Technical Data - airbushelicoptersinc.com · Further safety aspects of the EC135 are design...

Technical Data

1 Foreword....................................................................................................................................................... 7

2 General characteristics ............................................................................................................................. 112.1 Exterior dimensions ............................................................................................................................. 11

2.2 Interior dimensions............................................................................................................................... 12

2.3 Possible cabin arrangement (seats & equipment as option)................................................................ 12

2.4 Weight.................................................................................................................................................. 13

2.5 Fuel Capacities .................................................................................................................................... 13

2.6 Engines................................................................................................................................................ 14

2.7 Main transmission ratings .................................................................................................................... 14

3 EC135 Baseline Aircraft Definition........................................................................................................... 15

4 Recommended Mission Configurations .................................................................................................. 194.1 EMS - Conventional Avionics............................................................................................................... 21

4.1.1 EMS - Conventional Avionics (Air Ambulance Technology) ................................................................................................. 224.1.1.1 Mission Parameter....................................................................................................................................................... 224.1.1.2 Basic Mission Configuration ........................................................................................................................................ 234.1.1.3 Further Available Equipment ....................................................................................................................................... 254.1.1.4 Performance Data ....................................................................................................................................................... 28

4.1.2 EMS - Conventional Avionics (Aerolite) ................................................................................................................................ 304.1.2.1 Mission Parameter....................................................................................................................................................... 304.1.2.2 Basic Mission Configuration ........................................................................................................................................ 314.1.2.3 Further Available Equipment ....................................................................................................................................... 344.1.2.4 Performance Data ....................................................................................................................................................... 37

4.1.3 EMS - Conventional Avionics (Bucher Leichtbau) ................................................................................................................ 394.1.3.1 Mission Parameter....................................................................................................................................................... 394.1.3.2 Basic Mission Configuration ........................................................................................................................................ 394.1.3.3 Further Available Equipment ....................................................................................................................................... 434.1.3.4 Performance Data ....................................................................................................................................................... 46

4.2 EMS - Glass Cockpit............................................................................................................................ 494.2.1 EMS - Glass Cockpit (Air Ambulance Technology) .............................................................................................................. 50

4.2.1.1 Mission Parameter....................................................................................................................................................... 504.2.1.2 Basic Mission Configuration ........................................................................................................................................ 514.2.1.3 Further Available Equipment ....................................................................................................................................... 544.2.1.4 Performance Data ....................................................................................................................................................... 57

4.2.2 EMS - Glass Cockpit (Aerolite) ............................................................................................................................................. 594.2.2.1 Mission Parameter....................................................................................................................................................... 594.2.2.2 Basic Mission Configuration ........................................................................................................................................ 604.2.2.3 Further Available Equipment ....................................................................................................................................... 634.2.2.4 Performance Data ....................................................................................................................................................... 66

4.2.3 EMS - Glass Cockpit (Bucher Leichtbau) ............................................................................................................................. 684.2.3.1 Mission Parameter....................................................................................................................................................... 684.2.3.2 Basic Mission Configuration ........................................................................................................................................ 684.2.3.3 Further Available Equipment ....................................................................................................................................... 724.2.3.4 Performance Data ....................................................................................................................................................... 75

4.3 Disaster Management.......................................................................................................................... 774.3.1 Disaster Management (Air Ambulance Technology) ............................................................................................................ 78

4.3.1.1 Mission Parameter....................................................................................................................................................... 78

135.09.101.01 Page 1 of 202This 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

Technical Data

4.3.1.2 Basic Mission Configuration........................................................................................................................................ 794.3.1.3 Further Available Equipment....................................................................................................................................... 824.3.1.4 Performance Data ....................................................................................................................................................... 85

4.3.1.4.1 Evacuation Mission (MEDEVAC)....................................................................................................................... 854.3.1.4.2 Search And Rescue Mission (SAR) ................................................................................................................... 874.3.1.4.3 Intervention Mission........................................................................................................................................... 89

4.3.2 Disaster Management (Aerolite)........................................................................................................................................... 914.3.2.1 Mission Parameter ...................................................................................................................................................... 914.3.2.2 Basic Mission Configuration........................................................................................................................................ 924.3.2.3 Further Available Equipment....................................................................................................................................... 954.3.2.4 Performance Data ....................................................................................................................................................... 98

4.3.2.4.1 Evacuation Mission (MEDEVAC)....................................................................................................................... 984.3.2.4.2 Search and Rescue Mission (SAR) ................................................................................................................. 1004.3.2.4.3 Intervention Mission......................................................................................................................................... 102

4.3.3 Disaster Management (Bucher Leichtbau) ......................................................................................................................... 1044.3.3.1 Mission Parameter .................................................................................................................................................... 1044.3.3.2 Basic Mission Configuration...................................................................................................................................... 1054.3.3.3 Further Available Equipment..................................................................................................................................... 1084.3.3.4 Performance Data ..................................................................................................................................................... 111

4.3.3.4.1 Evacuation Mission (MEDEVAC)..................................................................................................................... 1114.3.3.4.2 Search and Rescue Mission (SAR) ................................................................................................................. 1134.3.3.4.3 Intervention Mission......................................................................................................................................... 115

4.4 Corporate ........................................................................................................................................... 1174.4.1 Mission Parameter.............................................................................................................................................................. 1184.4.2 Basic Mission Configuration ............................................................................................................................................... 1184.4.3 Further Available Equipment .............................................................................................................................................. 1204.4.4 Material and color definition................................................................................................................................................ 1234.4.5 Performance Data .............................................................................................................................................................. 124

4.5 Executive............................................................................................................................................ 1274.5.1 Mission Parameter.............................................................................................................................................................. 1284.5.2 Basic Mission Configuration ............................................................................................................................................... 1284.5.3 Further Available Equipment .............................................................................................................................................. 1304.5.4 Material and color definition................................................................................................................................................ 1334.5.5 Performance Data .............................................................................................................................................................. 134

4.6 HERMÈS............................................................................................................................................ 1374.6.1 Mission Parameter.............................................................................................................................................................. 1384.6.2 Basic Mission Configuration ............................................................................................................................................... 1384.6.3 Further Available Equipment .............................................................................................................................................. 1404.6.4 Performance Data .............................................................................................................................................................. 141

4.7 Utility .................................................................................................................................................. 1434.7.1 Mission Parameter.............................................................................................................................................................. 1444.7.2 Basic Mission Configuration ............................................................................................................................................... 1444.7.3 Further Available Equipment .............................................................................................................................................. 1464.7.4 Performance Data .............................................................................................................................................................. 149

4.7.4.1 Maximum Range ....................................................................................................................................................... 149

4.8 Offshore - Oil and Gas ....................................................................................................................... 1514.8.1 Mission Parameter.............................................................................................................................................................. 1524.8.2 Basic Mission Configuration ............................................................................................................................................... 1524.8.3 Further Available Equipment .............................................................................................................................................. 1554.8.4 Performance Data .............................................................................................................................................................. 158

4.8.4.1 Radius of Action ........................................................................................................................................................ 158

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

Page 2 of 202 135.09.101.01

Technical Data

5 Further Product Information ................................................................................................................... 1615.1 News, highlights and main improvements ......................................................................................... 161

5.2 Avionics.............................................................................................................................................. 1635.2.1 VFR Solutions..................................................................................................................................................................... 1635.2.2 IFR with Conventional Instrumentation............................................................................................................................... 1645.2.3 IFR Solutions with Glass Cockpit (MEGHAS)..................................................................................................................... 164

5.3 Antenna layouts ................................................................................................................................. 1665.3.1 Typical VFR antenna layout................................................................................................................................................ 1665.3.2 Typical IFR antenna layout ................................................................................................................................................. 167

5.4 Police ................................................................................................................................................. 1685.4.1 Aircraft Parameter............................................................................................................................................................... 1695.4.2 Typical components of a police configuration..................................................................................................................... 169

5.5 Additional available equipment .......................................................................................................... 171

5.6 Equipment required to comply with JAR-OPS 3 ................................................................................ 171

6 Main Performance.................................................................................................................................... 173

7 Support information ................................................................................................................................ 1917.1 Assets ................................................................................................................................................ 191

7.2 Inspection Programm......................................................................................................................... 191

7.3 Main components............................................................................................................................... 193

7.4 Eurocopter Maintenance Support Programs...................................................................................... 1947.4.1 Classical Support ................................................................................................................................................................ 1947.4.2 Maintencance, Repair and Overhaul .................................................................................................................................. 1947.4.3 Standard Exchange ............................................................................................................................................................ 1957.4.4 Guaranteed DMC (Repair by the Hour) .............................................................................................................................. 1957.4.5 Unscheduled Maintenance Insurance Plan (UMIP) ............................................................................................................ 1957.4.6 Parts By the Hour (PBH)..................................................................................................................................................... 195

7.5 Engine Maintenance program............................................................................................................ 1967.5.1 Pratt & Whitney................................................................................................................................................................... 196

7.5.1.1 PW206B2 Mean Time Between Overhaul (MTBO)................................................................................................... 1967.5.1.2 Service Life Limited (SLL) Components.................................................................................................................... 197

7.5.2 Turbomeca.......................................................................................................................................................................... 1977.5.2.1 Time Between Major Overhauls ................................................................................................................................ 1987.5.2.2 Life Limited Parts (LLP) ............................................................................................................................................. 198

7.6 Training .............................................................................................................................................. 199

7.7 Technical publications........................................................................................................................ 200

7.8 T.I.P.I. (Technical Information Publication on Internet)...................................................................... 2017.8.1 Description.......................................................................................................................................................................... 2017.8.2 Main features ...................................................................................................................................................................... 201

135.09.101.01 Page 3 of 202This 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

Technical Data

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Technical Data

Manufacturer´s notes - ATTENTION!

EUROCOPTER®s policy is one of on-going product enhancement which means that alterationsin definition, pictures, weights, dimensions or performance may be made at any time without noticebeing 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 aprior check as to its validity and prior written agreement of EUROCOPTER®.

The operational or certification regulations, as defined by the local authorities, can make compul-sory 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 theequipment not specifically related to the helicopter (for example: life jacket) or necessary for par-ticular missions (for example: supplemental oxygen). The operator is responsible for ascertainingwith his local authorities that the planned configuration of the helicopter complies with regulatoryrequirements 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.

135.09.101.01 Page 5 of 202This 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 2009

Technical Data

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Page 6 of 202 .09.100.

Technical Data

1 Foreword

The EC135 is a light twin-engine, multi-purpose helicopter of the 2-3 ton class with up to 8 seats forpilot/s and passengers. Underlining its multi-role capabilities, it can even be operated single pilot IFRas an option. The helicopter combines EUROCOPTER®'s latest Technologies, like advanced cockpitdesign, modern avionics, Fenestron® anti-torque-device and all-composite bearingless main rotor sys-tem, giving the helicopter an outstanding maneuverability. Optimized main rotor blades with advancedtip geometry in combination with a Fenestron® with unequal blade spacing make the EC135 the quie-test helicopter in its class, bringing it 6.5 DBA below the ultra-stringent ICAO limit. The built-in anti re-sonance isolation system (ARIS) filters rotor-induced vibrations and thus enhances flying comfort to amaximum. As a result, the vertical vibration level is far below 0.1g at hover with no increase with speed.

Due to its extreme simplicity, the rotor system contributes to highest safety standards and, at the sametime, reduces maintenance to a minimum. The first scheduled maintenance is the intermediate inspec-tion after 400 Flh. In addition, the rotor system together with high TBO gearbox and airframe compo-nents grant for high in-service-time of the helicopter.

Depending on the operator's preferences, the EC135 can be equipped with either Arrius 2B2 or Pratt& Whitney PW206B2 power plants - both are FADEC controlled. These powerful and reliable enginesin combination with the lifting system provide outstanding performance and vital power reserves evenin OEI scenarios.

For training purpose an OEI training mode is implemented to perform a realistic OEI training. This trai-ning mode is based on a twin engine training concept featuring a so called TRAINING and a TRAININGIDLE engine.

Twin-engine reliability is complemented by a tandem hydraulic and dual electrical system as well as aredundant lubrication and cooling system for the main transmission.

Further safety aspects of the EC135 are design elements like energy absorbing fuselage and seats,as well as the crash resistant fuel cells.

A wide range of quick interchangeable optional equipment is available for the EC135, e.g. emergencyfloats, hoist, SX16 search light, single or dual cargo hook and many more. Together with its most ver-satile cabin layout the EC135 is ready to operate in different missions, like police / surveillance, pas-senger / VIP transport, EMS, public service, to highlight on a few.


Technical Data

Compared to other helicopters in its class, the EC135 offers a large cabin, featuring:• Excellent outside visibility for pilots and passengers• Roomy cabin which accommodates long or bulky freight• Unrivalled side loading (no door posts) and rear lodading capability• Unobstructed and flat floor all over the cabin area with integrated airline rails

Alternatively to a conventional cockpit, the EC135 is available with "glass cockpit", which comprisesprimary flight displays (PFD) and NAV displays (ND). All LCD screens are well arranged on the instru-ment panel, easy to read even if viewed from an angle and feature perfect readability in any light con-ditions. The unique color coding, warning and information concept helps the pilot/s to collect all relevantparameters while suppressing presentation of non-relevant information.

Common to the conventional and the glass cockpit is the Central Panel Display System (CPDS). Inclu-ded in this CPDS there is Eurocopter's unique first limit indicator (FLI) which dramatically simplifies en-gine and torque monitoring. Being relieved from the instrument scan without missing vital information,the pilot/s can dedicate more of his/their attention to the mission.


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Technical Data

Conventional Instrumentation (analog instruments)

Glass Cockpit Instrumentation (MEGHAS / FCDS)


Technical Data

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2 General characteristics

2.1 Exterior dimensions


Technical Data

2.2 Interior dimensions

2.3 Possible cabin arrangement (seats & equipment as option)

Passenger transport

Floor area Volume

Cabin & baggage compartment 4.35 m² 46.83 ft² 4.90 m³ 173.04 ft³

Cockpit (pilot side) 1.15 m² 12.38 ft² 1.00 m³ 35.31 ft³

Total (undivided) 5.50 m² 59.21 ft² 5.90 m³ 208.35 ft³

Table 2.1: Interior Dimensions

Pilots Passengers

Standard 1 6 / 7

2 5 / 6

Corporate 1 (5) / 6 / (7)

2 (4) / 5 / (6)

Executive 1 5 / (6)

2 4 / (5)

Hermès 1 5

2 4

Table 2.2: Seat capacity of the different passenger transport mission configurations.


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Technical Data

EMS Missions• 1 pilot + 1 litter + up to 4 seats for doctor and attendants• 1 pilot + 2 litters + up to 3 seats for doctor and attendants• 2 pilots + 1 litter + up to 3 seats for doctor and attendants• 2 pilots + 2 litters + up to 2 seats for doctor and attendant

Freight transport• 1 pilot + 4.9 m³ (173.04 ft³) in cabin and cargo compartment

2.4 Weight

2.5 Fuel Capacities

Note: Tolerance of fuel figures: +/- 2%; Fuel density used is 0.8 kg/liter

Note: margin +/- 1.5% kg lb

• Empty weight, wet (in standard aircraft configuration) 1,455 3,208

• Useful load (for standard aircraft configuration) 1,455 3,208

• Pilot 80 176

• Payload and / or fuel 1,375 3,031

• Maximum take-off weight 2,910 6,415

Table 2.3: Weight

Useable Fuel Unuseable Fuel

lb kg l lb kg

• Main Tank 1038.6 471.1 588.9 7.5 3.4

• Supply Tank 196.8 89.3 111.6 9.3 4.2

• Total 1235.4 560.4 700.5 16.8 7.6

Table 2.4: Fuel Capacities


Technical Data

2.6 Engines

2 Pratt & Whitney turbine engines - PW206B2or2 Turbomeca turbine engines - ARRIUS 2B2

Engine ratings

2.7 Main transmission ratings

Thermodynamic limits per engine at SL, ISA kW ch shp

PW206B2

• One Engine Inoperative (OEI), 30 sec power 609 828 816

• One Engine Inoperative (OEI), 2.0 min power 580 789 777

• One Engine Inoperative (OEI), MCP 528 718 708

• Take-Off Power (TOP) 498 677 667

• Maximum Continuous Power (MCP) 457 621 612

ARRIUS 2B2

• One Engine Inoperative (OEI), 30 sec power 609 828 816

• One Engine Inoperative (OEI), 2.0 min power 580 789 777

• One Engine Inoperative (OEI), MCP 528 718 708

• Take-Off Power (TOP) 473 643 634

• Maximum Continuous Power (MCP) 442 601 592

Table 2.5: Engine ratings

Single engine operation kW ch shp

• 30 sec OEI power 1 x 526 1 x 715 1 x 705

• 2.0 min OEI power 1 x 513 1 x 698 1 x 687

• Maximum continuous OEI power 1 x 368 1 x 501 1 x 493

Twin engine operation

• Take-Off Power 2 x 320 2 x 435 2 x 429

• Maximum Continuous Power (MCP) 2 x 283 2 x 385 2 x 380

Table 2.6: Main transmission ratings


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3 EC135 Baseline Aircraft Definition

GENERAL• Energy absorbing fuselage• Tail boom with fixed horizontal stabilizer and two end-plates• Vertical fin with faired-in Fenestron ®• Upper deck with fittings for main gearbox, engines, hydraulic and cooling system• Cowlings for main transmission and engine• Skid-type landing gear with skid protectors, capable of taking ground-handling wheels• Long boarding steps, LH and RH Maintenance built-in steps and grips• Exterior painting (single color)

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 automatic locking system• Cabin boarding grips (LH and RH)• Interior paneling with integrated basic sound insulation• Flight controls (pilot side)• Engine controls with manual engine back-up system at pilot's collective pitch lever• Instrument panel with extension on pilot's side and glare shield• Ram-air and electrical ventilating system for cockpit and cabin• Headset holder in the cockpit• Headset holder in the cabin• Portable fire extinguisher• Stowage net for first aid kit at the LH rear clam-shell door• Flash light (torch)• 4 Mobile tie-down rings

BASIC INSTRUMENTATION• Central Panel Display System (CPDS), consisting of:

• Caution Advisory Display (CAD) with indication of:• Caution and advisory information• Fuel quantity indication

• Vehicle and Engine Monitoring Display (VEMD) with indication of:• Torque• Engine parameters (N1-RPM (for P&W) or ΔN1-RPM (for TM), oil pressure, oil temperature,

Turbine Outlet Temperature (TOT), engine/FADEC rep EEC failure and parameter codemessages, self diagnoses)

• FLI (First Limit Indicator) for TQ, TOT, N1 (for P&W) or ΔN1 (for TM) as analogue display• Main transmission parameters (oil pressure, oil temperature)• Dual ammeter (generator)


Technical Data

• Ammeter (battery)• Dual voltmeter• Outside Air Temperature (OAT)• Parameters of optional equipment (e.g. internal long range fuel tank)• Engine cycle counter (on flight report page)• Clock (2")• Magnetic compass• Triple (rotor and engines) RPM-indicator (2")• Standard instruments: (single pilot)1

• Airspeed indicator (3")• Encoding altimeter (3")• Vertical speed indicator (3")

• Warning unit:• Engine fire warning with fuel emergency shut-off• Warning lights• Aural warning

• Main switch panel:• DC power control• Digital engine control (FADEC)

• Pitot / static system with electrical heated pitot tube, pilot side• Static pressure crossover system.• Air Data computer

POWER PLANT• Two PRATT & WHITNEY PW206B2 turbine engines or

Two TURBOMECA ARRIUS 2B2 turbine engines These 2 engines are equipped with:

• fire detectors• electronic engine control (FADEC-BOX)• chip detectors with quick-disconnect plugs• overspeed protection system • twin-engine OEI-training mode• Oil cooling and lubricating system with thermostatic valve• Crash resistant fuel system with a flexible bladder-type fuel main tank and supply tank (split into

two sections)• Automatically controlled variable rotor speed system• Fuel tank filler flap, lockable

TRANSMISSION SYSTEM• Flat-shaped main gearbox with two stages• Chip detector system with quick-disconnect plug (main gearbox)• Redundant oil cooling and lubrication system• Main gearbox attachment with Anti-Resonance Isolation System (ARIS)• Free wheel assemblies in the engine input drives• Tail rotor drive shaft• Tail rotor gearbox with splash lubrication and oil level sight gauge• Chip detector system with quick-disconnect plug (tail rotor gearbox)

1.If glass cockpit instrumentation is chosen as optional equipment, these standard instruments are deleted and an altimeter (2‘‘)and an airspeed indicator (2‘‘) as back-up instruments are added.


