or complement of the proposed mission 

configuration must be done with the assistance of a EUROCOPTER DEUTSCHLAND GMBH ® 

sales representative. 


Title Weight [kg] Weight [lb] 

Enhanced exterior painting instead of standard painting 2.0 4.4 

Complex exterior painting instead of standard painting 2.0 4.4 

High visibility paint for main rotor blades 0.0 0.0 

Boarding grips for cockpit 0.1 0.2 

Wire strike protection system, fixed provisions 3.8 8.4 

Wire strike protection system, detachable parts 7.9 17.4 

Fuzz burner for tail rotor and intermediate gearbox 1.1 2.4 

Fuzz burner for main transmission 1.1 2.4 

Fuzz burner for engines 1.1 2.4 

Improved heat protection for engine cowling LH 0.6 1.3 

Improved heat protection for engine cowling RH 0.6 1.3 

Heat protection for engine cowling LH 0.4 0.9 

Engine compressor wash kit 1.7 3.7 

Vector Mast Moment System (VMMS) 0.3 0.7 

Inlet barrier filter, fixed provisions 5.5 12.1 

Inlet barrier filter, transmission cowling modification 1.9 4.2 

Inlet barrier filter, detachable parts (incl. 1 set filter elements) 18.9 41.7 

Inlet barrier filter cowling cover, detachable parts 3.2 7.1 

Inlet barrier filter elements (1 set + Trawash box) 0.0 0.0 

Inlet barrier filter maintenance kit 0.0 0.0 

Inlet barrier filter generator covers kit -0.1 -0.2 

Inlet barrier filter weather protection kit 3.0 6.6 

IFR - training screen, fixed provisions 0.1 0.2 

IFR - training screen, detachable parts 2.1 4.6 

Sliding door fastener, intermediate and max. position, LH 0.4 0.9 

Sliding door fastener, intermediate and max. position, RH 0.4 0.9 

Window in clam-shell door, LH 0.3 0.7 

Window in clam-shell door, RH 0.3 0.7 

Push-out cabin windows 3.2 7.1 

Sliding window in sliding door LH 0.6 1.3 

Sliding window in sliding door RH 0.6 1.3 

Sliding window in sliding door with spoiler LH 0.8 1.8 

Sliding window in sliding door with spoiler RH 0.8 1.8 

Tinted cockpit door windows LH/RH 0.0 0.0 

Tinted sliding door windows LH/RH 0.0 0.0 

Tinted sliding door windows with sliding windows LH/RH 0.0 0.0 







Tinted cabin windows LH/RH 0.0 0.0 

Tinted window in rear clam-shell door, LH 0.0 0.0 

Tinted window in rear clam-shell door, RH 0.0 0.0 

Multifunction step LH for standard landing gear (instead of standard boarding step) 3.4 7.5 

Multifunction step RH for standard landing gear (instead of standard boarding step) 3.4 7.5 

Copilot flight controls 6.5 14.3 

Pedal cover for copilot flight controls 0.3 0.7 

Collective control guards 0.4 0.9 

7“ copilot instrument panel with glare shield 1.5 3.3 

Map case in copilot door 0.5 1.1 

Map case on instrument panel glare shield 0.6 1.3 

Illuminated chart holder, copilot side 1.1 2.4 

Illuminated chart holder, pilot side 1.1 2.4 

Illuminated chart holder (NVG version), copilot side 1.1 2.4 

Illuminated chart holder (NVG version), pilot side 1.1 2.4 

Bleed air heating system 13.2 29.1 

Performance improvement kit for bleed air heating system 3.9 8.6 

Air conditioning / cooling system - Metro (STC) 51.3 113.1 

Ventilation for avionics compartment 0.7 1.5 

Battery, type “Saft”, ULM, 40Ah, 24V instead of standard battery 6.2 13.7 

Battery, type ”Saft”, ULM, 44Ah, 24V instead of standard battery 9.7 21.4 

AC system 1.5 3.3 

Additional electrical interface for mission equipment 0.8 1.8 

Power socket 28V MK / LH 0.9 2.0 

Additional circuit breaker panel 5.2 11.4 

Additional electrical unit 1.5 3.3 

Internal long range fuel tank system, fixed provisions 2.3 5.1 

Internal long range fuel tank system, detachable parts 38.0 83.8 

Self-sealing fuel supply tanks 14.0 30.9 

Fuel management system (Fuel flow meters) 1.0 2.2 

Main rotor blade folding, basic kit 0.3 0.7 

Main rotor blade folding, fixed provisions for ground handling kit 0.5 1.1 

Main rotor blade folding, ground handling kita 0.0 0.0 

Lashing points - 60 kts 1.3 2.8 

Lashing points - 100 kts 4.5 9.9 

a.GSE (15.0 kg) 


Snow skids 22.4 49.4 

Settling protectors, fixed provisions 0.1 0.2 

Settling protectors, detachable parts 8.1 17.9 

External hoist, LH, fixed provisions 9.8 21.6 

External hoist (without hook), detachable parts 62.9 138.7 

External hoist hook and standard damper 3.6 7.9 

External hoist, RH, fixed provisions 10.9 24.0 






External hoist hook damper floating device 0.4 0.9 

External hoist observation light, RH, fixed provisions 0.6 1.3 

External hoist observation light, detachable parts 0.8 1.8 

External hoist observation light, LH, fixed provisions 0.6 1.3 

Cable deflector protection on floats landing gear 1.2 2.6 

External rope down device for 2 persons, LH, fixed provisions 2.3 5.1 

External rope down device for 2 persons, RH, fixed provisions 2.3 5.1 

External rope down device for 2 persons, LH, detachable parts - ECMS (STC) 15.2 33.5 

External rope down device for 2 persons, RH, detachable parts - ECMS (STC) 15.2 33.5 

Cargo hook mirrors, fixed provisions 0.5 1.1 

Cargo hook mirrors, detachable parts 3.8 8.4 

Cover for cargo hook mirrors 0.4 0.9 

Cargo hook system, fixed provisions 9.3 20.5 

Cargo hook system, detachable parts 9.0 19.8 

Cargo hook weighing system, fixed provisions 0.4 0.9 

Cargo hook weighing system, detachable parts 1.8 4.0 

Dual cargo hook system, fixed provisions 7.3 16.1 

Dual cargo hook system, detachable parts 21.4 47.2 

Dual cargo hook weighing system, fixed provisions 0.3 0.7 

Dual cargo hook weighing system, detachable parts 2.6 5.7 

External loudspeaker system with siren 10.2 22.5 

Tail flood lights for tail rotor and clam-shell doors 1.4 3.1 

LED Anti-Collision Light (instead of standard version) 1.0 2.2 

Additional landing light at cross tube, LH, 250W 1.2 2.6 

Landing & search light, 400/200 W 4.5 9.9 

Search light SX16, fixed provisions 5.3 11.7 

Search light SX16, detachable parts (w/o vendor parts) 10.2 22.5 

Search light SX16, with infrared filter, vendor parts 29.8 65.7 

Strobe lights 0.7 1.5 

Emergency floats, fixed provisions 16.7 36.8 

Emergency floats, detachable parts 50.7 111.8 

Emergency hammer 0.2 0.4 

2nd portable fire extinguisher (high density seating, 10 BAE seats) 2.9 6.4 

2 nd portable fire extinguisher 2.6 5.7 

Helicopter Emergency Egress Lighting (HEEL) 5.5 12.1 

Illuminated signs „NO SMOKING / FASTEN SEAT BELT” 0.2 0.4 

ELT C406-N HM (Artex) + NAV option 3.9 8.6 

Underwater Locator Beacon (ULB) 0.3 0.7 

Automatic Deployable ELT (ADELT) 9.0 19.8 

Voice alert generator (NAT 611-014) 0.5 1.1 

Separation curtain for cockpit / cabin, fixed provisions 0.1 0.2 

Separation curtain for cockpit / cabin, detachable parts 1.1 2.4 

NVG compatible cabin and cargo compartment 0.2 0.4 

NVG compatible standard cockpit layout 0.8 1.8 

NVG friendly external lighting kit 0.1 0.2 

IR flasher 1.1 2.4 







Fire extinguishing bucket attachment (Bambi Bucket), fixed provisions 0.8 1.8 

Smoke detector 0.5 1.1 


Comfort improvement kit 24.1 53.1 

Height adjustable pilot seat instead of standard pilot seat 1.8 4.0 

Height adjustable copilot seat instead of standard copilot seat 1.8 4.0 

Passenger seating, 8 club seats (standard arrangement) 90.4 199.3 

Passenger seating, 3 club seats (front row, facing against flight direction) 33.8 74.5 

Passenger seating, 2 club seats (front row, facing against flight direction) 22.1 48.8 

Passenger seating, 1 club seat (middle row, LH) 11.7 25.8 

Passenger seating, 1 club seat (middle row, RH) 11.7 25.8 

Passenger seating, 3 club seats (rear row, facing in flight direction) 33.2 73.2 

Passenger seating, 2 club seats (rear row, facing in flight direction) 22.1 48.8 

High-density seating, 2 seats, 2 FWD - BAE Systems (STC) 26.9 59.3 

High-density seating, 3 seats, 3 FWD - BAE Systems (STC) 33.8 74.5 

High-density seating, 6 seats, 3 FWD / 3 AFT - BAE Systems (STC) 67.5 148.8 

High-density seating, 6 seats, 3 FWD / 3 LH - BAE Systems (STC) 71.5 157.6 

High-density seating, 6 seats, 3 FWD / 3 RH - BAE Systems (STC) 71.5 157.6 

High-density seating, 6 seats, 3 LH / 3 RH - BAE Systems (STC) 75.4 166.2 

High-density seating, 7 seats, 3 FWD / 2 LH / 2 RH - BAE Systems (STC) 89.8 198.0 





High-density seating, 10 seats, 3 FWD / 2 LH / 2 RH / 3 AFT - BAE Systems (STC) 123.5 272.3 