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Technical Data

ELECTRICAL INSTALLATIONTwo starter/generators (2 x 160 A, 28 VDC)• Nickel-Cadmium battery, (24 V, 17 Ah)• External power connector (STANAG 3302)• Power distribution system:

• Two primary busbars• Two shedding busbars• Two essential busbars• Two high load busbars (80 A) - for optional equipment only• Two high power busbars (200 A)

• Battery bus• One utility receptacle in LH side of cargo compartment (28VDC, 10A)• Lighting:

• Anti-collision warning light (red flashing)• Fixed, nose-mounted landing light (250 W)• Three position lights (red, green, white)• Adjustable instrument lighting• One utility light in the cockpit• 5 spot-lights in the cabin • One light in cargo compartment RH side

ROTOR AND FLIGHT CONTROLS• Bearingless Main Rotor system (BMR), consisting of:

• Rotor head/mast in one piece• Four fiber-reinforced composite main rotor blades with anti-erosion strips, control cuff, elastome-

ric lead-lag dampers and special blade tip painting• Main rotor control system with dual hydraulic boost system• Electrical trim system (cyclic)• Basic provisions for an easy integration of a track and balance system• Fenestron®-type tail rotor with ten metal blades (asymmetric blade spacing) and stator• Tail rotor gearbox cover• Tail rotor control system with flexball cable and single hydraulic booster• Yaw-SAS (Stability Augmentation System)• Mast moment system

GROUND HANDLING KIT1

• Two ground-handling wheels• Basic aircraft covers (short time)• Main rotor blade tie-down lash bags• Oil drain hoses• Fuel tank drain device• Keys for cockpit doors, cabin doors, baggage compartment doors and tank flap (one-key system)• Battery key• Lifting points

1.Weight not included in the standard helicopter empty weight


Technical Data

DOCUMENTATION (in English)• One Flight Manual1 • One Pilots-Checklist, revision service for five years2

• One Logbook2 (only paper, CD ROM on demand)• One Historical Record1 (only paper, CD ROM on demand)• One CD-ROM1 2 including AMM3, SDS3, WDM3, MSM, IPC• One additional Master Servicing Manual (MSM)1 2 on paper• One Service Bulletin Catalogue (SB)1 2 per contract, on paper• One List Of Applicable Publications (LOAP)1 2 on paper• One Avionics Manual (if avionics equipment is installed by EUROCOPTER®)2 3 on paper• Engine Documentation2, furnished by supplier, including:

• Maintenance Manual• Illustrated Parts Catalogue (IPC)

• Service Bulletins

1.Revision service included as long as the aircraft is operational2.Weight not included in the standard helicopter empty weight3.Customized documentation


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Technical Data

4 Recommended Mission Configurations

EUROCOPTER® proposes the following „favorite” mission configurations for the EC135. The createdpackages should be regarded as a first proposal to provide the customers with a first overview and togive a first impression about the EC135 and its multiple features.

Available mission configurationsThe following recommended mission configurations are available:• EMS - Conventional Cockpit• EMS - Glass Cockpit• Disaster Management• Corporate• Executive• Hermès• Utility• Offshore

The above listed configurations show a maximum level of compliancy. All EMS and Disaster Manage-ment mission configurations are available with STC kits from Air Ambulance Technology, Aerolite orBucher Leichtbau.

General StructureAll proposed packages consist of two parts: 1. Basic Mission Configuration2. Further Available Equipment

The first part contains mandatory options coming from flight regulations plus options which are highlyrecommended regarding the mission operation.

The second part provides a variety of options which can be added to customer‘s choice on top of therespective Basic Mission Configuration.

General rules for adding options to the Basic Mission ConfigurationSome simple rules have to be considered when adding options from the Further Available List to theBasic Mission Configuration:• Only options from the respective Further Available Equipment list may be added to the configuration.

Mixing options of different Further Available Equipment lists could lead to product incompatibilities.Therefore it has to be checked individually by EUROCOPTER®.

• Detachable parts require always the relevant fixed provisions.• Only one option (out of the several possibilities of the respective Further Available Equipment list)

can be selected for each following specific category:• External hoist• Sliding door fastener (for each side of the helicopter)• Lashing points• Stretcher type• Headsets• Headset adapter cable crew• Headset adapter cable pax


Technical Data

Performance CalculationAll performance mission calculations data used in this document is for information purpose only andEUROCOPTER DEUTSCHLAND GmbH takes no responsibility for the correctness of this informationas far as the applicability to the receiving party’s individual case is concerned. The present use of thenamed data shall not be construed as expressly or impliedly granting the receiving party any rights norbe deemed to constitute any kind of obligation or commitment of EUROCOPTER DEUTSCHLANDGmbH.

Further individual configurations / equipmentChapter 5 gives an overview of the modular avionics solutions possible for the EC135. In addition itprovides general information regarding further available equipment or solutions which are available onrequest. Typical police mission equipment and associated features can be found in chapter 5.4 Police.

The EC135 is the reference helicopter with its wide breadth of available options. This document showsa synopsis of the whole capability of this aircraft. If any mission equipment cannot be found in the tech-nical data please do not hesitate to contact EUROCOPTER® to receive further information.


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Technical Data

4.1 EMS - Conventional Avionics

With a lightweight conventional cockpit layout, compact outside dimensions, excellent outside visibilityfor VFR flights as well as a modular, flexible cabin arrangement, the EC135 is the most successful he-licopter for EMS missions in its class. It is also the quietest: the external noise level-below the strictestregulatory specifications-allows for operation in close approach to hospitals, which are often situatedin highly populated areas. Loading and unloading is carried out quickly and easily on either side or atthe rear, through the extra-large sliding doors or rear clamshell doors. Even during winching opera-tions, patients can be easily transferred into the hovering helicopter.

The EC135's skid landing gear along with its very compact design make it possible to land in very con-fined areas or unprepared terrains, wherever the injured are awaiting precious help. The high-set mainrotor and patented Fenestron® tail rotor ensure that the crew can work safely in the area of the rearclamshell doors while rotors are running, and in comfort: The helicopter provides ample room for up tofour crew members-a pilot, a doctor and one or two paramedics-as well as a patient. A second stretchercan be installed within seconds.

Ready for mission

All presented EMS - Conventional cockpit configurations include a complete EMS kit. All kits are fullyequipped with stretcher, medical seats and floor, cabinet, oxygen system, electrical and lighting sys-tem, as well as medical apparatuses and further mission equipment (e.g. rescue rucksack, vacuummattress, etc.).

Figure 4.1: EC135 landing in hostile environment


Technical Data

4.1.1 EMS - Conventional Avionics (Air Ambulance Technology)The EMS Kit including state of the art medical devices is designed for rescue, ambulance and neonatalair medical missions. The complete system is fitted to the available attachments on the helicopter floor.No modification to the helicopter structure is required. The easy and quick installation can be done wi-thin 25 minutes.

4.1.1.1 Mission Parameter

Flight Rules: VFR (Night)Instrumentation: ConventionalCat-A: Yes

Figure 4.2: EMS Kit - Air Ambulance Technology STC

Pilots 1 or 2

Medics 2

Patient 1


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Technical Data

4.1.1.2 Basic Mission Configuration

Baseline Aircraft

Subtotal: 1,455.0 3,208.31,5% Weight margin: 21.8 48.1

Subtotal (incl. margin): 1,476.8 3,256.4

General Equipment

Mission Equipment

Qty DocRef ComRef Title Weight[kg]

Weight[lb]

1 00-10002-A L0000-002-00 EC135 Baseline Aircraft 135.09.100.01 E 1,455.0 3,208.31 L0000-003-01 2 Turbomeca ARRIUS 2B2 turbine engines 0.0 0.01 L0000-003-02 2 Pratt & Whitney PW206B2 turbine engines 0.0 0.0


Weight[lb]

1 05-02016-C L1111-002-00 Two-color exterior painting instead of single color painting 1.5 3.31 05-03007-C L2562-001-00 First aid kita

a.First aid kit complies with german regulation rules 1. DV LuftBO paragraph 5(2). Type of operation, procedures or regulationsmay require a different/specific first aid kit.

1.5 3.31 05-12001-B L5232-001-00 Multifunction handle on the main gear box cowling (LH and RH) 0.6 1.31 05-22007-B L7924-001-00 Fuzz burners for engines 1.2 2.61 05-22008-C L2621-001-00 Engine fire extinguishing system 3.6 7.91 05-22014-A L5371-001-00 Engine outlet heat protection 1.2 2.61 05-30003-A L2565-002-00 Flash light copilot side 0.2 0.41 05-31025-B L5211-002-00 Sliding windows in sliding doors 1.9 4.21 05-31026-C L2514-002-00 Tinted sun shades for cockpit windshield roof section 1.9 4.21 05-31027-B L5633-001-10 Window in clam-shell door, LH 0.8 1.81 05-33001-B L3113-001-00 Slant panel 0.8 1.81 05-33002-B L3113-004-00 Center console 2.2 4.91 05-34002-B L2576-001-00 Avionics compartment 4.2 9.31 05-37016-C L6701-001-00 Copilot flight controls 6.0 13.21 05-38010-B L3111-001-00 10" copilot instrument panel with glare shield 2.9 6.41 05-39006-B L2514-003-01 Map case in copilot door 0.5 1.11 05-41004-C L2104-003-00 Bleed air heating system: EMS-version 7.0 15.41 05-61010-B L2433-003-00 Battery, type "Saft", ULM, 27 Ah, 24 V

instead of standard battery8.2 18.1

1 05-62010-C L2420-003-00 Dual AC system (2 x 350VA) 6.6 14.61 05-63003-B L2432-001-00 Starter/generator (2 x 200 A, 28V DC)

instead of standard generator3.6 7.9

1 05-71001-C L6351-002-00 Rotor brake system 5.3 11.7


Weight[lb]

1 06-11021-B L3274-001-10 Settling protectors, fixed provisions 1.9 4.21 06-11021-B L3274-001-20 Settling protectors, detachable parts 7.9 17.41 06-45023-B L3343-003-00 Landing & search light, 450 W 3.1 6.81 06-65004-B L2625-003-00 2nd portable fire extinguisher 2.8 6.21 06-66009-B L3322-001-00 Boarding step illumination 0.2 0.41 06-67044-B L2563-801-06 ELT C406-N HM (Artex) incl. NAV. opt. 3.3 7.3


Technical Data

Interior Layout

Avionics


Weight[lb]

1 07-30013-B L2524-002-00 Separation curtain for cockpit / cabin 2.1 4.61 07-40005-B L2513-200-00 Washable floor covering for cockpit 3.9 8.61 07-50025-C L5211-004-00 Securing device for complete opening of cockpit doors 0.8 1.81 07-50026-B L5231-001-00 One-hand latching system for clam-shell doors 1.0 2.21 07-50027-B L5231-002-00 Extended opening fasteners for clam-shell doors 0.3 0.71 07-70044-A AAT-30100-002-2 EMS Kit - Air Ambulance Technology (AAT) 200.0 441.01 Medical Floor (Universal) - AAT1 Stretcher "Blue Mattress", LH - AAT1 Medical Seat slidable, aft RH - AAT1 Medical Seat slidable & swivelling, front RH - AAT1 Medical Cabinet with 3 drawer, front center - AAT1 Medical Equipment Carrier, aft LH - AAT1 Retainer for Corpuls C3 - AAT1 Retainer for Corpuls C3 (only monitor) - AAT1 Retainer for Medumat Transport - AAT2 Retainer for Perfusor Space - AAT1 Retainer for Compact Suction Unit 3 - AAT1 Oxygen Station 3x3,0 lt. 200 bar, front RH - AAT1 Accessories - AAT1 Installation, Certifcation & Documentation - AAT3 Aluminium Oxygen Bottle 3,0 lt. - AAT1 Monitor & Defibrillator Corpuls C3 - GS1 Respirator Medumat Transport - Weinmann1 Suction Pump Compact Suction Unit 3 - Laerdal2 Infusion System Perfusor Space - Braun1 Blood Glucose Meter Omnitest Plus - Braun1 Respiration Backpack incl. contents - Weinmann1 Emergency Backpack incl. DIN13232-N contents - Weinmann1 Cervical Collar Set Perfit ACE & Mini Perfit ACE - Ambu1 Vacuum Mattress - Tyromont1 Rescue Bag with internal belt system - Tyromont


Weight[lb]

1 08-00028-A L2300-001-05 Av Pack SP VFR 41.2 90.81 Digital Audio Control System (NAT), incl. AMU50, ACP53

pilot and copilot1 Transponder (Mode S) GTX 330 (Garmin)1 Avionics/Radio master switches (Special EUROCOPTER®)1 "GPS/NAV/COM GNS 430 (Garmin), pilot,

incl. annunciator/switch MD 41"1 4'' Artificial horizon GH14-391, pilot (Honeywell)1 Gyro Magnetic Heading System KCS 55 A (Honeywell)

incl. KG-102A, KMT-112, KA-21B with HSI KI-525A, pilot1 AV Pack SP VFR, interconnection / wiring1 08-12036-B L4322-090-04 Fixed provisions for tactical radio (antenna, power supply,

ICS interface)2.2 4.9

1 08-16061-A L2341-193-40 Digital Audio Control System ACP53 (NAT), PAX 3.6 7.91 08-21014-C L3441-090-04 Radar altimeter KRA 405 B (Honeywell) 3.5 7.71 08-21014-C L3441-092-03 Radar altimeter indicator KNI 416 (Honeywell) 1.2 2.61 08-51012-A L3425-091-02 4" artificial horizon GH14-391 (Honeywell), copilot 2.5 5.5


Page 24 of 202 135.09.101.01

Technical Data

Subtotal: 363.2 800.93% weight margin: 10.9 24.0

Subtotal (incl. margin): 374.1 824.9

Total: 1,850.9 4,081.3

4.1.1.3 Further Available Equipment

General Equipment

1 08-51013-B L3425-806-51 2” stand-by horizon AI 804 DC (Goodrich), with emergency battery

6.6 14.6

1 08-52010-A L3421-091-02 2nd directional Gyro (3” unslaved indicator) 205 1BL on copilot side (Goodrich)

1.4 3.1

1 08-54001-C L3411-001-00 Copilot pitot static system 1.5 3.31 08-60003-A L3412-002-00 Copilot 3" instruments (airspeed indicator, altimeter,

vertical speed indicator; United Instruments)1.7 3.7

1 08-61010-B L3166-091-04 RMI KI 229 (Honeywell), copilot 2.2 4.91 08-61011-A L3167-091-02 CDI KI 204 (Honeywell), copilot 1.0 2.21 08-71002-C L2217-001-10 VFR SAS (VFR pitch/roll Stability Augmentation System) 5.6 12.3


Weight[lb]


Weight[lb]

1 05-12002-B L2551-003-00 Additional 4 tie-down fittings for airline attachment rails 0.6 1.31 05-21015-B L8541-001-10 Wire strike protection system, fixed provisions 3.3 7.31 05-21015-B L8541-001-20 Wire strike protection system, detachable partsa

a.The protective capability is degraded with the simultaneous fitment of: cargo hook mirror, radar radome.

8.2 18.11 05-22014-A L5611-002-00 Tinted front windshields 1.2 2.61 05-23006-B L7165-002-00 Engine compressor wash kit 3.2 7.11 05-25016-D L7161-001-10 Sand filter system, fixed provisions 11.3 24.91 05-25016-D L7161-001-20 Sand filter system, detachable parts 26.2 57.81 05-26012-B L1241-001-00 Anti-corrosion protection 5.2 11.51 05-31026-C L5621-001-00 Tinted window for cockpit doors 0.0 0.01 05-31045-A L5211-001-11 Lockable sliding window in copilots' door 0.1 0.21 05-31045-A L5211-001-12 Lockable sliding window in pilots' door 0.1 0.21 05-31086-A L5211-002-01 Ram air deflectors sliding doors 0.4 0.91 05-31098-A L5211-001-01 Ram air deflectors cockpit doors 0.6 1.31 05-32007-B L3042-001-00 Windshield wiper system 5.0 11.01 05-34003-B L2576-002-00 Dampers for avionics compartment 1.8 4.01 05-37017-B L6721-001-00 Covers for copilot flight controls -2.5 -5.51 05-39007-B L3111-001-10 Map cases on instrument panel glare shield 0.6 1.31 05-39008-B L3113-004-10 Illuminated chart holder for pilot side 1.0 2.21 05-39008-B L3113-004-20 Illuminated chart holder for copilot side 0.9 2.01 05-42041-A L2105-005-00 Air conditioning system 55.0 121.31 05-85008-C L2843-001-00 Fuel management system (Fuel flow meters) 1.2 2.61 05-92009-B L6611-001-10 Main rotor blade folding: basic kit 1.3 2.91 05-92009-B L6611-001-20 Main rotor blade folding: fixed provisions for ground

handling kitb

b.Requires L6611-001-10 Main rotor blade folding: basic kit.

0.8 1.8

1 05-92009-B L6611-001-30 Main rotor blade folding: ground handling kit 0.0 0.01 05-93007-C L8544-002-00 Lashing points (wind speeds up to 100 kts) 0.7 1.51 05-93008-B L8544-001-00 Lashing points (wind speeds up to 40 kts) 2.4 5.31 05-95001-C L1321-001-00 Cover kit for helicopter GSE GSE1 05-97001-C L6201-001-30 Accelerometers for Track and Balance system 0.0 0.01 05-97002-C L6201-002-10 Optical tracker (Chadwick Helmuth), fixed provisions 0.1 0.21 05-97002-C L6201-002-20 Optical tracker (Chadwick Helmuth), detachable parts 0.7 1.5


Technical Data

Mission Equipment

Interior Layout

Avionics


Weight[lb]

1 06-11022-C L3272-001-10 Snow skids, fixed provisions 0.9 2.01 06-11022-C L3272-001-20 Snow skids, detachable partsa

a.No simultaneous fitment with settling protectors.