Soundproofing kit 6.0 13.2 

EC145 Stylence ® separation wall 5.5 12.1 

Separation wall cabin baggage compartment, fixed provisions 2.0 4.4 

Washable floor covering for total floor area, complete 14.1 31.1 

Sealed cabin floor 0.4 0.9 

Jettisonable sliding doors 0.0 0.0 

Jettisonable cockpit doors 0.6 1.3 

Spoiler position for cockpit doors 1.0 2.2 

External protection for cabin frame, LH 0.3 0.7 

External protection for cabin frame, RH 0.3 0.7 

Door catch system for cockpit doors 0.1 0.2 

Door catch system for sliding doors 0.2 0.4 

Variable tie-down net 3.3 7.3 

Map cases in sliding doors LH/RH 0.7 1.5 

EMS Kit - Aerolite (AEL) 201.3 443.8 

Disaster Management Kit - Aerolite (AEL) 102.2 225.3 

EMS Kit - Air Ambulance Technology (AAT) 223.6 492.9 

Lengthened seat rails for cockpit rails 3.5 7.7 

Stretcher "Rescue" foldable for Helicopter Floor, LH/RH - AAT 18.7 41.2 






Stretcher "Cirrus 1000" foldable, LH/RH, fix provisions - AEL 1.0 2.2 

Stretcher "Cirrus 1000" foldable, LH/RH, detachable parts - AEL 14.5 32.0 

Attachment rails in cabin ceiling 4.6 10.1 

Standard Stylence® Package 7 seats layout 28.1 61.9 

Stylence® 8 th seat 11.9 26.2 

Stylence® curtain between cockpit and cabin 1.1 2.4 

Stylence® rear cabinet 16.0 35.3 

Multi-purpose fittings in cabin, LH 3.1 6.8 

Multi-purpose fittings in cabin, RH 3.1 6.8 

Special interior painting 0.0 0.0 

Avionics 


HF system HF-9000 (Rockwell Collins), fixed provisions 13.9 30.6 

HF system HF-9000 (Rockwell Collins), detachable parts 14.3 31.5 

Tactical radio VHF-FM NPX138N (NAT) a 2.3 5.1 

Tactical radio VHF-FM NPX138N - NVG (NAT) a 

2.3 5.1 

Fixed provisions for tactical radio #1 (antenna, power supply, ICS interface) 2.0 4.4 

Tactical Radio TETRA System 7-450 and CH150 control (Chelton) a 4.5 9.9 

Tactical radio RT-5000 and C-5000 control (NVG), fixed provisions 7.7 17.0 

Tactical radio RT-5000 and C-5000 control (NVG), detachable partsa 10.8 23.8 

Fixed provisions for GSM phone (antenna, 28VDC, interfacing to ICS) 0.8 1.8 

IRIDIUM satellite communication and tracking system (Sky Connect), satellite transceiver unit 4.2 9.3 

IRIDIUM satellite communication and tracking system (Sky Connect), cockpit dial panel 1.2 2.6 

IRIDIUM satellite communication and tracking system (Sky Connect), event switch panel 0.4 0.9 

IRIDIUM Satellite communication and tracking system (Sky Connect), cockpit dial panel - NVG 1.2 2.6 

Wireless Intercom System (Polycon) a 3.8 8.4 

IRIDIUM satellite phone AEROPHONE (Aerodata) 4.0 8.8 

Audio/Comm. control system ACU 6100 (Becker), EMS 1.4 3.1 

Audio/Comm. control system ACU 6100 (Becker), PAX/3rd station, cabin panel RH 0.3 0.7 

Audio/Comm. control system ACU 6100 (Becker), PAX/3rd station, 


0.1 0.2 




cabin panel cutout rearward #3 





0.1 0.2 

0.1 0.2 

0.1 0.2 

0.1 0.2 

Audio/Comm. control system ACU 6100 (Becker), Pax/3rd station 1.2 2.6 

Audio/Comm. control system ACU 6100 (Becker), Pax/4th station 1.2 2.6 

IC amplifier IC 3100 STEREO 2.3 5.1 

Cabin loudspeaker 2.2 4.9 

Cabin loudspeaker, NVG version 2.2 4.9 

Passenger address system DP4100 (Becker) 1.6 3.5 

Audio input 0.1 0.2 






Headset H 10-76 (David Clark), low impedance 0.6 1.3 

Headset H 10-56 (David Clark), high impedance 0.6 1.3 

Headset H 10-76 ANR/ENC with battery pack (David Clark), low impedance 0.8 1.8 

Headset H 10-56 ANR/ENC with battery pack (David Clark), high impedance 0.8 1.8 

Fixed provisions for ANR 0.5 1.1 

Headset AHX34-04 ANR LEMO 28 VDC (Bose), low impedance 0.3 0.7 

Headset AHX32-02 ANR U/174 with battery pack (Bose), low impedance 0.3 0.7 

Headset Adapter cable crew GLENAIR/U92 0.1 0.2 

Headset Adapter cable pax GLENAIR/U92 0.2 0.4 

Headset Adapter cable crew GLENAIR/LEMO ANR 0.1 0.2 

Headset Adapter cable pax GLENAIR/LEMO ANR 0.2 0.4 

Headset Adapter cable pax GLENAIR/LEMO ANR stereo 0.2 0.4 

Radar altimeter KRA 405 B (Honeywell) 3.2 7.1 

ADF system DFS-43A (Chelton/Wulfsberg) 8.6 19.0 

ADF control unit CDF-552 (Chelton) 1.4 3.1 

Direction Finder DF931-6 (Chelton), incl. Control unit 9.5 20.9 

Radar radome (for RDR 1600) 4.8 10.6 

Search And Rescue weather radar RDR 1600 (Telephonics) 16.6 36.6 

Color weather radar RDR 2000, radar radome 0.9 2.0 

Color weather radar RDR 2000, installation provisions (electrical and mechanical) 1.7 3.7 

Color weather radar RDR 2000, vendor parts (Honeywell) incl. control CP466 5.8 12.8 

Color weather radar RDR 2000, vendor parts (Honeywell) incl. control CP466, NVG 5.8 12.8 

Traffic Advisory System TAS 9900BX with interface to GNS430 7.1 15.7 

Traffic Advisory System TAS 9900BX with 3" indicator (Ryan) 10.3 22.7 

Enhanced Ground Proximity Warning System (EGPWS) MK XXI (Honeywell) 5.3 11.7 

FCDS/DAFCS interface switch (GNS430) 0.6 1.3 

Data transfer unit (DTU) for NMS - CMA-9000 (TARGA) 1.2 2.6 

Moving map EURONAV IV+ - RN6 (EuroAvionics), interfaced with FCDS, basic versiona 6.7 14.8 

Moving map EURONAV IV+ - RN6CM (Euro Avionics) interfaced with FCDS, basic version a 

3.9 8.6 

MEGHAS sensor kit 20.7 45.6 

AHRS Free Steering Mode 0.6 1.3 

MEGHAS - Flight Control Display System (FCDS) - Dual (2xSMD45/1xSMD68) 26.9 59.3 

Video Radar Unit (VRU) 4.8 10.6 

Automatic Flight Control System - AFCS 30.5 67.2 

M’ARMS ® Usage Monitoring System (UMS) 7.6 16.8 

M’ARMS ® Cockpit Voice and Flight Data Recorder (CVFDR) 16.0 35.3 

CVFDR read out kit 0.0 0.0 

MFDAU tool kit 0.0 0.0 

PGS software 0.0 0.0 

a.Tactical mission equipment cannot be certified by EASA. EUROCOPTER Deutschland GmbH® will ensure that the equipment 

is compatible with the basic helicopter and will assist the customer in obtaining certification or acceptance approval in his country. 





5.3 NVG Solutions and Certification 

In order to increase mission capabilities and flight safety during night operations, the EC145 can be 

fitted with NVG compatible cockpit and cabin layouts as well as exterior lighting. 

May 31, 2007, the first certification providing the EC145 with a NVG aided operation capability was 

granted from EASA, FAA and TCCA (Canada). Thus Eurocopter is the first Original Equipment Manufacturer 

(OEM) to offer this capability to civil operators. 

The certification is based on one specific configuration using among others the MEGHAS display system; 

suitable night vision goggles are specific goggles with class B filter from well known manufacturers 

(at press date, certified goggles are ITT F4949 and NOGALIGHT NL-93). 

On customer's request, Eurocopter will develop and certify other configurations and support also night 

vision goggle systems from other manufacturer. 

Please note that classic night flight capability remains unrestricted. 

Figure 5.3: Typical cockpit layout at night operation 




Blank 






6 Main Performance 

The following performance values and figures refer to an EC145, equipped with average production 

engines. 

Unless otherwise specified, the values and figures refer to a clean helicopter at Sea Level (SL), in International 

Standard Atmosphere (ISA) and zero wind condition. 

Performance on 2 engines (AEO) 

Gross Weight kg 

lb 

• Maximum speed VNE km/h 

kts 

• Maximum cruising speed VH km/h 

kts 

• Fuel consumption at maximum cruising 

speed 

2,400 

5,290 

2,700 

5,950 

3,000 

6,615 

3,300 

7,275 

3,585 

7,905 




kg/h 

lb/h 

• Recommended cruising speed km/h 

kts 

• Fuel consumption at recommended 

cruising speed 

kg/h 

lb/h 

• Fuel consumption at 65 KIAS kg/h 

lb/h 

• Maximum rate of climb (TOP) m/s 

ft/min 

• Hover ceiling IGE (TOP), (3 ft AGL), 

ISA 

• Hover ceiling OGE (TOP), ISA m 

ft 

• Service ceiling, MCP 

(climb reserve 200 ft/min), ISA 

• Range at recommended cruise speed 

(no reserve) with 

• standard fuel tank (694kg) 

• longe range fuel (869kg) 

• Endurance at 65 KIAS (no reserve) 

• with standard fuel tank 

• longe range fuel tank (869kg) 

m 

ft 

m 

ft 

km 

nm 

km 

nm 

h:min 

h:min 

278 

150 

256 

138 

258 

569 

237 

128 

234 

516 

178 

392 

14.9 

2,940 

5,485 

18,000 

5,485 

18,000 

5,485 

18,000 

--- 

--- 

--- 

--- 

--- 

--- 

278 

150 

254 

137 

258 

569 

239 

129 

238 

525 

183 

404 

13.0 

2,560 

5,485 

18,000 

5,120 

16,800 

5,485 

18,000 

705 

380 

--- 

--- 

3:55 

--- 

268 

145 

252 

136 

258 

569 

241 

130 

244 

538 

190 

418 

11.2 

2,210 

4,695 

15,400 

4,345 

14,260 

5,485 

18,000 

700 

377 

875 

472 

3:50 

4:50 

268 

145 

250 

135 

258 

569 

243 

131 

251 

554 

197 

434 

9.3 

1,840 

3,840 

12,600 

3,445 

11,300 

5,485 

18,000 

685 

370 

865 

467 

3:40 

4:40 

268 

145 

246 

133 

258 

569 

243 

131 

254 

560 

204 

450 

8.1 

1,600 

2,925 

9,600 

770 

2,230 

5,240 

17,200 

680 

370 

855 

461 

3:35 

4:30

Performance on 1 engine (OEI) 