21.9 48.31 06-21017-C L8512-001-10 External hoist LH, fixed provisions 8.6 19.01 06-21017-C L8512-001-20 External hoist 50m, detachable parts

(incl. 1 week winch operator training)59.2 130.5

1 06-21017-C L8512-001-21 External hoist 90m, detachable parts (incl. 1 week winch operator training)

62.7 138.3

1 06-26011-C L8511-002-10 Cargo hook mirrors RH, fixed provisions 0.8 1.81 06-26011-C L8511-002-20 Cargo hook mirrors RH, detachable parts 3.9 8.61 06-27022-B L8511-005-10 Dual cargo hook system, fixed provisions 4.3 9.51 06-27022-B L8511-005-20 Dual cargo hook system, detachable parts 21.5 47.41 06-27027-A L8511-003-10 Cargo hook weighing system, fixed provisionsb

b.Requires L8511-005-10 Dual cargo hook system, fixed provisions.

0.2 0.41 06-27027-A L8511-003-20 Cargo hook weighing system, detachable parts 1.5 3.31 06-31012-B L8531-001-00 External loudspeaker system with siren 11.5 25.41 06-46001-B L3344-001-00 Strobe lights, white 1.4 3.11 06-61015-B L3215-001-10 Emergency floats, fixed provisions 7.8 17.21 06-61015-B L3215-001-21 Emergency floats, detachable parts 64.6 142.41 06-65002-B L2566-001-00 Emergency hammer 0.2 0.4


Weight[lb]

1 07-15016-B L2512-003-10 Height adjustable pilot seat instead of standard pilot seat 1.8 4.01 07-15016-B L2512-003-20 Height adjustable copilot seat instead of standard copilot seat 1.8 4.01 07-30012-B L2581-001-00 Enhanced sound proofing kit 4.8 10.61 07-50028-A L5213-001-11 Sliding door fastener, intermediate and max. position, LH 1.0 2.21 07-50028-A L5213-001-12 Sliding door fastener, max. position, LH 0.4 0.91 07-50028-A L5213-001-21 Sliding door fastener, intermediate and max. position, RH 1.0 2.21 07-50028-A L5213-001-22 Sliding door fastener max. position, RH 0.4 0.91 07-50034-B L5212-001-00 Jettisonable cockpit doors 1.2 2.61 07-50036-B L2514-012-00 Covers for sliding door fairing LH/RH 0.1 0.21 07-50039-B L5211-010-00 Door catch system for cockpit doors 0.1 0.21 07-50039-B L5211-011-00 Door catch system for sliding doors 0.2 0.41 07-60014-B L2514-013-00 Map case in sliding doors LH/RH 1.4 3.1


Weight[lb]

1 08-10021-A L2314-090-15 HF communication system HF9000 (Rockwell Collins), fixed provisions

7.3 16.1

1 08-10021-A L2314-090-25 HF communication system HF9000 (Rockwell Collins), detachable parts

20.5 45.2

1 08-15028-B L2319-002-41 Fixed provisions for GSM phone (antenna, 28V DC, interface to ICS)

0.5 1.1

1 08-15523-A L2315-092-02 IRIDIUM satellite communication and tracking system Flightdeck (SkyConnect),

7.7 17.0

1 08-16061-A L2341-006-63 Voice alert generation for DACS (NAT) 0.0 0.01 08-25014-A L3169-092-02 Distance Measuring Equipment DME indicator KDI 572

(Honeywell)0.8 1.8

1 08-25014-A L3455-092-03 Distance Measuring Equipment DME KN 63 (Honeywell)a 2.0 4.4


Page 26 of 202 135.09.101.01

Technical Data

Headsets and Adapter cableIn any case EUROCOPTER® adapter cables are required to connect any type of headset or helmet tothe aircraft intercom system. Furthermore EUROCOPTER® provides different headset types for cus-tomer‘s choise.

Required adapter cables for the above listed Headsets (L2315-001-10 - L2315-001-72):

Required items for the above listed Headset (L2315-001-73):

1 08-26010-B L3431-092-02 Marker beacon receiver/lights KR 21 (Honeywell) 0.9 2.01 08-35007-B L3442-881-00 TAS 620 (Avidyne) interface with GNS430 0.2 0.41 08-35007-C L2327-001-01 Traffic Advisory System TAS 620 (Avidyne)b 9.5 20.91 08-43018-B L3442-091-00 GPS/NAV/COM GNS 430 (Garmin), copilot,

incl. annunciator/switch MD 41 (MidContinent)c8.3 18.3

1 08-61011-A L3167-091-01 CDI KI 206 (Honeywell), copilot instead of CDI KI 204d 0.0 0.0

a.Requires L3169-092-02 Distance Measuring Equipment DME indicator KDI 572 (Honeywell)b.Requires L3442-881-00 TAS 620 (Avidyne) interface with GNS430c.Requires L3167-091-01 CDI KI 206 (Honeywell), copilot instead of CDI KI 204d.Only available in conjunction with L3442-091-00 GPS/NAV/COM GNS 430 (Garmin), copilot


Weight[lb]

1 08-18018-C L2315-001-10 Headset H 10-76 (David Clark), low impedance 0.6 1.31 08-18018-C L2315-001-11 Headset H 10-56 (David Clark), high impedance 0.6 1.31 08-18018-C L2315-001-14 Headset H 10-76 ANR/ENC with battery pack (David Clark),

low impedance0.8 1.8

1 08-18018-C L2315-001-15 Headset H 10-56 ANR/ENC with battery pack (David Clark) high impedance

0.8 1.8

1 08-18060-A L2315-001-72 Headset AHX32-02 ANR U/174 with battery pack (Bose), low impedance

0.3 0.7


Weight[lb]

1 08-18061-A L2341-007-62 Headset Adapter cable crew GLENAIR/U92 0.1 0.21 08-18061-A L2341-007-63 Headset Adapter cable pax GLENAIR/U92 0.2 0.4


Weight[lb]

1 08-18060-A L2315-001-73 Headset AHX34-04 ANR LEMO 28 VDC (Bose), low impedance

0.3 0.7


Weight[lb]

1 08-18061-A L2341-007-67 Headset Adapter cable crew GLENAIR/LEMO ANR 0.1 0.21 08-18061-A L2341-007-68 Headset Adapter cable pax GLENAIR/LEMO ANR 0.1 0.21 08-16063-A L2341-007-54 Fixed provisions for ANR 0.5 1.1


Weight[lb]


Technical Data

4.1.1.4 Performance Data

Radius of Action

The calculated maximum radius of action for the mission below is 144 nm (267 km).

Mission profile• Take-off in SL (max. 2910 kg)• Climb flight AEO-MCP from SL to 3000ft with VY (65KIAS)• Level flight in 3000ft with VH• Descent from 3000ft to SL with R/D of -1500 fpm (80KIAS)• Landing, pick-up of patient and take-off in SL• Climb flight AEO-MCP from SL to 3000ft with VY (65KIAS)• Level flight in 3000ft with VH• Descent from 3000ft to SL with R/D of -1500 fpm (80KIAS)• Landing in SL

Mission Parameters

Drag relevant equipment installed: None

Bleed air heating: On

Reserve: 20 minutes in 1500ft at VBR

Temperature: ISA

Weight breakdown kg lb

Empty weight equipped 1851 4081

Crew (3) 255 562

Reserve fuel 68 150

Trip fuel 492 1085

Take-off weight 2666 5879

Patient (1)a

a. Patient weight considered for return leg

85 187


Page 28 of 202 135.09.101.01

Technical Data

Figure 4.3: Mission TOW versus radius of action diagram

0 20 40 60 80 100 120 140 150

2100

2200

2300

2400

2500

2600

2700

Pla

nned

TO

W [k

g]

Radius of action [nm]

Fuel Quantity 560 kg



Technical Data

4.1.2 EMS - Conventional Avionics (Aerolite)The EMS Kit is based on a modular concept with various optional components for scene rescue, inten-sive care, neonatal missions and search & rescue. The interior is designed to give maximum room andcomfort to the medical crew and patient.



Figure 4.4: EMS Kit - Aerolite STC

Pilots 1 or 2

Medics 2

Patient 1


Page 30 of 202 135.09.101.01

Technical Data


Baseline Aircraft



General Equipment

Mission Equipment


Weight[lb]



Weight[lb]


a.First aid kit complies with german regulation rules 1. DV LuftBO paragraph 5(2). Type of operation, procedures or regulationsmay require a different/specific first aid kit







Weight[lb]



Technical Data

Interior Layout


Weight[lb]

1 07-30013-B L2524-002-00 Separation curtain for cockpit / cabin 2.1 4.61 07-40005-B L2513-200-00 Washable floor covering for cockpit 3.9 8.61 07-50025-C L5211-004-00 Securing device for complete opening of cockpit doors 0.8 1.81 07-50026-B L5231-001-00 One-hand latching system for clam-shell doors 1.0 2.21 07-50027-B L5231-002-00 Extended opening fasteners for clam-shell doors 0.3 0.71 07-77001-A L8521-001-00 EMS main switch in overhead console for Aerolite installation 0.2 0.41 07-70047-A AEL-30100-005-2 EMS Kit - Aerolite (AEL) 197.4 435.31 Integral Floor, fix provisions - AEL1 Integral Floor, detachable parts - AEL1 Stretcher "Combi" with stretcher platform, LH,

fix provisions - AEL1 Stretcher "Combi" with stretcher platform, LH,

detachable parts - AEL1 Medical Seat stationary, aft RH, fix provisions - AEL1 Medical Seat stationary, aft RH, detachable parts - AEL1 Medical Seat slidable & swivelling, front RH,

fix provisions - AEL1 Medical Seat slidable & swivelling, front RH,

detachable parts - AEL1 Medical Cabinet medium height, front center,

fix provisions - AEL1 Medical Cabinet medium height, front center,

detachable parts - AEL1 Life Support Panel, window LH - AEL1 Power & Lighting System, mid center - AEL1 Infusion Hook, mid LH - AEL1 Medical Rack, aft LH, fix provisions - AEL1 Medical Rack, aft LH, detachable parts - AEL1 Medical Rack, window LH - AEL1 Ceiling Rails, mid LH - AEL1 Door Frame Rails, mid LH - AEL1 Retainer for Corpuls C3 - AEL1 Retainer for Corpuls C3 (only monitor) - AEL1 Retainer for Medumat Transport - AEL2 Retainer for Perfusor Space - AEL1 Retainer for Compact Suction Unit 3 - AEL1 Medical Oxygen System 3x3,0 lt. 200 bar, front RH,

fix provisions - AEL1 Medical Oxygen System 3x3,0 lt. 200 bar, front RH,

detachable parts - AEL2 Tie Down Web - AEL1 Installation, Certifcation & Documentation - AEL3 Carbon Oxygen Bottle 3,0 lt. - AEL1 Monitor & Defibrillator Corpuls C3 - GS1 Respirator Medumat Transport - Weinmann1 Suction Pump Compact Suction Unit 3 - Laerdal2 Infusion System Perfusor Space - Braun1 Blood Glucose Meter Omnitest Plus - Braun1 Respiration Backpack incl. contents - Weinmann1 Emergency Backpack incl. DIN13232-N contents - Weinmann1 Cervical Collar Set Perfit ACE & Mini Perfit ACE - Ambu1 Vacuum Mattress - Tyromont1 Rescue Bag with internal belt system - Tyromont


Page 32 of 202 135.09.101.01

Technical Data

Avionics



Total: 1,848.4 4,075.8


Weight[lb]






1 08-16061-A L2341-193-40 Digital Audio Control System ACP53 (NAT), PAX 3.6 7.91 08-21014-C L3441-090-04 Radar altimeter KRA 405 B (Honeywell) 3.5 7.71 08-21014-C L3441-092-03 Radar altimeter indicator KNI 416 (Honeywell) 1.2 2.61 08-51012-A L3425-091-02 4" artificial horizon GH14-391 (Honeywell), copilot 2.5 5.51 08-51013-B L3425-806-51 2” stand-by horizon AI 804 DC (Goodrich),

with emergency battery6.6 14.6


1.4 3.1





Technical Data


General Equipment

Mission Equipment


Weight[lb]




handling kitb


0.8 1.8



Weight[lb]

1 06-11022-C L3272-001-10 Snow skids, fixed provisions 0.9 2.01 06-11022-C L3272-001-20 Snow skids, detachable partsa 21.9 48.31 06-21017-C L8512-001-10 External hoist LH, fixed provisions 8.6 19.01 06-21017-C L8512-001-20 External hoist 50m, detachable parts



62.7 138.3

1 06-26011-C L8511-002-10 Cargo hook mirrors RH, fixed provisions 0.8 1.81 06-26011-C L8511-002-20 Cargo hook mirrors RH, detachable parts 3.9 8.61 06-27022-B L8511-005-10 Dual cargo hook system, fixed provisions 4.3 9.51 06-27022-B L8511-005-20 Dual cargo hook system, detachable parts 21.5 47.41 06-27027-A L8511-003-10 Cargo hook weighing system, fixed provisionsb 0.2 0.4


Page 34 of 202 135.09.101.01

Technical Data

Interior Layout

Avionics

1 06-27027-A L8511-003-20 Cargo hook weighing system, detachable parts 1.5 3.31 06-31012-B L8531-001-00 External loudspeaker system with siren 11.5 25.41 06-46001-B L3344-001-00 Strobe lights, white 1.4 3.11 06-61015-B L3215-001-10 Emergency floats, fixed provisions 7.8 17.21 06-61015-B L3215-001-21 Emergency floats, detachable parts 64.6 142.41 06-65002-B L2566-001-00 Emergency hammer 0.2 0.4

a.No simultaneous fitment with settling protectors.b.Requires L8511-005-10 Dual cargo hook system, fixed provisions.


Weight[lb]



Weight[lb]


7.3 16.1


20.5 45.2


0.5 1.1


7.7 17.0


(Honeywell)0.8 1.8

1 08-25014-A L3455-092-03 Distance Measuring Equipment DME KN 63 (Honeywell)a

a.Requires L3169-092-02 Distance Measuring Equipment DME indicator KDI 572 (Honeywell).

2.0 4.41 08-26010-B L3431-092-02 Marker beacon receiver/lights KR 21 (Honeywell) 0.9 2.01 08-35007-B L3442-881-00 TAS 620 (Avidyne) interface with GNS430 0.2 0.41 08-35007-C L2327-001-01 Traffic Advisory System TAS 620 (Avidyne)b

b.Requires L3442-881-00 TAS 620 (Avidyne) interface with GNS430.

9.5 20.91 08-43018-B L3442-091-00 GPS/NAV/COM GNS 430 (Garmin), copilot, incl. annunciator/

switch MD 41 (MidContinent)c

c.Requires L3167-091-01 CDI KI 206 (Honeywell), copilot instead of CDI KI 204

8.3 18.3

1 08-61011-A L3167-091-01 CDI KI 206 (Honeywell), copilot instead of CDI KI 204d

d.Only available in conjunction with L3442-091-00 GPS/NAV/COM GNS 430 (Garmin), copilot

0.0 0.0


Weight[lb]


Technical Data


Required adapter cables for the above listed Headsets (L2315-001-10 -L2315-001-72):



Weight[lb]




0.8 1.8


0.3 0.7


Weight[lb]



Weight[lb]


0.3 0.7


Weight[lb]



Page 36 of 202 135.09.101.01

Technical Data


Radius of Action



Mission Parameters




Temperature: ISA



Crew (3) 255 562

Reserve fuel 68 150

Trip fuel 492 1085


Patient (1)a


85 187


Technical Data


0 20 40 60 80 100 120 140 150

2100

2200

2300

2400

2500

2600

2700

Pla

nned

TO

W [k

g]





Page 38 of 202 135.09.101.01

Technical Data

4.1.3 EMS - Conventional Avionics (Bucher Leichtbau)The EMS Kit provides all necessary equipment to carry out professional air ambulance missions. Thecabin layout is made in order to take care for most of your missions and can be adapted according toyour special requirements. The system is designed to accommodate all equipment without using spe-cial tools.




Baseline Aircraft



Figure 4.6: EMS Kit - Bucher Leichtbau STC

Pilots 1 or 2

Medics 2

Patient 1


Weight[lb]



Technical Data

General Equipment

Mission Equipment

Interior Layout


Weight[lb]









Weight[lb]



Weight[lb]

1 07-30013-B L2524-002-00 Separation curtain for cockpit / cabin 2.1 4.61 07-40005-B L2513-200-00 Washable floor covering for cockpit 3.9 8.61 07-50025-C L5211-004-00 Securing device for complete opening of cockpit doors 0.8 1.81 07-50026-B L5231-001-00 One-hand latching system for clam-shell doors 1.0 2.21 07-50027-B L5231-002-00 Extended opening fasteners for clam-shell doors 0.3 0.71 07-77002-A L8522-001-00 EMS main switch in overhead console for Bucher Leichtbau

installation0.2 0.4

1 07-70040-A BUL-30100-001-2 EMS Kit - Bucher Leichtbau (BUL) 152.9 337.11 Integral Floor, fix provisions - BUL1 Integral Floor, detachable parts - BUL1 Stretcher “Airy”, LH, fix provisions - BUL1 Stretcher “Airy”, LH, detachable parts - BUL


Page 40 of 202 135.09.101.01

Technical Data

1 Medical Seat stationary, aft RH, fix provisions - BUL1 Medical Seat stationary, aft RH, detachable parts - BUL1 Medical Seat slidable & swivelling, front RH,

fix provisions - BUL1 Medical Seat slidable & swivelling, front RH,

detachable parts - BUL1 Medical Cabinet, front center - BUL1 Service & Control Panel, window LH, fix provisions - BUL1 Service & Control Panel, window LH, detachable parts - BUL1 Electrical Supply System - BUL1 Lighting System, mid center, fix provisions - BUL1 Lighting System, mid center, detachable parts - BUL1 Lighting System, front LH, fix provisions - BUL1 Lighting System, front LH, detachable parts - BUL1 Infusion Hook, mid LH, fix provisions - BUL1 Infusion Hook, mid LH, detachable parts - BUL1 Medical Equipment Rails, aft LH, fix provisions - BUL1 Medical Equipment Rails, aft LH, detachable parts - BUL1 Retainer for Corpuls C3 - BUL1 Retainer for Corpuls C3 (only monitor) - BUL1 Retainer for Medumat Transport - BUL2 Retainer for Perfusor Space - BUL1 Retainer for Compact Suction Unit 3, fix provisions - BUL1 Retainer for Compact Suction Unit 3, detachable parts - BUL1 Oxygen Bottle Rack 3x3,0 lt. 200 bar, window RH,

fix provisions - BUL1 Oxygen Bottle Rack 3x3,0 lt. 200 bar, window RH,

detachable parts - BUL1 Cargo Restrain System - BUL1 Installation, Certifcation & Documentation - BUL3 Carbon Oxygen Bottle 3,0 lt. - BUL1 Monitor & Defibrillator Corpuls C3 - GS1 Respirator Medumat Transport - Weinmann1 Suction Pump Compact Suction Unit 3 - Laerdal2 Infusion System Perfusor Space - Braun1 Blood Glucose Meter Omnitest Plus - Braun1 Respiration Backpack incl. contents - Weinmann1 Emergency Backpack incl. DIN13232-N contents - Weinmann1 Cervical Collar Set Perfit ACE & Mini Perfit ACE - Ambu1 Vacuum Mattress - Tyromont1 Rescue Bag with internal belt system - Tyromont


Weight[lb]


Technical Data

Avionics



Total: 1,802.6 3,974.8


Weight[lb]






1 08-16061-A L2341-193-40 Digital Audio Control System ACP53 (NAT), PAX 3.6 7.91 08-21014-C L3441-090-04 Radar altimeter KRA 405 B (Honeywell) 3.5 7.71 08-21014-C L3441-092-03 Radar altimeter indicator KNI 416 (Honeywell) 1.2 2.61 08-51012-A L3425-091-02 4" artificial horizon GH14-391 (Honeywell), copilot 2.5 5.51 08-51013-B L3425-806-51 2” stand-by horizon AI 804 DC (Goodrich),



1.4 3.1





Page 42 of 202 135.09.101.01

Technical Data


General Equipment

Mission Equipment


Weight[lb]




handling kitb


0.8 1.8



Weight[lb]




62.7 138.3



Technical Data

Interior Layout

Avionics




Weight[lb]

1 07-15016-B L2512-003-10 Height adjustable pilot seat instead of standard pilot seat 1.8 4.01 07-15016-B L2512-003-20 Height adjustable copilot seat instead of standard copilot seat 1.8 4.01 07-30012-B L2581-001-00 Enhanced sound proofing kit 4.8 10.61 07-50028-A L5213-001-11 Sliding door fastener, intermediate and max. position, LH 1.0 2.21 07-50028-A L5213-001-12 Sliding door fastener, max. position, LH 0.4 0.91 07-50028-A L5213-001-21 Sliding door fastener, intermediate and max. position, 1.0 2.21 07-50028-A L5213-001-22 Sliding door fastener max. position, RH 0.4 0.91 07-50034-B L5212-001-00 Jettisonable cockpit doors 1.2 2.61 07-50036-B L2514-012-00 Covers for sliding door fairing LH/RH 0.1 0.21 07-50039-B L5211-010-00 Door catch system for cockpit doors 0.1 0.21 07-50039-B L5211-011-00 Door catch system for sliding doors 0.2 0.41 07-60014-B L2514-013-00 Map case in sliding doors LH/RH 1.4 3.1


Weight[lb]


7.3 16.1


20.5 45.2


0.5 1.1

1 08-15523-A L2315-092-02 IRIDIUM satellite communication and tracking systemFlightdeck (SkyConnect),

7.7 17.0


(Honeywell)0.8 1.8

1 08-25014-A L3455-092-03 Distance Measuring Equipment DME KN 63 (Honeywell)a

a.Requires L3169-092-02 Distance Measuring Equipment DME indicator KDI 572 (Honeywell).

2.0 4.41 08-26010-B L3431-092-02 Marker beacon receiver/lights KR 21 (Honeywell) 0.9 2.01 08-35007-B L3442-881-00 TAS 620 (Avidyne) interface with GNS430 0.2 0.41 08-35007-C L2327-001-01 Traffic Advisory System TAS 620 (Avidyne)b

b.Requires L3442-881-00 TAS 620 (Avidyne) interface with GNS430.

9.5 20.91 08-43018-B L3442-091-00 GPS/NAV/COM GNS 430 (Garmin), copilot, incl. annunciator/

switch MD 41 (MidContinent)c

c.Requires L3167-091-01 CDI KI 206 (Honeywell), copilot instead of CDI KI 204

8.3 18.3

1 08-61011-A L3167-091-01 CDI KI 206 (Honeywell), copilot instead of CDI KI 204d

d.Only available in conjunction with L3442-091-00 GPS/NAV/COM GNS 430 (Garmin), copilot

0.0 0.0


Weight[lb]


Page 44 of 202 135.09.101.01

Technical Data





Weight[lb]




0.8 1.8


0.3 0.7


Weight[lb]



Weight[lb]

1 08-18060-A L2315-001-73 Headset AHX34-04 ANR LEMO 28 VDC (Bose), low impedance 0.3 0.7


Weight[lb]



Technical Data


Radius of Action

The calculated maximum radius of action for the mission below is 144.5 nm (268 km).


Mission Parameters




Temperature: ISA



Crew (3) 255 562

Reserve fuel 68 150

Trip fuel 492 1085


Patient (1)a


85 187


Page 46 of 202 135.09.101.01

Technical Data


0 20 40 60 80 100 120 140 150

2100

2200

2300

2400

2500

2600

2700

Pla

nned

TO

W [k

g]





Technical Data

Blank


Page 48 of 202 135.09.101.01

Technical Data

4.2 EMS - Glass Cockpit

The EC135 was tailor-made for secondary inter-hospital missions in close cooperation with doctorsand rescue experts, providing:• A modular design to comply with different users' needs• A suitable cabin design for maximum use and installation of several medical devices• In-flight esuscitation (CPR) and endotracheal intubation capabilities• A cabin-accessible baggage compartment • A hygienic, easy-to-clean floor• Rear or side stretcher loading• An Anti-Resonance Isolation System (ARIS), ensuring low vibration levels and a smooth ride

Optional mission equipment such as the autopilot, moving map and weather radar support the pilot du-ring IFR flights and enhance overall flight safety. A "Flying Intensive Care Station" or incubators arealso available on a modular basis.

Ready for mission

All presented EMS - Glass cockpit configurations include a complete EMS kit. All kits are fully equippedwith stretcher, medical seats and floor, cabinet, oxygen system, electrical and lighting system, as wellas medical apparatuses and further mission equipment (e.g. rescue rucksack, vacuum mattress, etc.).

Figure 4.8: Typical layout of an EC135 ambulance helicopter


Technical Data

4.2.1 EMS - Glass Cockpit (Air Ambulance Technology)The EMS Kit including state of the art medical devices is designed for rescue-/ ambulance- and neo-natal air medical missions. The complete system is fitted to the available attachments on the helicopterfloor. No modification to the helicopter structure is required. The easy and quick installation can bedone within 25 minutes.


Flight Rules: IFRInstrumentation: Glass Cockpit (MEGHAS)Cat-A: Yes

Figure 4.9: EMS Kit - Air Ambulance Technology STC

Pilots 1 or 2

Medics 2

Patient 1


Page 50 of 202 135.09.101.01

Technical Data


Baseline Aircraft



General Equipment


Weight[lb]



Weight[lb]



1.5 3.31 05-12001-B L5232-001-00 Multifunction handle on the main gear box cowling (LH and RH) 0.6 1.31 05-22007-B L7924-001-00 Fuzz burners for engines 1.2 2.61 05-22008-C L2621-001-00 Engine fire extinguishing system 3.6 7.91 05-22014-A L5371-001-00 Engine outlet heat protection 1.2 2.61 05-30003-A L2565-002-00 Flash light copilot side 0.2 0.41 05-31025-B L5211-002-00 Sliding windows in sliding doors 1.9 4.21 05-31026-C L2514-002-00 Tinted sun shades for cockpit windshield roof section 1.9 4.21 05-31027-B L5633-001-10 Window in clam-shell door, LH 0.8 1.81 05-33001-B L3113-001-00 Slant panel 0.8 1.81 05-33002-B L3113-004-00 Center console 2.2 4.91 05-34002-B L2576-001-00 Avionics compartment 4.2 9.31 05-37016-C L6701-001-00 Copilot flight controls 6.0 13.21 05-38010-B L3111-001-04 7" copilot instrument panel with glare shield 2.7 6.01 05-39006-B L2514-003-01 Map case in copilot door 0.5 1.11 05-39007-B L3111-001-10 Map cases on instrument panel glare shield 0.6 1.31 05-39008-B L3113-004-10 Illuminated chart holder for pilot side 1.0 2.21 05-41004-C L2104-003-00 Bleed air heating system: EMS-version 7.0 15.41 05-61010-B L2433-006-00 Battery, type "Saft", ULM, 40 Ah, 24 V


1 05-62010-C L2420-005-00 AC system (50 VA) 1.9 4.21 05-63003-B L2432-001-00 Starter/generator (2 x 200 A, 28V DC)




Technical Data

Mission Equipment

Interior Layout


Weight[lb]

1 06-11021-B L3274-001-10 Settling protectors, fixed provisions 1.9 4.21 06-11021-B L3274-001-20 Settling protectors, detachable parts 7.9 17.41 06-12008-C L3217-001-00 Reinforced rear landing gear cross tube 1.0 2.21 06-45023-B L3343-003-00 Landing & search light, 450 W 3.1 6.81 06-65004-B L2625-003-00 2nd portable fire extinguisher 2.8 6.21 06-66009-B L3322-001-00 Boarding step illumination 0.2 0.41 06-67044-B L2563-801-06 ELT C406-N HM (Artex) incl. NAV. opt. 3.3 7.3


Weight[lb]

1 07-30013-B L2524-002-00 Separation curtain for cockpit / cabin 2.1 4.61 07-40005-B L2513-200-00 Washable floor covering for cockpit 3.9 8.61 07-50025-C L5211-004-00 Securing device for complete opening of cockpit doors 0.8 1.81 07-50026-B L5231-001-00 One-hand latching system for clam-shell doors 1.0 2.21 07-50027-B L5231-002-00 Extended opening fasteners for clam-shell doors 0.3 0.71 07-70044-A AAT-30100-002-2 EMS Kit - Air Ambulance Technology (AAT) 200.0 441.01 Medical Floor (Universal) - AAT1 Stretcher "Blue Mattress", LH - AAT1 Medical Seat slidable, aft RH - AAT1 Medical Seat slidable & swivelling, front RH - AAT1 Medical Cabinet with 3 drawer, front center - AAT1 Medical Equipment Carrier, aft LH - AAT1 Retainer for Corpuls C3 - AAT1 Retainer for Corpuls C3 (only monitor) - AAT1 Retainer for Medumat Transport - AAT2 Retainer for Perfusor Space - AAT1 Retainer for Compact Suction Unit 3 - AAT1 Oxygen Station 3x3,0 lt. 200 bar, front RH - AAT1 Accessories - AAT1 Installation, Certifcation & Documentation - AAT3 Aluminium Oxygen Bottle 3,0 lt. - AAT1 Monitor & Defibrillator Corpuls C3 - GS1 Respirator Medumat Transport - Weinmann1 Suction Pump Compact Suction Unit 3 - Laerdal2 Infusion System Perfusor Space - Braun1 Blood Glucose Meter Omnitest Plus - Braun1 Respiration Backpack incl. contents - Weinmann1 Emergency Backpack incl. DIN13232-N contents - Weinmann1 Cervical Collar Set Perfit ACE & Mini Perfit ACE - Ambu1 Vacuum Mattress - Tyromont1 Rescue Bag with internal belt system - Tyromont


Page 52 of 202 135.09.101.01

Technical Data

Avionics



Total: 1,925.9 4,246.6


Weight[lb]

1 08-00031-A L2300-011-05 AV PACK DP IFR GC G430 75.7 166.91 Digital Audio Control System (NAT), incl. AMU50, ACP53

pilot and copilot1 Transponder (Mode S) GTX 330 (Garmin)1 Distance Measuring Equipment DME CDM 451 (Chelton)1 Marker beacon receiver/ lights KR 21 (Honeywell)1 Avionics/Radio master switches (Special EUROCOPTER®)1 GPS/NAV/COM GNS 430 (Garmin), copilot,

interfaced with FCDS (GPS stand-alone)1 GPS/NAV/COM GNS 430 (Garmin), pilot, interfaced with FCDS1 2” std-by horizon AI 804 DC (Goodrich), incl. emergency battery1 MEGHAS - Flight Control Display System (FCDS) -

Dual (4xSMD45)1 AV Pack DP IFR GC G430, interconnection / wiring1 08-12036-B L4322-090-04 Fixed provisions for tactical radio (antenna, power supply,


1 08-16061-A L2341-193-40 Digital Audio Control System ACP53 (NAT), PAX 3.6 7.91 08-21014-C L3441-090-04 Radar altimeter KRA 405 B (Honeywell) 3.5 7.71 08-46040-A L3168-092-07 Digital moving map EURONAV IV+ -RN6 (Euro Avionics),

interfaced with FCDSa

a.Approval for VFR only, maps and special options not included.

5.4 11.9

1 08-53002-B L2212-400-00 MEGHAS Sensor Kit 17.0 37.51 08-54001-C L3411-001-00 Copilot pitot static system 1.5 3.31 08-65004-B L3443-010-00 Video Radar Unit (VRU) 5.0 11.01 08-72001-B L2212-001-00 Digital Automatic Flight Control System - DAFCS 27.0 59.5


Technical Data


General Equipment

Mission Equipment


Weight[lb]



8.2 18.11 05-22014-A L5611-002-00 Tinted front windshields 1.2 2.61 05-23006-B L7165-002-00 Engine compressor wash kit 3.2 7.11 05-25016-D L7161-001-10 Sand filter system, fixed provisions 11.3 24.91 05-25016-D L7161-001-20 Sand filter system, detachable parts 26.2 57.81 05-26012-B L1241-001-00 Anti-corrosion protection 5.2 11.51 05-31026-C L5621-001-00 Tinted window for cockpit doors 0.0 0.01 05-31028-C L2524-030-10 IFR - training screen, fixed provisions 0.1 0.21 05-31028-C L2524-030-20 IFR - training screen, detachable parts 1.6 3.51 05-31045-A L5211-001-11 Lockable sliding window in copilots' door 0.1 0.21 05-31045-A L5211-001-12 Lockable sliding window in pilots' door 0.1 0.21 05-31086-A L5211-002-01 Ram air deflectors sliding doors 0.4 0.91 05-31098-A L5211-001-01 Ram air deflectors cockpit doors 0.6 1.31 05-32007-B L3042-001-00 Windshield wiper system 5.0 11.01 05-34003-B L2576-002-00 Dampers for avionics compartment 1.8 4.01 05-37017-B L6721-001-00 Covers for copilot flight controls -2.5 -5.51 05-39008-B L3113-004-20 Illuminated chart holder for copilot side 0.9 2.01 05-42041-A L2105-005-00 Air conditioning system 55.0 121.31 05-85008-C L2843-001-00 Fuel management system (Fuel flow meters) 1.2 2.61 05-92009-B L6611-001-10 Main rotor blade folding: basic kit 1.3 2.91 05-92009-B L6611-001-20 Main rotor blade folding: fixed provisions for ground

handling kitb


0.8 1.8



Weight[lb]




62.7 138.3



Page 54 of 202 135.09.101.01

Technical Data

Interior Layout

Avionics




Weight[lb]



Weight[lb]


7.3 16.1


20.5 45.2


0.5 1.1


7.7 17.0

1 08-16061-A L2341-006-63 Voice alert generation for DACS (NAT) 0.0 0.01 08-24015-C L3452-092-09 ADF control unit CDF-552 (Chelton/Wulfsberg) 1.2 2.61 08-24015-C L3452-092-17 ADF receiver DF-431B, (Chelton/Wulfsberg)a

a.Requires L3452-092-09 ADF control unit CDF-552 (Chelton/Wulfsberg) and vice versa.

9.6 21.21 08-31019-B L2571-001-00 Radar radome for RDR 2000 2.0 4.41 08-31019-B L3443-090-02 Color weather radar RDR 2000 (Honeywell)b

b.Requires L2571-001-00 Radar radome for RDR2000.

6.6 14.61 08-35007-B L3442-881-00 TAS 620 (Avidyne) interface with GNS430 0.2 0.41 08-35007-C L2327-001-01 Traffic Advisory System TAS 620 (Avidyne)c

c.Requires L3442-881-00 TAS 620 (Avidyne) interface with GNS430.

9.5 20.91 08-53004-B L3424-000-00 AHRS Free Steering Mode 0.5 1.11 08-81018-C L2321-007-00 M’ARMS® Cockpit Voice and Flight Data Recorder (CVFDR),

ground station not included15.7 34.6


Weight[lb]


Technical Data





Weight[lb]




0.8 1.8


0.3 0.7


Weight[lb]



Weight[lb]


0.3 0.7


Weight[lb]



Page 56 of 202 135.09.101.01

Technical Data


Maximum Range

The calculated maximum range for the mission below is 274 nm (507 km).

Mission profile• Take-off in SL (max. 2910 kg)• Climb flight AEO-MCP from SL to 7000ft with VY (65KIAS)• Level flight in 7000ft with VBR• Descent from 7000ft to SL with R/D of -1000 fpm (80KIAS)• Landing in SL

Mission Parameters



Contingency fuel 10%

Reserve: 30 minutes in 1500ft at VY (65KIAS)

Temperature: ISA



Crew (3) 255 562

Patient (1) 85 187

Reserve fuel 80 150

Contingency fuel 44 97

Trip fuel 436 961



Technical Data

Figure 4.10: Mission TOW versus range diagram

0 40 80 120 160 200 240 280 300

2300

2400

2500

2600

2700

2800

2900

Pla

nned

TO

W [k

g]

Range [nm]



Page 58 of 202 135.09.101.01

Technical Data

4.2.2 EMS - Glass Cockpit (Aerolite)The EMS Kit is based on a modular concept with various optional components for scene rescue, inten-sive care, neonatal missions and search & rescue. The interior is designed to give maximum room andcomfort to the medical crew and patient.