Gross Weight kg 

lb 

• Single engine service ceiling, OEI MCP, 

100 ft/min climb reserve, ISA 

• Single engine service ceiling, OEI, MCP, 

100 ft/min climb reserve, ISA + 20°C 

• Maximum rate of climb, OEI MCP, SL, 

ISA 

• Max. temperature for CAT A, take-off 

from clear heliport at SL 

• Max. weight HOGE, OEI 2.5 min-power, 

SL, ISA 

• Max. weight HOGE, OEI 2.5 min-power, 

SL, ISA + 20°C 

2,400 

5,290 

2,700 

5,950 

3,000 

6,615 


3,300 

7,275 

3,585 

7,905 

Operating limitations 

The helicopter can be operated within the following altitude and temperature limitations (according to 

the Flight Manual): 




m 

ft 

m 

ft 

m/s 

ft/min 

5,455 

17,900 

4,965 

16,300 

5.7 

1,120 

4,590 

15,060 

4,025 

13,220 

4.4 

860 

3,755 

12,320 

3,095 

10,160 

3.2 

630 

2,965 

9,730 

2,185 

7,170 

2.1 

420 

1,995 

6,550 

1,335 

4,390 

1.2 

230 

°C + 50 + 50 + 50 + 49 + 42 

kg 

lb 

kg 

lb 

• Max. weight CAT A, VTOL, SL, ISA kg 

lb 

• Max. weight CAT A, VTOL, SL, ISA + 

10°C 

• Maximum operating altitude 5,485 m PA 

18,000 ft PA 

• Maximum operating altitude for hover in ground effect, takeoff 

and landing 

• Minimum temperature -45°C 

kg 

lb 

2,785 

6,140 

2,520 

5,555 

3,415 

7,530 

3,320 

7,320 

5,485 m PA or DA 

18,000 ft PA or DA 

whichever is less 

• Maximum temperature ISA +35°C 

(max. +50°C)


Hover In Ground Effect (HIGE, TOP) 

Figure 6.1: Hover In Ground Effect (HIGE, TOP) 




Hover Out Of Ground Effect (HOGE, TOP) 

Figure 6.2: Hover out Of Ground Effect (HOGE, TOP) 






Take-Off Weight, Cat A, Clear Heliport 

Figure 6.3: Take-Off Weight, Cat A, Clear Heliport 




Take-Off Weight, Cat A, VTOL 

Figure 6.4: Take-Off Weight, Cat A, VTOL 






Maximum Cruising Speed 

Figure 6.5: Maximum Cruising Speed 




Maximum Rate Of Climb, TOP, 3585 kg (MTOW) 

Figure 6.6: Maximum Rate Of Climb, TOP, 3,585 kg (MTOW) 






Maximum Rate Of Climb, MCP, 3,585 kg (MTOW) 

Figure 6.7: Maximum Rate Of Climb, MCP, 3,585 kg (MTOW) 




Fuel consumption (AEO) 

Figure 6.8: Fuel consumption (AEO) 

see page 72 








see page 72 





see pages 

70 and 71 







Payload versus range (AEO) 

Figure 6.11: Payload versus range (AEO) 




Blank 






7 Support Information 

7.1 Assets 

Proven reliability and availability based on experience 

EUROCOPTER DEUTSCHLAND GMBH ® s helicopter production programs have developed a strong 

reputation worldwide for being fully committed to providing customers with operational, capable aircraft 

that achieve high availability combined with cost-effective support systems. To achieve this record of 

performance, EUROCOPTER DEUTSCHLAND GMBH ® has stressed the importance of working together 

with its customers to ensure constant feedback on their demonstrated in-service Reliability, Availability 

and Maintainability/Testability (RAM) data. The main objective is to reach the most optimized 

operational cost ensuring the highest flight safety. 

EUROCOPTER DEUTSCHLAND GMBH ® has built and delivered EC145 helicopters for almost ten 

years. More than 300 helicopters are in service worldwide. The total flight hours accumulated at the 

end of December 2009 are approximately 325,000 Fh. The "lead the fleet" aircraft has accumulated 

approximately 5,400 Fh. 

7.2 Inspection Program 

The Maintenance Program specifies the intervals between maintenance operations that are recommended 

by EUROCOPTER DEUTSCHLAND GMBH ® , irrespective of whether they are mandatory or 

not. 

The program can: 

• either be used as is, 

• or be adapted by each operator to suit his own specific organization, provided he complies with the 

maximum intervals. 

The following table provides an overview of all inspections. Scheduled inspections with shorter time 

intervals have to be added to those with longer time intervals. 

This means, that for example the Periodical Inspection contains the Supplementary Check and the 12- 

Month Inspection. 

Scheduled airframe inspection Maintenance level Estimated man hour 

Pre-flight check O - Level Pilot task 

Supplementary check at 100 hours O - Level 1,3 hours 

12-month inspection I - Level 16 hours 

Periodic inspection at 600 hours I - Level 82 hours 

Extended periodic inspection at 6000 hours a 

I - Level tbd 

a.will be deleted with one of the next revisions of MSM 

Organizational Level (O) 

Tasks of the daily servicing, checks, inspections for condition, replacement of modular components, 

simple repairs, no special tools necessary. 

Intermediate Level (I) 

Smaller repairs ON/OFF helicopter, periodical inspections, replacement of modular components which 

require special tools and/or test equipment. 





Note 

All the "hands-on" aircraft values mentioned here above are given on the basis of a 20,000 flight hours 

life cycle. They refer only to the scheduled inspections for the standard helicopter without optional 

equipment in accordance with the Master Servicing Manual (MSM). 

The announced Man Hours are without incoming flight, work preparation, reworking, servicing, Service 

Bulletin implementation and unscheduled maintenance. 

As an alternative to the current maintenance program described above, EUROCOPTER DEUTSCH- 

LAND GMBH ® provides the Continuous Maintenance Program (CMP). The CMP consists of individual 

work packages to be performed each within a defined timeframe. A specific tolerance is effective for 

all work packages, which refer to the start and end time of the individual work packages. Thus, this 

program allows the continued flight operation without being interrupted by inspections with longer 

downtimes. Depending on the yearly flight hours, three different models are available. One program is 

applicable for an average flight profile (from 300 Fh up to 600 Fh per year), one for a high-timer flight 

profile (more than 600 Fh per year) and one for a low-timer flight profile (less than 300 Fh per year). 