Figure 4.11: EMS Kit - Aerolite STC

Pilots 1 or 2

Medics 2

Patient 1


Technical Data


Baseline Aircraft



General Equipment

Mission Equipment


Weight[lb]



Weight[lb]









Weight[lb]



Page 60 of 202 135.09.101.01

Technical Data

Interior Layout


Weight[lb]

1 07-30013-B L2524-002-00 Separation curtain for cockpit / cabin 2.1 4.61 07-40005-B L2513-200-00 Washable floor covering for cockpit 3.9 8.61 07-50025-C L5211-004-00 Securing device for complete opening of cockpit doors 0.8 1.81 07-50026-B L5231-001-00 One-hand latching system for clam-shell doors 1.0 2.21 07-50027-B L5231-002-00 Extended opening fasteners for clam-shell doors 0.3 0.71 07-77001-A L8521-001-00 EMS main switch in overhead console for Aerolite installation 0.2 0.41 07-70047-A AEL-30100-005-2 EMS Kit - Aerolite (AEL) 197.4 435.31 Integral Floor, fix provisions - AEL1 Integral Floor, detachable parts - AEL1 Stretcher "Combi" with stretcher platform, LH,

fix provisions - AEL1 Stretcher "Combi" with stretcher platform, LH,

detachable parts - AEL1 Medical Seat stationary, aft RH, fix provisions - AEL1 Medical Seat stationary, aft RH, detachable parts - AEL1 Medical Seat slidable & swivelling, front RH,

fix provisions - AEL1 Medical Seat slidable & swivelling, front RH,

detachable parts - AEL1 Medical Cabinet medium height, front center,

fix provisions - AEL1 Medical Cabinet medium height, front center,

detachable parts - AEL1 Life Support Panel, window LH - AEL1 Power & Lighting System, mid center - AEL1 Infusion Hook, mid LH - AEL1 Medical Rack, aft LH, fix provisions - AEL1 Medical Rack, aft LH, detachable parts - AEL1 Medical Rack, window LH - AEL1 Ceiling Rails, mid LH - AEL1 Door Frame Rails, mid LH - AEL1 Retainer for Corpuls C3 - AEL1 Retainer for Corpuls C3 (only monitor) - AEL1 Retainer for Medumat Transport - AEL2 Retainer for Perfusor Space - AEL1 Retainer for Compact Suction Unit 3 - AEL1 Medical Oxygen System 3x3,0 lt. 200 bar, front RH,

fix provisions - AEL1 Medical Oxygen System 3x3,0 lt. 200 bar, front RH,

detachable parts - AEL2 Tie Down Web - AEL1 Installation, Certifcation & Documentation - AEL3 Carbon Oxygen Bottle 3,0 lt. - AEL1 Monitor & Defibrillator Corpuls C3 - GS1 Respirator Medumat Transport - Weinmann1 Suction Pump Compact Suction Unit 3 - Laerdal2 Infusion System Perfusor Space - Braun1 Blood Glucose Meter Omnitest Plus - Braun1 Respiration Backpack incl. contents - Weinmann1 Emergency Backpack incl. DIN13232-N contents - Weinmann1 Cervical Collar Set Perfit ACE & Mini Perfit ACE - Ambu1 Vacuum Mattress - Tyromont1 Rescue Bag with internal belt system - Tyromont


Technical Data

Avionics



Total: 1,923.4 4,241.2


Weight[lb]


pilot and copilot1 Transponder (Mode S) GTX 330 (Garmin)1 Distance Measuring Equipment DME CDM 451 (Chelton)1 Marker beacon receiver/ lights KR 21 (Honeywell)1 Avionics/Radio master switches (Special EUROCOPTER®)1 GPS/NAV/COM GNS 430 (Garmin), copilot, interfaced

with FCDS (GPS stand-alone)1 GPS/NAV/COM GNS 430 (Garmin), pilot, interfaced with FCDS1 2” std-by horizon AI 804 DC (Goodrich), incl. emergency battery1 MEGHAS - Flight Control Display System (FCDS) -



1 08-16061-A L2341-193-40 Digital Audio Control System ACP53 (NAT), PAX 3.6 7.91 08-21014-C L3441-090-04 Radar altimeter KRA 405 B (Honeywell) 3.5 7.71 08-46040-A L3168-092-07 Digital moving map EURONAV IV+ -RN6 (Euro Avionics),

interfaced with FCDSa


5.4 11.9



Page 62 of 202 135.09.101.01

Technical Data


General Equipment

Mission Equipment


Weight[lb]




handling kitb


0.8 1.8



Weight[lb]




62.7 138.3

1 06-26011-C L8511-002-10 Cargo hook mirrors RH, fixed provisions 0.8 1.81 06-26011-C L8511-002-20 Cargo hook mirrors RH, detachable parts 3.9 8.61 06-27022-B L8511-005-10 Dual cargo hook system, fixed provisionsb 4.3 9.51 06-27022-B L8511-005-20 Dual cargo hook system, detachable parts 21.5 47.41 06-27027-A L8511-003-10 Cargo hook weighing system, fixed provisions 0.2 0.4


Technical Data

Interior Layout

Avionics




Weight[lb]



Weight[lb]


7.3 16.1


20.5 45.2


0.5 1.1


7.7 17.0




b.Requires L2571-001-00 Radar radome for RDR2000.






Weight[lb]


Page 64 of 202 135.09.101.01

Technical Data





Weight[lb]




0.8 1.8


0.3 0.7


Weight[lb]



Weight[lb]


0.3 0.7


Weight[lb]



Technical Data


Maximum Range


Mission profile• Take-off in SL (max. 2910 kg)• Climb flight AEO-MCP from SL to 7000ft with VY (65KIAS)• Level flight in 7000ft with VBR• Descent from 7000ft to SL with R/D of -1000 fpm (80KIAS)• Landing in SL

Mission Parameters





Temperature: ISA



Crew (3) 255 562

Patient (1) 85 187

Reserve fuel 80 150


Trip fuel 436 961



Page 66 of 202 135.09.101.01

Technical Data


0 40 80 120 160 200 240 280 300

2300

2400

2500

2600

2700

2800

2900

Pla

nned

TO

W [k

g]

Range [nm]



Technical Data

4.2.3 EMS - Glass Cockpit (Bucher Leichtbau)The EMS Kit provides all necessary equipment to carry out professional air ambulance missions. Thecabin layout is made in order to take care for most of your missions and can be adapted according toyour special requirements. The system is designed to accommodate all equipment without using spe-cial tools.




Baseline Aircraft



Figure 4.13: EMS Kit - Bucher Leichtbau STC

Pilots 1 or 2

Medics 2

Patient 1


Weight[lb]



Page 68 of 202 135.09.101.01

Technical Data

General Equipment

Mission Equipment

Interior Layout


Weight[lb]









Weight[lb]



Weight[lb]

1 07-30013-B L2524-002-00 Separation curtain for cockpit / cabin 2.1 4.61 07-40005-B L2513-200-00 Washable floor covering for cockpit 3.9 8.61 07-50025-C L5211-004-00 Securing device for complete opening of cockpit doors 0.8 1.81 07-50026-B L5231-001-00 One-hand latching system for clam-shell doors 1.0 2.21 07-50027-B L5231-002-00 Extended opening fasteners for clam-shell doors 0.3 0.71 07-77002-A L8522-001-00 EMS main switch in overhead console for Bucher Leichtbau

installation0.2 0.4

1 07-70040-A BUL-30100-001-2 EMS Kit - Bucher Leichtbau (BUL) 152.9 337.11 Integral Floor, fix provisions - BUL


Technical Data

1 Integral Floor, detachable parts - BUL1 Stretcher “Airy”, LH, fix provisions - BUL1 Stretcher “Airy”, LH, detachable parts - BUL1 Medical Seat stationary, aft RH, fix provisions - BUL1 Medical Seat stationary, aft RH, detachable parts - BUL1 Medical Seat slidable & swivelling, front RH,

fix provisions - BUL1 Medical Seat slidable & swivelling, front RH,

detachable parts - BUL1 Medical Cabinet, front center - BUL1 Service & Control Panel, window LH, fix provisions - BUL1 Service & Control Panel, window LH, detachable parts - BUL1 Electrical Supply System - BUL1 Lighting System, mid center, fix provisions - BUL1 Lighting System, mid center, detachable parts - BUL1 Lighting System, front LH, fix provisions - BUL1 Lighting System, front LH, detachable parts - BUL1 Infusion Hook, mid LH, fix provisions - BUL1 Infusion Hook, mid LH, detachable parts - BUL1 Medical Equipment Rails, aft LH, fix provisions - BUL1 Medical Equipment Rails, aft LH, detachable parts - BUL1 Retainer for Corpuls C3 - BUL1 Retainer for Corpuls C3 (only monitor) - BUL1 Retainer for Medumat Transport - BUL2 Retainer for Perfusor Space - BUL1 Retainer for Compact Suction Unit 3, fix provisions - BUL1 Retainer for Compact Suction Unit 3, detachable parts - BUL1 Oxygen Bottle Rack 3x3,0 lt. 200 bar, window RH,

fix provisions - BUL1 Oxygen Bottle Rack 3x3,0 lt. 200 bar, window RH,

detachable parts - BUL1 Cargo Restrain System - BUL1 Installation, Certifcation & Documentation - BUL3 Carbon Oxygen Bottle 3,0 lt. - BUL1 Monitor & Defibrillator Corpuls C3 - GS1 Respirator Medumat Transport - Weinmann1 Suction Pump Compact Suction Unit 3 - Laerdal2 Infusion System Perfusor Space - Braun1 Blood Glucose Meter Omnitest Plus - Braun1 Respiration Backpack incl. contents - Weinmann1 Emergency Backpack incl. DIN13232-N contents - Weinmann1 Cervical Collar Set Perfit ACE & Mini Perfit ACE - Ambu1 Vacuum Mattress - Tyromont1 Rescue Bag with internal belt system - Tyromont


Weight[lb]


Page 70 of 202 135.09.101.01

Technical Data

Avionics



Total: 1,877.6 4,140.1


Weight[lb]


pilot and copilot1 Transponder (Mode S) GTX 330 (Garmin)1 Distance Measuring Equipment DME CDM 451 (Chelton)1 Marker beacon receiver/ lights KR 21 (Honeywell)1 Avionics/Radio master switches (Special EUROCOPTER®)1 GPS/NAV/COM GNS 430 (Garmin), copilot, interfaced

with FCDS (GPS stand-alone)1 GPS/NAV/COM GNS 430 (Garmin), pilot, interfaced with FCDS1 2” std-by horizon AI 804 DC (Goodrich), incl. emergency battery1 MEGHAS - Flight Control Display System (FCDS) -



1 08-16061-A L2341-193-40 Digital Audio Control System ACP53 (NAT), PAX 3.6 7.91 08-21014-C L3441-090-04 Radar altimeter KRA 405 B (Honeywell) 3.5 7.71 08-46040-A L3168-092-07 Digital moving map EaURONAV IV+ -RN6 (Euro Avionics),

interfaced with FCDS


5.4 11.9



Technical Data


General Equipment

Mission Equipment


Weight[lb]




handling kitb


0.8 1.8



Weight[lb]




62.7 138.3



Page 72 of 202 135.09.101.01

Technical Data

Interior Layout

Avionics




Weight[lb]



Weight[lb]


7.3 16.1


20.5 45.2


0.5 1.1


7.7 17.0




b.Requires L2571-001-00 Radar radome RDR2000.


c.Requires L3442-881-00 TAS 620 (Avidyne) interface with GNS430




Weight[lb]


Technical Data

Headsets and Adapter cableIn any case EUROCOPTER®adapter cables are required to connect any type of headset or helmet tothe aircraft intercom system. Furthermore EUROCOPTER® provides different headset types for cus-tomer‘s choise.




Weight[lb]




0.8 1.8


0.3 0.7


Weight[lb]



Weight[lb]


0.3 0.7


Weight[lb]



Page 74 of 202 135.09.101.01

Technical Data


Maximum Range


Mission profile• Take-off in SL (max. 2910 kg)• Climb flight AEO-MCP from SL to 7000ft with VY (65KIAS)• Level flight in 7000ft with VBR• Landing in SL• Descent from 7000ft to SL with R/D of -1000 fpm (80KIAS)

Mission Parameters





Temperature: ISA



Crew (3) 255 562

Patient (1) 85 187

Reserve fuel 79 174


Trip fuel 437 964



Technical Data


0 40 80 120 160 200 240 280 300

2300

2400

2500

2600

2700

2800

2900

Pla

nned

TO

W [k

g]

Range [nm]



Page 76 of 202 135.09.101.01

Technical Data

4.3 Disaster Management

The EC135 can be fitted with disaster management equipment to perform rapid interventions in situa-tions of high risk, adverse weather, catastrophes and disasters, and in emergencies such as floods,earthquakes, landslides, and heavy snowfalls. The EC135 can quickly respond to forest fires, emer-gency situations such as terrorist attacks and can also perform environmental protection missions.

Ready for missionAll presented Disaster Management configurations include a complete mission kit. All kits are fullyequipped with stretchers, seats, stowage rack inlcuding oxygen bottles, as well as medical appara-tuses and further mission equipment (e.g. rescue rucksack, vacuum mattress, etc.).

Figure 4.15: Typical EC135 Disaster Management on duty


Technical Data

4.3.1 Disaster Management (Air Ambulance Technology)The Disaster Management Kit is designed in module part system for disaster missions. The completesystem is fitted to the available attachments on the helicopter floor. No modification to the helicopterstructure is required. The easy and quick installation can be done within 15 minutes.



EVACUATION

SEARCH AND RESCUE

Figure 4.16: Disaster Management Kit - Air Ambulance Technology STC

Pilots 1 or 2

Medics 2

Patient 2

Pilots 1 or 2

Medics 2

Patient 1


Page 78 of 202 135.09.101.01

Technical Data

INTERVENTION


Baseline Aircraft



General Equipment

Pilots 1 or 2

Pax 6


Weight[lb]

1 00-10002-A L0000-002-00 EC135 Baseline Aircraft 135.09.100.01 E 1,455.0 3,208.31 L0000-003-01 2 Turbomeca ARRIUS 2B2 turbine engines1 L0000-003-02 2 Pratt & Whitney PW206B2 turbine engines


Weight[lb]



1.5 3.31 05-12001-B L5232-001-00 Multifunction handle on the main gear box cowling (LH and RH) 0.6 1.31 05-22007-B L7924-001-00 Fuzz burners for engines 1.2 2.61 05-22008-C L2621-001-00 Engine fire extinguishing system 3.6 7.91 05-22014-A L5371-001-00 Engine outlet heat protection 1.2 2.61 05-30003-A L2565-002-00 Flash light copilot side 0.2 0.41 05-31026-C L2514-002-00 Tinted sun shades for cockpit windshield roof section 1.9 4.21 05-33001-B L3113-001-00 Slant panel 0.8 1.81 05-33002-B L3113-004-00 Center console 2.2 4.91 05-34002-B L2576-001-00 Avionics compartment 4.2 9.31 05-36007-B L8532-002-30 Multifunction step LH (instead of std. boarding step) 4.9 10.81 05-37016-C L6701-001-00 Copilot flight controls 6.0 13.21 05-38010-B L3111-001-04 7" copilot instrument panel with glare shield 2.7 6.01 05-39006-B L2514-003-01 Map case in copilot door 0.5 1.11 05-39007-B L3111-001-10 Map cases on instrument panel glare shield 0.6 1.31 05-39008-B L3113-004-10 Illuminated chart holder for pilot side 1.0 2.21 05-41004-C L2104-003-00 Bleed air heating system: EMS-version 7.0 15.41 05-61010-B L2433-006-00 Battery, type "Saft", ULM, 40 Ah, 24 V






Technical Data

Mission Equipment

Interior Layout


Weight[lb]

1 06-11021-B L3274-001-10 Settling protectors, fixed provisions 1.9 4.21 06-11021-B L3274-001-20 Settling protectors, detachable parts 7.9 17.41 06-12008-C L3217-001-00 Reinforced rear landing gear cross tube 1.0 2.21 06-24009-B L8534-002-11 External rope-down device for 2 persons, fixed provisions LH 4.1 9.01 06-24009-B L8534-002-12 External rope-down device for 2 persons, fixed provisions RH 3.9 8.61 06-24009-B L8534-002-21 External rope-down device for 2 persons, detachable parts LH 13.1 28.91 06-24009-B L8534-002-22 External rope-down device for 2 persons, detachable parts RH 13.1 28.91 06-26011-C L8511-002-10 Cargo hook mirrors RH, fixed provisions 0.8 1.81 06-26011-C L8511-002-20 Cargo hook mirrors RH, detachable parts 3.9 8.61 06-27022-B L8511-005-10 Dual cargo hook system, fixed provisions 4.3 9.51 06-27022-B L8511-005-20 Dual cargo hook system, detachable parts 21.5 47.41 06-31012-B L8531-001-00 External loudspeaker system with siren 11.5 25.41 06-45020-A L3346-300-10 Search light SX16, fixed provisions 5.6 12.31 06-45020-A L3346-300-20 Search light SX16, detachable parts, without vendor parts. 10.1 22.31 06-45020-A L3346-500-10 Search light SX16, vendor parts 23.0 50.71 06-45023-B L3343-003-00 Landing & search light, 450 W 3.1 6.81 06-65004-B L2625-003-00 2nd portable fire extinguisher 2.8 6.21 06-67044-B L2563-801-06 ELT C406-N HM (Artex) incl. NAV. opt. 3.3 7.31 06-81009-B L8503-001-10 Fire extinguishing bucket attachment (Bambi Bucket),

fixed provisions0.8 1.8


Weight[lb]

1 07-27001-B L2522-007-00 3 forward passenger seats, facing backwards with 4 point safety harness

38.1 84.0

1 07-27004-B L2522-004-10 Utility seats for 3 rear passengers, model EUROCOPTER®, fixed provisions

1.2 2.6

1 07-27004-B L2522-004-20 Utility seats for 3 rear passengers, model EUROCOPTER®, detachable parts

33.2 73.2

1 07-40005-B L2513-220-00 Washable floor covering for cockpit, cabin and cargo compartment

11.5 25.4

1 07-40017-A L8552-001-00 Sealed cabin floor 0.3 0.71 07-50027-B L5231-002-00 Extended opening fasteners for clam-shell doors 0.3 0.71 07-50028-A L5213-001-11 Sliding door fastener, intermediate and max. position, LH 1.0 2.21 07-50028-A L5213-001-21 Sliding door fastener, intermediate and max. position, RH 1.0 2.21 07-50035-B L8504-813-00 Spoiler position for cockpit doors 1.1 2.41 07-60015-B L2514-014-00 Variable tie-down net 3.3 7.31 07-70043-A AAT-30100-001-2 Disaster Management Kit - Air Ambulance Technology (AAT) 74.8 164.91 Stretcher "Rescue" foldable for Helicopter Floor, LH - AAT1 Stretcher "Rescue" foldable for Helicopter Floor, RH - AAT1 Medical Seat stationary, front LH - AAT1 Medical Seat stationary, front RH - AAT1 Medical Device Holder, front center - AAT1 Floor Adapter for Medical Seats & Medical Device Holder - AAT1 Accessories - AAT1 Installation, Certifcation & Documentation - AAT1 Aluminium Oxygen Bottle 3,0 lt. - AAT1 Monitor & Defibrillator Argus Pro Life Care - Schiller2 Cervical Collar Set Perfit ACE & Mini Perfit ACE - Ambu1 Blood Glucose Meter Omnitest Plus - Braun1 Respiration Backpack incl. contents - Weinmann


Page 80 of 202 135.09.101.01

Technical Data

Avionics

Subtotal: 538.3 1,187.03% weight margin: 16.1 35.6

Subtotal (incl. margin): 554.4 1,222.6

Total: 2,031.3 4,479.0

1 Emergency Backpack incl. DIN13232-N contents - Weinmann2 Cervical Collar Set Perfit ACE & Mini Perfit ACE - Ambu


Weight[lb]


pilot and copilot1 Transponder (Mode S) GTX 330 (Garmin)1 Distance Measuring Equipment DME CDM 451 (Chelton)1 Marker beacon receiver/ lights KR 21 (Honeywell)1 Avionics/Radio master switches (Special EUROCOPTER®)1 GPS/NAV/COM GNS 430 (Garmin), copilot,

interfaced with FCDS (GPS stand-alone)1 GPS/NAV/COM GNS 430 (Garmin), pilot, interfaced with FCDS1 2” std-by horizon AI 804 DC (Goodrich),

incl. emergency battery1 MEGHAS - Flight Control Display System (FCDS) -



1 08-16061-A L2341-193-40 Digital Audio Control System ACP53 (NAT), PAX 3.6 7.91 08-21014-C L3441-090-04 Radar altimeter KRA 405 B (Honeywell) 3.5 7.71 08-24015-C L3452-092-09 ADF control unit CDF-552 (Chelton/Wulfsberg) 1.2 2.61 08-24015-C L3452-092-17 ADF receiver DF-431B, (Chelton/Wulfsberg) 9.6 21.21 08-31034-B L2571-002-00 Radar radome for RDR 1600 4.8 10.61 08-31034-B L3443-004-00 Search and rescue weather radar RDR 1600 (Telephonics) 16.7 36.81 08-53002-B L2212-400-00 MEGHAS Sensor Kit 17.0 37.51 08-54001-C L3411-001-00 Copilot pitot static system 1.5 3.31 08-65004-B L3443-010-00 Video Radar Unit (VRU) 5.0 11.01 08-72001-B L2212-001-00 Digital Automatic Flight Control System - DAFCS 27.0 59.5


Weight[lb]


Technical Data


General Equipment


Weight[lb]


a.The protective capability is degraded with the simultaneous fitment of: cargo hook mirror, search light SX16, radar radome.

8.2 18.11 05-22014-A L5611-002-00 Tinted front windshields 1.2 2.61 05-23006-B L7165-002-00 Engine compressor wash kit 3.2 7.11 05-25016-D L7161-001-10 Sand filter system, fixed provisions 11.3 24.91 05-25016-D L7161-001-20 Sand filter system, detachable parts 26.2 57.81 05-26012-B L1241-001-00 Anti-corrosion protection 5.2 11.51 05-31025-B L5211-002-00 Sliding windows in sliding doors 1.9 4.21 05-31026-C L5621-001-00 Tinted window for cockpit doors 0.0 0.01 05-31027-B L5633-001-10 Window in clam-shell door, LH 0.8 1.81 05-31027-B L5633-001-20 Window in clam-shell door, RH 0.8 1.81 05-31028-C L2524-030-10 IFR - training screen, fixed provisions 0.1 0.21 05-31028-C L2524-030-20 IFR - training screen, detachable parts 1.6 3.51 05-31045-A L5211-001-11 Lockable sliding window in copilots' door 0.1 0.21 05-31045-A L5211-001-12 Lockable sliding window in pilots' door 0.1 0.21 05-31086-A L5211-002-01 Ram air deflectors sliding doorsb

b.Requires L5211-002-00 Sliding windows in sliding doors.

0.4 0.91 05-31098-A L5211-001-01 Ram air deflectors cockpit doors 0.6 1.31 05-32007-B L3042-001-00 Windshield wiper system 5.0 11.01 05-34003-B L2576-002-00 Dampers for avionics compartment 1.8 4.01 05-36007-B L8532-002-40 Multifunction step RH (instead of std. boarding step) 4.9 10.81 05-37017-B L6721-001-00 Covers for copilot flight controls -2.5 -5.51 05-39008-B L3113-004-20 Illuminated chart holder for copilot side 0.9 2.01 05-42041-A L2105-005-00 Air conditioning system 55.0 121.31 05-81032-C L2818-100-10 Internal long range fuel tank system, fixed provisions 2.6 5.71 05-81032-C L2818-100-20 Internal long range fuel tank system, detachable partsc

c.No simutaneous fitment with the stretcher of the disaster management kit.

36.1 79.61 05-81033-B L2812-001-00 Self sealing fuel supply tanks 4.5 9.91 05-85008-C L2843-001-00 Fuel management system (Fuel flow meters) 1.2 2.61 05-92009-B L6611-001-10 Main rotor blade folding: basic kit 1.3 2.91 05-92009-B L6611-001-20 Main rotor blade folding: fixed provisions for ground

handling kitd

d.Requires L6611-001-10 Main rotor blade folding: basic kit.

0.8 1.8



Page 82 of 202 135.09.101.01

Technical Data

Missions Equipment

Interior Layout

Avionics


Weight[lb]



21.9 48.31 06-27027-A L8511-003-10 Cargo hook weighing system, fixed provisions 0.2 0.41 06-27027-A L8511-003-20 Cargo hook weighing system, detachable parts 1.5 3.31 06-46001-B L3344-001-00 Strobe lights, white 1.4 3.11 06-61015-B L3215-001-10 Emergency floats, fixed provisions 7.8 17.21 06-61015-B L3215-001-21 Emergency floats, detachable parts 64.6 142.41 06-65002-B L2566-001-00 Emergency hammer 0.2 0.41 06-66009-B L3322-001-00 Boarding step illumination 0.2 0.4


Weight[lb]

1 07-15016-B L2512-003-10 Height adjustable pilot seat instead of standard pilot seat 1.8 4.01 07-15016-B L2512-003-20 Height adjustable copilot seat instead of standard copilot seat 1.8 4.01 07-30012-B L2581-001-00 Enhanced sound proofing kit 4.8 10.61 07-30013-B L2524-002-00 Separation curtain for cockpit / cabin 2.1 4.61 07-50026-B L5231-001-00 One-hand latching system for clam-shell doors 1.0 2.21 07-50030-B L8512-003-00 Abrasion protection at sliding door 0.2 0.41 07-50034-B L5212-001-00 Jettisonable cockpit doors 1.2 2.61 07-50036-B L2514-012-00 Covers for sliding door fairing LH/RH 0.1 0.21 07-50039-B L5211-010-00 Door catch system for cockpit doors 0.1 0.21 07-50039-B L5211-011-00 Door catch system for sliding doors 0.2 0.41 07-60014-B L2514-013-00 Map case in sliding doors LH/RH 1.4 3.1


Weight[lb]


7.3 16.1


20.5 45.2


0.5 1.1


7.7 17.0

1 08-16061-A L2341-006-63 Voice alert generation for DACS (NAT) 0.0 0.01 08-35007-B L3442-881-00 TAS 620 (Avidyne) interface with GNS430 0.2 0.41 08-35007-C L2327-001-01 Traffic Advisory System TAS 620 (Avidyne)a

a.Requires L3442-881-00 TAS 620 (Avidyne) interface with GNS430.

9.5 20.91 08-46040-A L3168-092-07 Digital moving map EURONAV IV+ -RN6 (Euro Avionics),

interfaced with FCDSb

b.Approval for VFR only, maps and special options not included.

5.4 11.9

1 08-53004-B L3424-000-00 AHRS Free Steering Mode 0.5 1.11 08-81018-C L2321-007-00 M’ARMS® Cockpit Voice and Flight Data Recorder (CVFDR),



Technical Data





Weight[lb]




0.8 1.8


0.3 0.7


Weight[lb]



Weight[lb]


0.3 0.7


Weight[lb]



Page 84 of 202 135.09.101.01

Technical Data


4.3.1.4.1Evacuation Mission (MEDEVAC)

Radius of Action


Mission profile• Take-off in SL (max. 2910 kg)• Climb flight AEO-MCP from SL to 3000ft with VY (65KIAS)• Level flight in 3000ft with VH• Landing, pick-up of 2 patients and take-off in SL• Descent from 3000ft to SL with R/D of -1500 fpm (80KIAS)• Climb flight AEO-MCP from SL to 3000ft with VY (65KIAS)• Level flight in 3000ft with VH• Descent from 3000ft to SL with R/D of -1500 fpm (80KIAS)• Landing in SL

Mission Parameters

Drag relevant equipment installed: Radar radome RDR1600, external loudspeaker system

Equipment not installed: External rope down device (RH, LH)Search light SX16Cargo hook system and mirrors3 forward passenger seatsUtility seats for 3 rear passengers



Temperature: ISA


Empty weight equippeda

a.Total Weight (refer to 4.3.1.2.Basic Mission Configuration) minus the weight ofthe uninstalled equipment.

1871 4126

Crew (4) 340 750

Reserve fuel 71 157

Trip fuel 489 1078


Patient (2)b

b. Patient weight considered for return leg.

170 375


Technical Data


0 20 40 60 80 100 120 140 150

2300

2400

2500

2600

2700

2800

2900

Pla

nned

TO

W [k

g]




Page 86 of 202 135.09.101.01

Technical Data

4.3.1.4.2Search And Rescue Mission (SAR)

Radius of action versus search time

For a search phase of 2 minutes the calculated maximum radius of action for the mission below is: 124 nm (230 km).

For a radius of action of 10 nm the calculated maximum search time for the mission below is: 143.5 minutes.

Mission profile• Take-off in SL (max. 2910 kg)• Climb flight AEO-MCP from SL to 3000ft with VY (65KIAS)• Level flight in 3000ft with VH• Descent from 3000ft to SL with R/D of -1500 fpm (80KIAS)• Search phase in SL, 2 minutes• Rescue phase (pick-up of rescued person) in SL with HOGE, 5 minutes• Climb flight AEO-MCP from SL to 3000ft with VY (65KIAS)• Level flight in 3000ft with VH• Descent from 3000ft to SL with R/D of -1500 fpm (80KIAS)• Landing in SL

Mission Parameters

Drag relevant equipment installed: Radar radome RDR1600, external loudspeaker system, car-go hook system, search light SX16

Equipment not installed: External rope down device (RH, LH)Cargo hook mirrors3 forward passenger seatsUtility seats for 3 rear passengers1 stretcher and locker system of the disaster management kit



Temperature: ISA




1908 4207

Crew (3) 255 562

Reserve fuel 66 146

Trip fuel 494 1089


Patient (1)b

b. Patient weight considered for return leg

85 187


Technical Data

Figure 4.18: Search time versus radius of action diagram

0 20 40 60 80 100 120 140 150

0

30

60

90

120

150

Sea

rch

time

[min

]



Page 88 of 202 135.09.101.01

Technical Data

4.3.1.4.3Intervention Mission

Radius of action


Mission profile• Take-off in SL (max. 2910 kg)• Climb flight AEO-MCP from SL to 3000ft with VY (65KIAS)• Level flight in 3000ft with VH• Descent from 3000ft to SL with R/D of -1500 fpm (80KIAS)• Rope-down phase (dropping off special unit) in SL with HOGE, 5 minutes• Climb flight AEO-MCP from SL to 3000ft with VY (65KIAS)• Level flight in 3000ft with VH• Descent from 3000ft to SL with R/D of -1500 fpm (80KIAS)• Landing in SL

Mission Parameters

Drag relevant equipment installed: Radar radome RDR1600, external loudspeaker system, rope-down device (RH, LH)

Equipment not installed: External rope down device (RH, LH)Cargo hook system and mirrorsSearch light SX16Disaster management kit

Bleed air heating: Off


Temperature: ISA




1894 4176

Crew (1) 85 187

Special unit (5)b

b. 110 kg / 243 lb each

550 1213

Reserve fuel 61 135

Trip fuel 320 706



Technical Data


0 20 40 60 80 100 120 140

0

200

400

600

800

Pay

load

[kg]


5 Intervention Team Members @ 110kg


Page 90 of 202 135.09.101.01

Technical Data

4.3.2 Disaster Management (Aerolite)The Disaster Management Kit is based on a modular concept with various optional components medi-cal evacuation. The interior is designed to give maximum room and comfort to the medical crew andpatient. The kit is quick detachable for a fast mission configuration change.



EVACUATION

SEARCH AND RESCUE

Figure 4.20: Disaster Management Kit - Aerolite STC

Pilots 1 or 2

Medics 2

Patient 2

Pilots 1 or 2

Medics 2

Patient 1


Technical Data

INTERVENTION


Baseline Aircraft

Subtotal: 1,445.0 3,208.31.5% weight margin: 21.8 48.1


General Equipment

Pilots 1 or 2

Pax 6


Weight[lb]

1 00-10002-A L0000-002-00 EC135 Baseline Aircraft 135.09.100.01 E 1455.0 3208.31 L0000-003-01 2 Turbomeca ARRIUS 2B2 turbine engines 0.0 0.01 L0000-003-02 2 Pratt & Whitney PW206B2 turbine engines 0.0 0.0


Weight[lb]









Page 92 of 202 135.09.101.01

Technical Data

Mission Equipment

Interior Layout


Weight[lb]




Weight[lb]


38.1 84.0


1.2 2.6


33.2 73.2


11.5 25.4

1 07-40017-A L8552-001-00 Sealed cabin floor 0.3 0.71 07-50027-B L5231-002-00 Extended opening fasteners for clam-shell doors 0.3 0.71 07-50028-A L5213-001-11 Sliding door fastener, intermediate and max. position, LH 1.0 2.21 07-50028-A L5213-001-21 Sliding door fastener, intermediate and max. position, RH 1.0 2.21 07-50035-B L8504-813-00 Spoiler position for cockpit doors 1.1 2.41 07-60015-B L2514-014-00 Variable tie-down net 3.3 7.31 07-70045-A AEL-30100-004-2 Disaster Management Kit - Aerolite (AEL) 96.5 212.81 Stretcher "Cirrus 1000" foldable, LH, fix provisions - AEL1 Stretcher "Cirrus 1000" foldable, LH, detachable parts - AEL1 Stretcher "Cirrus 1000" foldable, RH, fix provisions - AEL1 Stretcher "Cirrus 1000" foldable, RH, detachable parts - AEL1 Pax Seat stationary, front LH - AEL1 Pax Seat stationary, front RH - AEL1 Life Support Module, front center - AEL1 Floor Frame for Pax Seats & Life Support Module - AEL1 Installation, Certifcation & Documentation - AEL1 Carbon Oxygen Bottle 3,0 lt. - AEL1 Monitor & Defibrillator Argus Pro Life Care - Schiller2 Infusion System Power Infuser - Zoll1 Blood Glucose Meter Omnitest Plus - Braun


Technical Data

Avionics



Total: 2,053.6 4,528.2

1 Respiration Backpack incl. contents - Weinmann1 Emergency Backpack incl. DIN13232-N contents - Weinmann2 Cervical Collar Set Perfit ACE & Mini Perfit ACE - Ambu


Weight[lb]


pilot and copilot1 Transponder (Mode S) GTX 330 (Garmin)1 Distance Measuring Equipment DME CDM 451 (Chelton)1 Marker beacon receiver/ lights KR 21 (Honeywell)1 Avionics/Radio master switches (Special EUROCOPTER®1 GPS/NAV/COM GNS 430 (Garmin), copilot,

interfaced with FCDS (GPS stand-alone)1 GPS/NAV/COM GNS 430 (Garmin), pilot, interfaced with FCDS1 2” std-by horizon AI 804 DC (Goodrich),






Weight[lb]


Page 94 of 202 135.09.101.01

Technical Data


General Equipment


Weight[lb]


a.The protective capability is degrated with the simultanous fitment of: cargo hook mirror, search light SX16, radar radome.




c.No simultaneous fitment with stretcher of the disaster management kit.


handling kitd


0.8 1.8



Technical Data

Missions Equipment

Interior Layout

Avionics


Weight[lb]



21.9 48.31 06-27027-A L8511-003-10 Cargo hook weighing system, fixed provisions 0.2 0.41 06-27027-A L8511-003-20 Cargo hook weighing system, detachable parts 1.5 3.31 06-46001-B L3344-001-00 Strobe lights, white 1.4 3.11 06-61015-B L3215-001-10 Emergency floats, fixed provisions 7.8 17.21 06-61015-B L3215-001-21 Emergency floats, detachable parts 64.6 142.41 06-65002-B L2566-001-00 Emergency hammer 0.2 0.41 06-66009-B L3322-001-00 Boarding step illumination 0.2 0.4


Weight[lb]



Weight[lb]


7.3 16.1


20.5 45.2


0.5 1.1


7.7 17.0



9.5 20.91 08-46040-A L3168-092-07 Digital moving map EURONAV IV+ -RN6 (Euro Avionics), i

nterfaced with FCDSb


5.4 11.9




Page 96 of 202 135.09.101.01

Technical Data





Weight[lb]




0.8 1.8


0.3 0.7


Weight[lb]



Weight[lb]


0.3 0.7


Weight[lb]



Technical Data



Radius of action


Mission profile• Take-off in SL (max. 2910 kg)• Climb flight AEO-MCP from SL to 3000ft with VY (65KIAS)• Level flight in 3000ft with VH• Descent from 3000ft to SL with R/D of -1500 fpm (80KIAS)• Landing, pick-up of 2 patients and take-off in SL• Climb flight AEO-MCP from SL to 3000ft with VY (65KIAS)• Level flight in 3000ft with VH• Descent from 3000ft to SL with R/D of -1500 fpm (80KIAS)• Landing in SL

Mission Parameters





Temperature: ISA




1893 4174

Crew (4) 340 750

Reserve fuel 71 157

Trip fuel 489 1078


Patient (2)b


170 375


Page 98 of 202 135.09.101.01

Technical Data


0 20 40 60 80 100 120 140 150

2300

2400

2500

2600

2700

2800

2900

Pla

nned

TO

W [k

g]




Technical Data

4.3.2.4.2Search and Rescue Mission (SAR)


For a search phase of 2 minutes the calculated maximum radius of action for the mission below is: 123.5 nm (229 km).


Mission profile• Take-off in SL (max. 2910 kg)• Climb flight AEO-MCP from SL to 3000ft with VY (65KIAS)• Level flight in 3000ft with VH• Descent from 3000ft to SL with R/D of -1500 fpm (80KIAS)• Search phase in SL, 2 minutes• Rescue phase (pick-up of rescued person) in SL with HOGE, 5 minutes• Climb flight AEO-MCP from SL to 3000ft with VY (65KIAS)• Level flight in 3000ft with VH• Descent from 3000ft to SL with R/D of -1500 fpm (80KIAS)• Landing in SL

Mission Parameters


Equipment not installed: External rope down device (RH, LH)Cargo hook mirrors3 forward passenger seatsUtility seats for 3 rear passengers1 stretcher system of the disaster management kit



Temperature: ISA




1934 4265

Crew (3) 255 562

Reserve fuel 66 146

Trip fuel 494 1089


Patient (1)b


85 187


Page 100 of 202 135.09.101.01

Technical Data


0 20 40 60 80 100 120 140 150

0

30

60

90

120

150

Sea

rch

time

[min

]



Technical Data


Radius of action



Mission Parameters





Temperature: ISA




1894 4176

Crew (1) 85 187

Special unit (5)b

b.110 kg / 243 lb each

550 1213

Reserve fuel 61 135

Trip fuel 320 706



Page 102 of 202 135.09.101.01

Technical Data

Figure 4.23: Radius of action diagram

0 20 40 60 80 100 120 140

0

200

400

600

800

Pay

load

[kg]




Technical Data

4.3.3 Disaster Management (Bucher Leichtbau)The Disaster Management Kit provides the equipment to carry out fast and light rescue missions. Thecabin layout can be adapted according to your special requirements and can be extended with additi-onal equipment. The system is designed to accommodate all equipment without using special tools.