Please refer also to the figure below, which shows the allocation of the work packages through one 

cycle, using the example of the average flight profile. 

Figure 7.1: Example of the average flight profile 

The following table provides an overview of all engine inspections. Each inspection has to be performed 

for the respective time frame. For example, a large inspection like the 600 Fh inspection does not 

contain the 30 Fh, 100 Fh and 300 Fh. 

Scheduled engine inspection 

Daily checks (Pilot task) 

Maintenance level Estimated mean man hour 

Checks before the 1st flight O - Level 0,033 h 

Checks between two flights visit (1) O - Level 0,017 h 

Checks after the last flight of the day O - Level 0,067 h 

Periodic inspections (acc. MM Aug. 2008) 

30 Hours O - Level 0,25 h 




1200 Hours I - Level 3,00 h 

3000 Hours I - Level 27,86 h 





7.3 Main Components 

Time Between Overhaul (TBO) / Service Life Limit (SLL) 

Main components TBO as per MSM 

Rev. 10 

Cartridge of fuel pump 5.000 Fh 

NOTE: list non exhaustive 

SLL as per MSM 

Rev. 10 

Main rotor blade assy 12.000 Fh 

Main transmission 3.600 Fh 

Main rotor shaft 30.000 Fh 

Freewheel clutch 3.600 Fh 

Intermediate gearbox 1.500 Fha Input shaft (intermediate gearbox) 4.200 Fh 

Output shaft (intermediate gearbox) 4.200 Fh 

Laminated pile assy (tail rotor head) 13.000 Flights 

Tail rotor transmission 1.800 Fh1 Input shaft (tail rotor transmission) 4.600 Fh 

Output shaft (tail rotor transmission) 4.600 Fh 

Short front shaft (tail rotor drive) 20.000 Fh 

Long shaft (tail rotor drive) 6.000 Fh 

Short rear shaft (tail rotor drive) 30.000 Fh 

Engine 3.000 Fh 

a.TBO extension program in progress 

Time Between Overhauls (TBO): 

The component in question must be removed at each interval that corresponds to the value indicated, 

in order to undergo the operations in a specialized workshop that will enable it to be put back into service 

for the next interval. A TBO is granted with a 10 % operational margin, limited at +300 hours. The 

given time limit may be exceeded by 3% of the respective interval. 

All subcomponents may have a Service Life limit, rated above the TBO limit. 

Service Life Limit (SLL): 

The service life limit is an airworthiness limit. The component in question must be removed from service 

when it reaches the limit indicated. 




7.4 EUROCOPTER DEUTSCHLAND GMBH ® Maintenance Support 

Programs 


EUROCOPTER DEUTSCHLAND GMBH ® offers its clients a comprehensive array of repair and overhaul 

services to ensure availability and costs control. This array of services ranges from basic OEM 

repair and overhaul services up to comprehensive Parts By the Hour (PBH) maintenance programs. 

The different services are each tailored for one different user profiles and demands, such as customers: 

• with a high number of flight hours, 

• with a low number of flight hours, 

• looking for immediate component availability, 

• that wish budget control, 

•... 

To respond to the different customers' demands EUROCOPTER DEUTSCHLAND GMBH ® offers the 

following flexible and modular services: 

• Classical Support 

• Standard exchange 

• Repair with guaranteed Turn Around Times (TAT) 

• Guaranteed Direct Maintenance Costs (DMC) 

• Unscheduled Maintenance Insurance Plan 

• Parts By the Hour service 

7.4.1 Classical Support 

The classical support consists of a comprehensive Initial Provisioning package to sustain aircraft operation. 

This package includes Spare Parts, Tools, Test Equipment, etc. 

The required level of operational availability determines the quantity and therefore the investment required. 

With this support package the customer bears the responsibility to procure the right mix and 

quantity of components and spare parts, to monitor their repair and to manage obsolescence. 

7.4.2 Standard Exchange 

The Standard Exchange consists in replacing a defective part with a serviceable and interchangeable 

part within 48 hours subject to availability. This service is available for equipment, blades and dynamic 

components. 

7.4.3 Repair with Guaranteed TAT 

EUROCOPTER DEUTSCHLAND GMBH ® offers for some components a repair with commitment on 

guaranteed TAT. When this lead time is exceeded for the repair, EUROCOPTER DEUTSCHLAND 

GMBH ® provides the customer with a standard part exchange delivery at the same price as agreed for 

the repair. 

7.4.4 Guaranteed DMC 

The Guaranteed DMC services offers guaranteed repair and overhaul TATs as well as guaranteed prices. 

This addition to the classical repair and overhaul enables the customer to best size its inventory. 

Price for this service is calculated per flight hour, thus enabling the customer to spread and predict both 

his scheduled and unscheduled maintenance expenses. The guaranteed DMC service is available for 

dynamic components, blades and basic equipment. 





7.4.5 Unscheduled Maintenance Insurance Plan (UMIP) 

With the UMIP, EUROCOPTER DEUTSCHLAND GMBH ® gives the customer the option to secure unscheduled 

maintenance costs while remaining responsible for the scheduled events (overhaul, life limited 

part replacement). Price for this service is calculated per flight hour. 

The UMIP service includes component unscheduled repairs and guaranteed parts replacement within 

24 hours through Standard Exchange based on a dedicated inventory. This service is available for dynamic 

components, blades and basic equipment. 

7.4.6 Parts By the Hour (PBH) 

The Parts By the Hour (PBH) service is a comprehensive program that offers and balances at the same 

time guaranteed maintenance costs, reduced inventory and minimized helicopter downtime. This service 

is intended for customers looking for total cost control and high level of aircraft readiness. Price 

for this service is calculated per flight hour. 