EVACUATION

SEARCH AND RESCUE

Figure 4.24: Disaster Management Kit Bucher Leichtbau STC

Pilots 1 or 2

Medics 2

Patient 2

Pilots 1 or 2

Medics 2

Patient 1


Page 104 of 202 135.09.101.01

Technical Data

INTERVENTION


Baseline Aircraft



General Equipment

Pilots 1 or 2

Pax 6


Weight[lb]



Weight[lb]









Technical Data

Mission Equipment

Interior Layout


Weight[lb]




Weight[lb]


38.1 84.0


1.2 2.6


33.2 73.2


11.5 25.4

1 07-40017-A L8552-001-00 Sealed cabin floor 0.3 0.71 07-50027-B L5231-002-00 Extended opening fasteners for clam-shell doors 0.3 0.71 07-50028-A L5213-001-11 Sliding door fastener, intermediate and max. position, LH 1.0 2.21 07-50028-A L5213-001-21 Sliding door fastener, intermediate and max. position, RH 1.0 2.21 07-50035-B L8504-813-00 Spoiler position for cockpit doors 1.1 2.41 07-60015-B L2514-014-00 Variable tie-down net 3.3 7.31 07-70041-A BUL-30100-002-2 Disaster Management Kit - Bucher Leichtbau (BUL) 71.7 158.11 Stretcher "Ferno" foldable, LH - BUL1 Stretcher "Ferno" foldable, RH - BUL1 Medical Seat stationary, front LH - BUL1 Medical Seat stationary, front RH - BUL1 Universal Center Console, front center - BUL1 Retainer for Argus Pro Life Care - BUL1 Floor Adapter for Medical Seats & Universal

Center Console - BUL1 Installation, Certifcation & Documentation - BUL1 Carbon Oxygen Bottle 3,0 lt. - BUL1 Monitor & Defibrillator Argus Pro Life Care - Schiller2 Infusion System Power Infuser - Zoll1 Blood Glucose Meter Omnitest Plus - Braun


Page 106 of 202 135.09.101.01

Technical Data

Avionics



Total: 2,028.1 4,471.9

1 Respiration Backpack incl. contents - Weinmann1 Emergency Backpack incl. DIN13232-N contents - Weinmann2 Cervical Collar Set Perfit ACE & Mini Perfit ACE - Ambu


Weight[lb]


pilot and copilot1 Transponder (Mode S) GTX 330 (Garmin)1 Distance Measuring Equipment DME CDM 451 (Chelton)1 Marker beacon receiver/ lights KR 21 (Honeywell)1 Avionics/Radio master switches (Special EUROCOPTER®1 GPS/NAV/COM GNS 430 (Garmin), copilot,

interfaced with FCDS (GPS stand-alone)1 GPS/NAV/COM GNS 430 (Garmin), pilot, interfaced with FCDS1 2” std-by horizon AI 804 DC (Goodrich), incl. emergency batte-

ry1 MEGHAS - Flight Control Display System (FCDS) -





Weight[lb]


Technical Data


General Equipment


Weight[lb]


a.The protective capability is degraded with the simultaneous fitment of: cargo hook mirror, search light SX16, radar radome.




c.No simultaneous fitment with the stretcher of the disaster management kit.


handling kitd


0.8 1.8



Page 108 of 202 135.09.101.01

Technical Data

Missions Equipment

Interior Layout

Avionics


Weight[lb]

1 06-11022-C L3272-001-10 Snow skids, fixed provisions 0.9 2.01 06-11022-C L3272-001-20 Snow skids, detachable parts 21.9 48.31 06-27027-A L8511-003-10 Cargo hook weighing system, fixed provisions 0.2 0.41 06-27027-A L8511-003-20 Cargo hook weighing system, detachable partsa


1.5 3.31 06-46001-B L3344-001-00 Strobe lights, white 1.4 3.11 06-61015-B L3215-001-10 Emergency floats, fixed provisions 7.8 17.21 06-61015-B L3215-001-21 Emergency floats, detachable parts 64.6 142.41 06-65002-B L2566-001-00 Emergency hammer 0.2 0.41 06-66009-B L3322-001-00 Boarding step illumination 0.2 0.4


Weight[lb]



Weight[lb]


7.3 16.1


20.5 45.2


0.5 1.1


7.7 17.0



9.5 20.91 08-46040-A L3168-092-07 Digital moving map EURONAV IV+ -RN6 (Euro Avionics),

interfaced with FCDSb


5.4 11.9




Technical Data





Weight[lb]




0.8 1.8


0.3 0.7


Weight[lb]



Weight[lb]


0.3 0.7


Weight[lb]



Page 110 of 202 135.09.101.01

Technical Data



Radius of action


Mission profile• Take-off in SL (max. 2910 kg)• Climb flight AEO-MCP from SL to 3000ft with VY (65KIAS)• Level flight in 3000ft with VH• Descent from 3000ft to SL with R/D of -1500 fpm (80KIAS)• Landing, pick-up of 2 patients and take-off in SL• Climb flight AEO-MCP from SL to 3000ft with VY (65KIAS)• Level flight in 3000ft with VH• Descent from 3000ft to SL with R/D of -1500 fpm (80KIAS)• Landing in SL

Mission Parameters





Temperature: ISA




1867 4117

Crew (4) 340 750

Reserve fuel 71 157

Trip fuel 489 1078


Patient (2)b


170 375


Technical Data


0 20 40 60 80 100 120 140 15

2300

2400

2500

2600

2700

2800

2900

Pla

nned

TO

W [k

g]




Page 112 of 202 135.09.101.01

Technical Data

4.3.3.4.2Search and Rescue Mission (SAR)


For a search phase of 2 minutes the calculated maximum radius of action for the mission below is: 124 nm (230 km).


Mission profile• Take-off in SL (max. 2910 kg)• Climb flight AEO-MCP from SL to 3000ft with VY (65 KIAS)• Level flight in 3000ft with VH• Descent from 3000ft to SL with R/D of -1500 fpm (80 KIAS)• Search phase in SL, 2 minutes• Rescue phase (pick-up of rescued person) in SL with HOGE, 5 minutes• Climb flight AEO-MCP from SL to 3000ft with VY (65 KIAS)• Level flight in 3000ft with VH• Descent from 3000ft to SL with R/D of -1500 fpm (80 KIAS)• Landing in SL

Mission Parameters


Equipment not installed: External rope down device (RH, LH)Cargo hook mirrors3 forward passenger seatsUtility seats for 3 rear passengers1 stretcher system of the disaster management kit



Temperature: ISA



Crew (3) 255 562

Reserve fuel 66 146

Trip fuel 494 1089


Patient (1)a


85 187


Technical Data


0 20 40 60 80 100 120 140 150

0

30

60

90

120

150

Sea

rch

time

[min

]



Page 114 of 202 135.09.101.01

Technical Data


Radius of action



Mission Parameters





Temperature: ISA




1894 4176

Crew (1) 85 187

Special unit (5)b

b. 110 kg / 243 lb each

550 1213

Reserve fuel 61 135

Trip fuel 320 706



Technical Data


0 20 40 60 80 100 120 140

0

200

400

600

800

Pay

load

[kg]




Page 116 of 202 135.09.101.01

Technical Data

4.4 Corporate

The EC135 Corporate configuration offers comfortable, classic surroundings. Genuine materials suchas real wood and leather combined with highly accurate production methods ensure a lightweight inte-rior that maximizes the helicopter's range. The elegant interior design with stylish seats and cabinetscreates an exclusive ambience. This configuration can comfortably accommodate up to six passengersplus a pilot, providing ample legroom space. An optional version accommodates sevens passengersand a pilot in equally comfortable conditions.

A combination of two rear seats (3 point safety seat belts), accompanied with an elegant cabinet in themiddle ensures the most comfortable travelling in this class by providing two armrests in the windowniches and an armrest mounted on the cabinet. For access to cabinet the armrest can be folded back-wards. On request an icebox and two cup holders are available. In the front row of the passenger cabin3 seats covered with leather are installed. The middle seat can be exchanged with a front cabinet onrequest. The pilot seats (5 point safety seat belts) are upholstered and covered with leather to providea harmonic interior. The carpet completes a comfortable impression of the design line. Safety belts areadjusted to the leather color of the seats and sides of the cabinet. To underline the comfortable andour prestigious approach the belt shutters are made of metal and are brushed.

For further information concerning components, features, colors and materials of the Corporate kitplease refer to the technical data support document „EC135 Corporate & Executive Interior Cata-logue”.

Figure 4.28: Picture shows optional equipment of an EC135 5 seats corporate package


Technical Data

4.4.1 Mission ParameterFlight Rules: IFRInstrumentation: Glass Cockpit (MEGHAS)Cat-A: Yes

4.4.2 Basic Mission Configuration

Baseline Aircraft



General Equipment

Pilots 1 or 2

Pax 5


Weight[lb]



Weight[lb]

1 05-02016-C L1111-004-00 Multicolor exterior painting instead of single color painting 2.0 4.41 05-03007-C L2562-001-00 First aid kita 1.5 3.31 05-12001-B L5232-001-00 Multifunction handle on the main gear box cowling

(LH and RH)0.6 1.3

1 05-22007-B L7924-001-00 Fuzz burners for engines 1.2 2.61 05-22008-C L2621-001-00 Engine fire extinguishing system 3.6 7.91 05-22014-A L5371-001-00 Engine outlet heat protection 1.2 2.61 05-23006-B L7165-002-00 Engine compressor wash kit 3.2 7.11 05-30003-A L2565-002-00 Flash light copilot side 0.2 0.41 05-31026-C L2514-002-00 Tinted sun shades for cockpit windshield roof section 1.9 4.21 05-33001-B L3113-001-00 Slant panel 0.8 1.81 05-33002-B L3113-004-00 Center console 2.2 4.91 05-34002-B L2576-001-00 Avionics compartment 4.2 9.31 05-37016-C L6701-001-00 Copilot flight controls 6.0 13.21 05-38010-B L3111-001-04 7" copilot instrument panel with glare shield 2.7 6.01 05-39006-B L2514-003-01 Map case in copilot door 0.5 1.11 05-39007-B L3111-001-10 Map cases on instrument panel glare shield 0.6 1.31 05-39008-B L3113-004-10 Illuminated chart holder for pilot side 1.0 2.21 05-41004-C L2104-100-00 Bleed air heating system 6.6 14.61 05-42041-A L2105-005-00 Air conditioning system 55.0 121.31 05-61010-B L2433-006-00 Battery, type "Saft", ULM, 40 Ah, 24 V


1 05-62010-C L2420-005-00 AC system (50 VA) 1.9 4.2


Page 118 of 202 135.09.101.01

Technical Data

Mission Equipment

Interior Layout

1 05-63003-B L2432-001-00 Starter/generator (2 x 200 A, 28V DC) instead of standard generator

3.6 7.9




Weight[lb]

1 06-12008-C L3217-001-00 Reinforced rear landing gear cross tube 1.0 2.21 06-45023-B L3343-003-00 Landing & search light, 450 W 3.1 6.81 06-67044-B L2563-801-06 ELT C406-N HM (Artex) incl. NAV. opt. 3.3 7.3


Weight[lb]

1 07-30012-B L2581-001-00 Enhanced sound proofing kit 4.8 10.61 07-30015-B L2524-001-00 Separation wall for cabin / cargo compartment 4.4 9.71 07-50036-B L2514-012-00 Covers for sliding door fairing LH/RH 0.1 0.21 07-50039-B L5211-010-00 Door catch system for cockpit doors 0.1 0.21 07-50039-B L5211-011-00 Door catch system for sliding doors 0.2 0.41 07-60014-B L2514-013-00 Map case in sliding doors LH/RH 1.4 3.11 07-60015-B L2514-014-00 Variable tie-down net 3.3 7.31 07-80027-A AAT-30200-004-2 5 Corporate Passenger Transport 107.2 236.41 Corporate carpet cockpit1 Corporate carpet cabin1 Corporate carpet cargo compartment1 Armrest in rear window LH / RH4 Corporate covers for controls (collective and cyclic)1 Corporate passenger seat (2 front)1 Corporate passenger seats (2 rear)1 Corporate passenger seat (1 front, middle)1 Corporate pilot seat heightadjustable

(instead of std. pilot seat)1 Corporate co-pilot heightadjustable

(instead of std. pilot seat)1 Corporate cabinet (rear) with armrest5 Passenger service unit (air outlets and reading lights)1 07-86001-B L2525-100-35 Special painted interior 0.1 0.21 07-90006-B L2514-011-00 Retractable coat hooks (2ea) in rear cabin 0.1 0.2


Weight[lb]


Technical Data

Avionics



Total: 1,864.3 4,110.8

4.4.3 Further Available Equipment

General Equipment


Weight[lb]

1 08-00031-A L2300-011-05 AV PACK DP IFR GC G430 75.7 166.91 Digital Audio Control System (NAT), incl. AMU50,

ACP53 pilot and copilot1 Transponder (Mode S) GTX 330 (Garmin)1 Distance Measuring Equipment DME CDM 451 (Chelton)1 Marker beacon receiver/ lights KR 21 (Honeywell)1 Avionics/Radio master switches (Special EUROCOPTER®)1 GPS/NAV/COM GNS 430 (Garmin), copilot,

interfaced with FCDS (GPS stand-alone)1 GPS/NAV/COM GNS 430 (Garmin), pilot,

interfaced with FCDS1 2” std-by horizon AI 804 DC (Goodrich),


Dual (4xSMD45)1 AV Pack DP IFR GC G430, interconnection / wiring1 08-21014-C L3441-090-04 Radar altimeter KRA 405 B (Honeywell) 3.5 7.71 08-53002-B L2212-400-00 MEGHAS Sensor Kit 17.0 37.51 08-54001-C L3411-001-00 Copilot pitot static system 1.5 3.31 08-72001-B L2212-001-00 Digital Automatic Flight Control System - DAFCS 27.0 59.5


Weight[lb]

1 05-12002-B L2551-003-00 Additional 4 tie-down fittings for airline attachment rails 0.6 1.31 05-21015-B L8541-001-10 Wire strike protection system, fixed provisions 3.3 7.31 05-21015-B L8541-001-20 Wire strike protection system, detachable partsa 8.2 18.11 05-22014-A L5611-002-00 Tinted front windshields 1.2 2.61 05-25016-D L7161-001-10 Sand filter system, fixed provisions 11.3 24.91 05-25016-D L7161-001-20 Sand filter system, detachable parts 26.2 57.81 05-26012-B L1241-001-00 Anti-corrosion protection 5.2 11.51 05-31026-C L5621-001-00 Tinted window for cockpit doors 0.0 0.01 06-31026-C L5632-001-00 Tinted windows for passenger cabin,

(incl. sliding windows for sliding doors)0.6 1.3

1 05-31028-C L2524-030-10 IFR - training screen, fixed provisions 0.1 0.21 05-31028-C L2524-030-20 IFR - training screen, detachable parts 1.6 3.51 05-31045-A L5211-001-11 Lockable sliding window in copilots' door 0.1 0.21 05-31045-A L5211-001-12 Lockable sliding window in pilots' door 0.1 0.21 05-32007-B L3042-001-00 Windshield wiper system 5.0 11.01 05-34003-B L2576-002-00 Dampers for avionics compartment 1.8 4.01 05-37017-B L6721-001-00 Covers for copilot flight controls -2.5 -5.51 05-39008-B L3113-004-20 Illuminated chart holder for copilot side 0.9 2.01 05-81032-C L2818-100-10 Internal long range fuel tank system, fixed provisions 2.6 5.71 05-81032-C L2818-100-20 Internal long range fuel tank system, detachable parts 36.1 79.61 05-85008-C L2843-001-00 Fuel management system (Fuel flow meters) 1.2 2.6


Page 120 of 202 135.09.101.01

Technical Data

Mission Equipment

Interior Layout

Avionics

1 05-92009-B L6611-001-10 Main rotor blade folding: basic kit 1.3 2.91 05-92009-B L6611-001-20 Main rotor blade folding: fixed provisions

for ground handling kitb0.8 1.8

1 05-92009-B L6611-001-30 Main rotor blade folding: ground handling kit 0.0 0.01 05-93007-C L8544-002-00 Lashing points (wind speeds up to 100 kts) 0.7 1.51 05-93008-B L8544-001-00 Lashing points (wind speeds up to 40 kts) 2.4 5.31 05-93011-A L8544-003-10 Lashing points (ship landing), fixed provisions 4.2 9.31 05-93011-A L8544-003-20 Lashing points (ship landing), detachable parts 0.6 1.31 05-95001-C L1321-001-00 Cover kit for helicopter GSE GSE1 05-97001-C L6201-001-30 Accelerometers for Track and Balance system 0.0 0.0

a.The protective capability is degraded with the simultaneous fitment of: radar radome.b.Requires L6611-001-10 Main rotor blade folding: basic kit.


Weight[lb]

1 06-11021-B L3274-001-10 Settling protectors, fixed provisions 1.9 4.21 06-11021-B L3274-001-20 Settling protectors, detachable parts 7.9 17.41 06-11022-C L3272-001-10 Snow skids, fixed provisions 0.9 2.01 06-11022-C L3272-001-20 Snow skids, detachable partsa

a.No simultaneous fitment with settling protectors and vice versa.

21.9 48.31 06-46001-B L3344-001-00 Strobe lights, white 1.4 3.11 06-61015-B L3215-001-10 Emergency floats, fixed provisions 7.8 17.21 06-61015-B L3215-001-21 Emergency floats, detachable parts 64.6 142.41 06-65002-B L2566-001-00 Emergency hammer 0.2 0.41 06-66008-C L3353-005-00 Emergency lightsb

b.Boarding step illmination is already a part of this package and does not need to be selected separately.

2.9 6.41 06-66009-B L3322-001-00 Boarding step illumination 0.2 0.41 06-66010-B L3353-006-20 Illuminated signs "NO SMOKING/FASTEN SEAT BELT" 0.8 1.8


Weight[lb]

1 07-50026-B L5231-001-00 One-hand latching system for clam-shell doors 1.0 2.21 07-50034-B L5212-001-00 Jettisonable cockpit doors 1.2 2.6


Weight[lb]


7.3 16.1


20.5 45.2


0.5 1.1

1 08-15507-B L2315-092-00 IRIDIUM satellite phone AEROPHONE (Aerodata)incl. cockpit dial panel

4.7 10.4

1 08-15532-A L2341-195-40 VIP SATCOM – private modea 2.2 4.91 08-15532-A L2341-195-50 VIP SATCOM – wired handset, rear window niche RHa 0.6 1.31 08-16061-A L2341-006-63 Voice alert generation for DACS (NAT) 0.0 0.01 08-24015-C L3452-092-09 ADF control unit CDF-552 (Chelton/Wulfsberg) 1.2 2.61 08-24015-C L3452-092-17 ADF receiver DF-431B, (Chelton/Wulfsberg)b 9.6 21.2


Weight[lb]


Technical Data




1 08-31019-B L2571-001-00 Radar radome for RDR 2000 2.0 4.41 08-31019-B L3443-090-02 Color weather radar RDR 2000 (Honeywell)c 6.6 14.61 08-35007-B L3442-881-00 TAS 620 (Avidyne) interface with GNS430 0.2 0.41 08-35007-C L2327-001-01 Traffic Advisory System TAS 620 (Avidyne)d 9.5 20.91 08-46040-A L3168-092-07 Digital moving map EURONAV IV+ -RN6 (Euro Avionics),

interfaced with FCDSe5.4 11.9

1 08-53004-B L3424-000-00 AHRS Free Steering Mode 0.5 1.11 08-65004-B L3443-010-00 Video Radar Unit (VRU) 5.0 11.01 08-81018-C L2321-007-00 M’ARMS® Cockpit Voice and Flight Data Recorder (CVFDR),


a.Requires L2315-092-00 IRIDIUM satellite phone AEROPHONE (Aerodata) incl. cockpit dial panel.b.Requires L3452-092-09 ADF control unit CDF-552 (Chelton/Wulfsberg) and vice versa.c.Requires L2571-001-00 Radar Radome RDR2000.d.Requires L3442-881-00 TAS 620 (Avidyne) interface with GNS430.e.Requires L3443-010-00 Video Radar Unit (VRU).