The PBH service includes component unscheduled repairs component overhauls as well as Life Limited 

Part replacement. Parts replacement is guaranteed within 24 hours FCA through Standard Exchange 

based on a dedicated inventory. This service is available for dynamic components, blades and 

basic equipment. 

7.5 Engine Maintenance Program 

Always looking to maximize your efficiency and reduce your costs, Turbomeca, the engine manufacturer 

has developed an improved service offering. 

Whatever the mission, wherever it may be, for business or pleasure, Turbomeca offers a range of services 

tailored to your needs. 

Turbomeca tailor-made services cover Standard Exchange, AOG and Warranty needs for total peace 

of mind in the air and on the ground. 

Among the maintenance packages proposed, Turbomeca developed specific maintenance packages, 

the Support By the Hour® coverages, as described hereafter. 

7.5.1 Standard Coverage: „Classic” SBH ® 

The "classic" Support by the Hour (SBH ® ) is a global support service offered to operators to enable 

them to maintain the best availability of their engines fleet through a contract arrangement paid by running 

hours. 

The Support by the Hour (SBH ® ) is operated mainly through Standard Exchange supported by Turbomeca 

dedicated Corporate Pool. 

7.5.2 Customized Coverage: SBH ® „Mission” 

The new service, Support By the Hour® Mission, offers a modular series of comprehensive service and 

engine management packages, whereby Turbomeca undertakes to guarantee its operator's engine 

availability and care. 

From basic engine support requirement to fully comprehensive range of additional services, three different 

types of packages are offered to operators: Pro, Prime and Privilege. 

Depending on mission constraints and needs the operator can choose between a series of options: 




7.5.3 Turbomeca Internet Web Site - TOOLS 


Turbomeca Operator On-Line Support (TOOLS site) is entirely dedicated to helping customers. With 

24/7 availability, operators can access important information when they want to, from where they want 

to, winning precious time and staying head. TOOLS at www.turbomeca-support.com 

7.5.4 Time Between Major Overhauls 

The initial TBO value of the ARRIEL 1E2 applicable to the engine / modules / accessories are: 

• Complete engine 3,000 hours or 15 years a 

• Module 01 (Accessory gearbox) On Condition 

• Module 02 (Axial compressor) 6,000 hours 

• Module 03 (Gas generator) 3,000 hours 

• Module 04 (Power turbine) 6,000 hours 

• Module 05 (Reduction gearbox) 3,000 hours 

• Fuel Control Unit 3,000 hours or 10 years a 

a. First occurs 

7.5.5 Life-Limited Parts (LLP) 

Certain components of the engine, failure of which is classified as a hazardous effect according to Engine 

Regulation, have service life limits expressed in cycles (reference flight cycle). They are known 

as critical Life-Limited Parts (LLP). 

The limited service life to which this term refers is the number of cycles that a critical life-limited part 

can run before having to be withdrawn from service. 

The Life-Limited Parts on the ARRIEL 1E2 are: 

• Axial compressor 14,000 cycles 

• Centrifugal impeller 14,000 cycles 

• Injection wheel 10,000 cycles 

•1 st stage HP turbine disc 10,000 cycles 

•2 nd stage HP turbine disc 10,000 cycles 

• Power turbine disc 10,000 cycles 





7.6 Training 

With more than 50 years of experience, the EUROCOPTER DEUTSCHLAND GMBH ® training centers 

provide the most comprehensive, coherent and highest standard helicopter training in the world for pilots 

and technicians, whether civilian or military. 

Qualification training, allowing operators to comply with regulatory requirements, and services training, 

more mission oriented and tailored to the customers' operational needs, are addressed. 

All training courses are established according to the relevant civil aviation authorities' requirements. 

The centers are approved by the relevant airworthiness authorities (EASA, FAA, DGAC, LBA, CAA…). 

We are certified ISO 9001: V2000 and regularly audited by independent organisms such as Véritas, 

AFAQ… 

EUROCOPTER DEUTSCHLAND GMBH ® training centers provide a wide range of courses and services, 

from basic training up to preparation for the most sophisticated civil and military missions. 

As part of the full range of services on offer, EUROCOPTER DEUTSCHLAND GMBH ® also plays an 

active role in helicopter pilot development through its Ab Initio programs. 

Centers are equipped with multimedia classrooms. This includes computers overhead projectors and 

state-of-the-art means such as Computer Aided Instruction (CAI), Computer Based Training (CBT). 

Some centers also have self-learning laboratories. 

EUROCOPTER DEUTSCHLAND GMBH ® has set up a network of 14 training centers. For detailed information 

refer to EUROCOPTER DEUTSCHLAND GMBH ® specific publication. 

7.7 Technical Publications 

EUROCOPTER DEUTSCHLAND GMBH ® provides all the technical publications necessary for safely 

operating and maintaining its aircraft cost effectively. 

EUROCOPTER DEUTSCHLAND GMBH ® technical publications are available on an interactive electronic 

medium or in hard copies. 

The INDOC CD-ROM includes the Aircraft Maintenance Manual (AMM), System Description Section 

(SDS), Master Servicing Manual (MSM), Illustrated Parts Catalogue (IPC) and the Wiring Diagram Manual 

(WDM). 

The Component Maintenance Manual (CMM) is available on CD-ROM or hard copy, depending on the 

vendor. 

Along with the INDOC CD-ROM, EUROCOPTER DEUTSCHLAND GMBH ® provides a hard copy of 

the Airworthiness and Technical Publication (Flight Manual, Pilots Check List, Master Servicing Manual 

…) as well as the Service Bulletin Catalogue. 

The CD ROM is available in English or French; it includes the latest information and is updated regularly. 




7.8 T.I.P.I. (Technical Information Publication on Internet) 

7.8.1 Description 


T.I.P.I. website is entirely dedicated to provide a real-time issuing service for the following publications: 

• Service Bulletin, Service Letter, Service Information, Technical Information Letter 

• List of Applicable Publications (LOAP) 

• Master Minimum Equipment List (MMEL) 

7.8.2 Main Features 

• Each time a publication is issued, the customer is automatically informed by an e-mail. 

• The download of the publication in pdf format is possible either directly from the e-mail or after logging 

on the T.I.P.I. website. 

• A keywords search tool is provided (aircraft family, type of publication, date of edition...). 

Address: www.eurocopter.com/services/technical publications/T.I.P.I. 

The publications are available in English, French or German depending on the case. 

• A small summary, already included in the e-mail, helps the customer to understand quickly the subject. 

• Small icons allow the customer to identify immediately the type of information received. 





8 List of Abbreviations 

Abbreviation Meaning 

ADC Air Data Computer 

ADF Automatic Direction Finder 

AE American Eurocopter 

AEO All Engines Operating 

AFCS Automatic Flight Control System 

AGL Above Ground Level 

AHRS Attitude Heading Reference System 

AM Amplitude Modulation 

AMM Aircraft Maintenance Manual 

ANR Active Noice Reduction 

AOG Aircraft On Ground 

CAA Civil Aviation Authority 

CAD Cautions and Advisory Display 

CAI Computer Aided Instruction 

CBT Computer Based Training 

CMM Component Maintenance Manual 

CMP Continuous Maintenance Program 

COM Cockpit Operating Manual 

CPDS Central Panel Display System 

CVFDR Cockpit Voice and Flight Data Recorder 

DA Density Altitude 

DAFCS Digital Automatic Flight Control System 

dB Decibel 

DC Direct Current 

DGAC Direction Générale de l‘Aviation Civile 

DMC Direct Maintenance Costs 

DME Distance Measuring Equipment 

DTU Data Transfer Unit 

EASA European Aviation Safety Agency 

ECMM Electronic Component Maintenance Manual 

EGPWS Enhanced Ground Proximity Warning System 

ELT Emergency Locator Transmitter 

EMS Emergency Medical Service 

FAA Federal Aviation Administration 

FCA Free Carrier 

FCDS Flight Control Display System 

FLI First Limit Indicator 

FLIR Forward Looking Infrared 





FMS Flight Manual Supplement 

FWD Forward 

GPS Global Positioning System 

HEEL Helicopter Emergency Egress Lighting 

HEMS Helicopter Emergency Medical Service 

HIGE Hover In Ground Effect 

HOGE Hover Out of Ground Effect 

HP High Pressure 

IBF Inlet Barrier Filter 

IC InterCommunication 

ICAO International Civil Aviation Organisation 

ICP Instrument Control Panel 

ICS Intercommunication System 

IFR Instrument Flight Rules 

ILS Instrument Landing System 

IPC Illustrated Parts Catalog 

ISA International Standard Atmosphere 

ITAR International Traffic in Arms Regulations 

JAR-OPS Joint Airworthiness Requirement - Opterations 

KIAS Knots Indicated Airspeed 

LBA Luftfahrt-Bundesamt 

LCD Liquid Crystal Display 

LH Left Hand 

LLP Life-Limited Part 

LOAP List Of Applicable Publication 

MCP Maximum Continuous Power 

MM Mast Moment 

MMEL Master Minimum Equipment List 

MSM Master Servicing Manual 

MTOW Maximum Take-Off Weight 

NAV Navigation 

ND Navigation Display 

NMS Navigation Management System 

NVG Night Vision Goggles 

OAT Outside Air Temperature 

OEI One Engine Inoperative 

OEM Original Equipment Manufacturer 

PA Pressure Altitude 

PBH Parts By the Hour 

PFD Primary Flight Display 







R/D Rate of Descent 

RAM Random Access Memory 

RCU Reconfiguration Unit 

RH Right Hand 

RPM Revolutions Per Minute 

SAS Stability Augmentation System 

SB Service Bulletin 

SBH ® Support By the Hour 

SDS System Description Section 

SL Sea Level 

SLL Service Life Limit 

STC Supplemental Type Certificate (FAA) 

TAS Traffic Advisory System 

TAT Turn Around Time 

TBO Time Between Overhaul 

TCCA Transport Canada Civil Aviation 

TQ Torque 

TOP Take-Off Power 

TOT Turbine Outlet Temperature 

UMIP Unscheduled Maintenance Insurance Plan 

UMS Usage Monitoring System 

VARTOMS Variable Rotor speed and Torque Matching System 

VBR Best Range Speed 

VDC Volt Direct Current 

VEMD Vehicle and Engine Multifunction Display 

VFR Visual Flight Rules 

VH Maximum Horizontal Speed 

VHF Very High Frequency 

VIP Very Important Person 

VMMS Vector Mast Moment System 

VNE Never-Exceed Speed 

VOR VHF Omnidirectional Radio Range 

VRU Video Radar Unit 

VTOL Vertical Take-Off and Landing 

VY Best Rate of Climb Speed 

W Watt 

WAAS Wide Area Augmentation System 

WDM Wiring Diagram Manual 




Blank

Table of content - Eurocopter

Create successful ePaper yourself

Delete template?

Save as template?