Weight[lb]




0.8 1.8


0.3 0.7


Weight[lb]



Weight[lb]


0.3 0.7


Weight[lb]



Weight[lb]


Page 122 of 202 135.09.101.01

Technical Data

4.4.4 Material and color definitionThe default color line of the Corporate configuration is defined as SAHARA. Detailed information con-cerning this color line is given in the listing below.

Further color line schemes are avaiable on request. Please refer to the technical data support docu-ment „EC135 Interior Catalog”.

Option Material Color

VIP Pilot seat

Cover5-point savety beltsBuckles

LeatherPolyethylenMetall

Beige (CS 402)BeigeBrushed

VIP Copilot seat




VIP Passenger seats (2 front)




VIP Passenger seats (2 rear)




VIP Passenger seats (1 front, middle)




VIP Cabinet rear

Side wallsTop / front coversLatches

LeatherWoodMetal

Beige (CS 402)Maple Burl (316)Brushed

VIP PSU (air outlets and lights)

Surface Metal Brushed

VIP Covers for controls (collective and cyclic)

Cover Leather Beige (CS 402)

VIP Carpet for cockpit, cabin and cargo compartment

Carpet machine tuftedCarpet edges

WoolLeather

Light Beige (ME 402)Beige (CS 402)

Armrest in rear window niche LH / RH


Special painted interior

Paint Light Ivory (RAL 1015)


Technical Data

4.4.5 Performance Data

Maximum Range


Mission profile• Take-off in SL (max 2910 kg)• Climb flight AEO-MCP from SL to 7000ft with VY (65KIAS)• Level flight in 7000ft with VBR• Descent from 7000ft to SL with R/D of -1000 fpm (80KIAS)• Landing in SL

Mission Parameters



Air conditioning system: Off


Temperature: ISA



Crew (1) 85 187

Passengers (5+1)a

a.Each passenger 85 kg / 187 lb. 5 passengers in cabin and 1 on copliot side.

510 1125

Reserve fuel 66 146

Trip fuel 384 847



Page 124 of 202 135.09.101.01

Technical Data

Figure 4.29: Payload versus range diagram

0 50 100 150 200 250 300 350

0

200

400

600

800

Pay

load

[kg]

Range [nm]

5+1 Passengers @ 85kg


Technical Data

Blank


Page 126 of 202 135.09.101.01

Technical Data

4.5 Executive

The EC135 Executive configuration provides passengers with an outstanding work environment: thereis ample room for up to four people. High-tech materials such as carbon fiber and lightweight alumi-num-alloy with the best and most precise manufacturing technologies give a stylish, modern appea-rance. Ergonomically-designed cabinets offer a well-balanced combination of space and elegance.

This exclusive interior layout comprises pilot (5 point safety seat belts) and passenger seats (3 pointsafety seat belts) covered with high quality leather. The safety seat belts are adjusted in harmony withthe seat leather and the metal buckles and shutters are of type "Brushed". Front and rear cabinet arecovered with the same leather type on the side and top sections. The insides of the cabinets provideadditional map cases, storage and holder for bottles. The cabin panels are covered with high qualitypaint. An exclusive carpet for the three cabin sections is bordered with leather and fits to the designprogram. The leather covers for the cyclic stick and the collective stick are adjusted to the design line.EC135 provides 5 PSU to provide fresh air and personal reading light to the passengers. These PSUare made of metal and type "Brushed" and enforce the elegance of this VIP solution.

For further information concerning components, features, colors and materials of the Corporate kitplease refer to the technical data support document „EC135 Corporate & Executive Interior Cata-logue”.

Figure 4.30: Typical Executive layout of an EC135a

a.3 point safety belts for passanger seats are standard. 4 point safety belts are available on request.


Technical Data



Baseline Aircraft



General Equipment

Pilots 1 or 2

Pax 4


Weight[lb]



Weight[lb]

1 05-02016-C L1111-004-00 Multicolor exterior painting instead of single color painting 2.0 4.41 05-03007-C L2562-001-00 First aid kita 1.5 3.31 05-12001-B L5232-001-00 Multifunction handle on the main gear box cowling

(LH and RH)0.6 1.3

1 05-22007-B L7924-001-00 Fuzz burners for engines 1.2 2.61 05-22008-C L2621-001-00 Engine fire extinguishing system 3.6 7.91 05-22014-A L5371-001-00 Engine outlet heat protection 1.2 2.61 05-23006-B L7165-002-00 Engine compressor wash kit 3.2 7.11 05-30003-A L2565-002-00 Flash light copilot side 0.2 0.41 05-31026-C L2514-002-00 Tinted sun shades for cockpit windshield roof section 1.9 4.21 05-33001-B L3113-001-00 Slant panel 0.8 1.81 05-33002-B L3113-004-00 Center console 2.2 4.91 05-34002-B L2576-001-00 Avionics compartment 4.2 9.31 05-37016-C L6701-001-00 Copilot flight controls 6.0 13.21 05-38010-B L3111-001-04 7" copilot instrument panel with glare shield 2.7 6.01 05-39006-B L2514-003-01 Map case in copilot door 0.5 1.11 05-39007-B L3111-001-10 Map cases on instrument panel glare shield 0.6 1.31 05-39008-B L3113-004-10 Illuminated chart holder for pilot side 1.0 2.21 05-41004-C L2104-100-00 Bleed air heating system 6.6 14.61 05-42041-A L2105-005-00 Air conditioning system 55.0 121.31 05-61010-B L2433-006-00 Battery, type "Saft", ULM, 40 Ah, 24 V


1 05-62010-C L2420-005-00 AC system (50 VA) 1.9 4.2


Page 128 of 202 135.09.101.01

Technical Data

Mission Equipment

Interior Layout


3.6 7.9




Weight[lb]



Weight[lb]

1 07-30012-B L2581-001-00 Enhanced sound proofing kit 4.8 10.61 07-30015-B L2524-001-00 Separation wall for cabin / cargo compartment 4.4 9.71 07-50036-B L2514-012-00 Covers for sliding door fairing LH/RH 0.1 0.21 07-50039-B L5211-010-00 Door catch system for cockpit doors 0.1 0.21 07-50039-B L5211-011-00 Door catch system for sliding doors 0.2 0.41 07-60014-B L2514-013-00 Map case in sliding doors LH/RH 1.4 3.11 07-60015-B L2514-014-00 Variable tie-down net 3.3 7.31 07-80029-A AEL-30200-001-2 4 Seat Executive VIP Configuration 132.1 291.31 Executive carpet cockpit1 Executive carpet for cabin1 Executive carpet for cargo compartment1 Armrest in rear window niche LH / RH1 Executive pilot seat, 5 point seat belts, heightadjustable

(instead of standard seat)1 Executive copilot seat, 5 point seat belts, heightadjustable

(instead of standard seat)1 Executive passenger seats (2 front)1 Executive passenger seats (2 rear)1 Executive cabinet (rear)1 Executive cabinet (front)2 Executive head set holder5 Executive Personal service unit (air outlets and reading lights)4 Executive covers for controls (collective and cyclic)2 Executive Adjustment Bleed Air Heating1 Executive Placards, Standard (Metal brushed)1 07-86001-B L2525-100-35 Special painted interior 0.1 0.21 07-90006-B L2514-011-00 Retractable coat hooks (2ea) in rear cabin 0.1 0.2


Weight[lb]


Technical Data

Avionics



Total: 1,890.0 4.167.4


General Equipment


Weight[lb]






Dual (4xSMD45)1 AV Pack DP IFR GC G430, interconnection / wiring1 08-21014-C L3441-090-04 Radar altimeter KRA 405 B (Honeywell) 3.5 7.71 08-53002-B L2212-400-00 MEGHAS Sensor Kit 17.0 37.51 08-54001-C L3411-001-00 Copilot pitot static system 1.5 3.31 08-72001-B L2212-001-00 Digital Automatic Flight Control System - DAFCS 27.0 59.5


Weight[lb]

1 05-12002-B L2551-003-00 Additional 4 tie-down fittings for airline attachment rails 0.6 1.31 05-21015-B L8541-001-10 Wire strike protection system, fixed provisions 3.3 7.31 05-21015-B L8541-001-20 Wire strike protection system, detachable partsa 8.2 18.11 05-22014-A L5611-002-00 Tinted front windshields 1.2 2.61 05-25016-D L7161-001-10 Sand filter system, fixed provisions 11.3 24.91 05-25016-D L7161-001-20 Sand filter system, detachable parts 26.2 57.81 05-26012-B L1241-001-00 Anti-corrosion protection 5.2 11.51 05-31026-C L5621-001-00 Tinted window for cockpit doors 0.0 0.01 06-31026-C L5632-001-00 Tinted windows for passenger cabin,

incl. sliding windows for sliding doors0.6 1.3

1 05-31028-C L2524-030-10 IFR - training screen, fixed provisions 0.1 0.21 05-31028-C L2524-030-20 IFR - training screen, detachable parts 1.6 3.51 05-31045-A L5211-001-11 Lockable sliding window in copilots' door 0.1 0.21 05-31045-A L5211-001-12 Lockable sliding window in pilots' door 0.1 0.21 05-32007-B L3042-001-00 Windshield wiper system 5.0 11.01 05-34003-B L2576-002-00 Dampers for avionics compartment 1.8 4.01 05-37017-B L6721-001-00 Covers for copilot flight controls -2.5 -5.51 05-39008-B L3113-004-20 Illuminated chart holder for copilot side 0.9 2.01 05-81032-C L2818-100-10 Internal long range fuel tank system, fixed provisions 2.6 5.71 05-81032-C L2818-100-20 Internal long range fuel tank system, detachable parts 36.1 79.61 05-85008-C L2843-001-00 Fuel management system (Fuel flow meters) 1.2 2.6


Page 130 of 202 135.09.101.01

Technical Data

Mission Equipment

Interior Layout

Avionics

1 05-92009-B L6611-001-10 Main rotor blade folding: basic kit 1.3 2.91 05-92009-B L6611-001-20 Main rotor blade folding: fixed provisions

for ground handling kitb0.8 1.8

1 05-92009-B L6611-001-30 Main rotor blade folding: ground handling kit 0.0 0.01 05-93007-C L8544-002-00 Lashing points (wind speeds up to 100 kts) 0.7 1.51 05-93008-B L8544-001-00 Lashing points (wind speeds up to 40 kts) 2.4 5.31 05-93011-A L8544-003-10 Lashing points (ship landing), fixed provisions 4.2 9.31 05-93011-A L8544-003-20 Lashing points (ship landing), detachable parts 0.6 1.31 05-95001-C L1321-001-00 Cover kit for helicopter GSE GSE1 05-97001-C L6201-001-30 Accelerometers for Track and Balance system 0.0 0.0

a.The protective capability is degraded with the simultaneous fitment of: radoar radome.b.Requires L6611-001-10 Main rotor blade folding: basic kit.


Weight[lb]


a.No simultaneous fitment with settling protectors and vice versa.

21.9 48.31 06-46001-B L3344-001-00 Strobe lights, white 1.4 3.11 06-61015-B L3215-001-10 Emergency floats, fixed provisions 7.8 17.21 06-61015-B L3215-001-21 Emergency floats, detachable parts 64.6 142.41 06-65002-C L2566-001-00 Emergency hammer 0.2 0.41 06-66008-C L3353-005-00 Emergency lightsb

b.Boarding step illumination is already part of this package and does not need to be selected separately.

2.9 6.41 06-66009-B L3322-001-00 Boarding step illumination 0.2 0.41 06-66010-B L3353-006-20 Illuminated signs "NO SMOKING/FASTEN SEAT BELT" 0.8 1.8


Weight[lb]

1 07-50026-B L5231-001-00 One-hand latching system for clam-shell doors 1.0 2.21 07-50034-B L5212-001-00 Jettisonable cockpit doors 1.2 2.6


Weight[lb]


7.3 16.1


20.5 45.2


0.5 1.1

1 08-15507-B L2315-092-00 IRIDIUM satellite phone AEROPHONE (Aerodata) incl. cockpit dial panel

4.7 10.4

1 08-15532-A L2341-195-40 VIP SATCOM – private modea 2.2 4.91 08-15532-A L2341-195-50 VIP SATCOM – wired handset, rear window niche RHa 0.6 1.31 08-16061-A L2341-006-63 Voice alert generation for DACS (NAT) 0.0 0.01 08-24015-C L3452-092-09 ADF control unit CDF-552 (Chelton/Wulfsberg) 1.2 2.61 08-24015-C L3452-092-17 ADF receiver DF-431B, (Chelton/Wulfsberg)b 9.6 21.2


Weight[lb]


Technical Data




1 08-31019-B L2571-001-00 Radar radome for RDR 2000 2.0 4.41 08-31019-B L3443-090-02 Color weather radar RDR 2000 (Honeywell)c 6.6 14.61 08-35007-B L3442-881-00 TAS 620 (Avidyne) interface with GNS430 0.2 0.41 08-35007-C L2327-001-01 Traffic Advisory System TAS 620 (Avidyne)d 9.5 20.91 08-46040-A L3168-092-07 Digital moving map EURONAV IV+ -RN6 (Euro Avionics),

(interfaced with FCDS)ef5.4 11.9



a.Requires L2315-092-00 IRIDIUM satellite phone AEROPHONE (Aerodata) incl. cockpit dial panel.b.Requires L3452-092-09 ADF control unit CDF-552 (Chelton/Wulfsberg) and vice versa.c.Requires L2571-001-00 Radar radome RDR2000.d.Requires L 3442-881-00 TAS 620 (Avidyne) interface with GNS430.e.Requires L3443-010-00 Video Radar Unit (VRU).f.Approval for VFR only, maps and special options not included.


Weight[lb]




0.8 1.8


0.3 0.7


Weight[lb]



Weight[lb]


0.3 0.7


Weight[lb]



Weight[lb]


Page 132 of 202 135.09.101.01

Technical Data

4.5.4 Material and color definitionThe default color line of the Executive configuration is defined as SAHARA. Detailed information con-cerning this color line is given in the listing below.

Further color line schemes are avaiable on request. Please refer to the technical data support docu-ment „EC135 Interior Catalog”.

Option Material Color

VIP Pilot seat




VIP Copilot seat




VIP Passenger seats (2 front)




VIP Passenger seats (2 rear)




VIP Cabinet front


LeatherLeatherMetal

Beige (CS 402)Almond (1015)Brushed

VIP Cabinet rear


LeatherLeatherMetal

Beige (CS 402)Almond (1015)Brushed

VIP PSU (air outlets and lights)

Surface Metal Brushed

VIP Covers for controls (collective and cyclic)


VIP Carpet for cockpit, cabin and cargo compartment

Carpet long pile and hand tuftedLinked carpet edges

WoolLeather

Light Beige (ME 402)Beige (CS 402)

Armrest in rear window niche LH / RH


Special painted interior

Paint Light Ivory (RAL 1015)


Technical Data


Maximum Range



Mission Parameters




Contingency 5%


Temperature: ISA



Crew (1) 85 187

Passengers (4+1)a

a.Each passenger 85 kg / 187 lb. 4 passengers in cabin and 1 on copilot side.

425 937

Reserve fuel 65 143


Trip fuel 423 933



Page 134 of 202 135.09.101.01

Technical Data


0 50 100 150 200 250 300 350

0

200

400

600

800

Pay

load

[kg]

Range [nm]

4+1 Passengers @ 85kg


Technical Data

Blank


Page 136 of 202 135.09.101.01

Technical Data

4.6 HERMÈS

The l'Hélicoptère par Hermès, also part of the EC135 family, has been ingeniously designed to providea sober, luxurious space for passengers. The cabin includes the latest design elements and introducesa new concept for stowing clothes and luggage. Everything about the cabin is so exquisitely Hermès:the headrest, the cabinets, the armrests… Hermès has changed the concept of flying.

This helicopter is a available in a range of exterior colors. The interior may combine a variety af mate-rials and colors as is the custom with all ranges of procucts offered by the House.

Figure 4.32: Typical Layout of an EC135 Hermès interior


Technical Data



Baseline Aircraft

Subtotal: 1,455.0 3,208.31,5% weight margin: 21.8 48.1

Subtotal (inclmargin): 1,476.8 3,256.4

General Equipment

Mission Equipment

Pilots 1 or 2

Pax 4


Weight[lb]

1 00-10002-A L0000-002-00 EC135 Standard Aircraft 135.08.100.01 E 1,455.0 3,208.31 L0000-003-01 2 Turbomeca ARRIUS 2B2 turbine engines1 L0000-003-02 2 Pratt & Whitney PW206B2 turbine engines


Weight[lb]

1 05-22008-C L2621-001-00 Engine fire extinguishing system 3.6 7.91 05-30003-A L2565-002-00 Flash light copilot side 0.2 0.41 05-32007-B L3042-001-00 Windshield wiper system 5.0 11.01 05-33001-B L3113-001-00 Slant panel 0.8 1.81 05-33002-B L3113-004-00 Center console 2.2 4.91 05-34002-B L2576-001-00 Avionics compartment 4.2 9.31 05-37016-C L6701-001-00 Copilot flight controls 6.2 13.71 05-38010-B L3111-001-04 7" copilot instrument panel with glare shield 2.7 6.01 05-39006-B L2514-003-01 Map case in copilot door 0.5 1.11 05-39008-B L3113-004-10 Illuminated chart holder for pilot side 1.0 2.21 05-61010-B L2433-006-00 Battery, type "Saft", ULM, 40 Ah, 24 V






Weight[lb]



Page 138 of 202 135.09.101.01

Technical Data

Interior Layout


Weight[lb]

1 07-50036-B L2514-012-00 Covers for sliding door fairing LH/RH 0.1 0.21 07-50039-B L5211-010-00 Door catch system for cockpit doors 0.1 0.21 07-50039-B L5211-011-00 Door catch system for sliding doors 0.2 0.41 07-80025-A L2521-005-00 Hermès Package: 256.5 565.61 Armrest in rear window niches Hermès1 Carpet for cockpit, cabin and cargo compartment Hermès1 Rear cabinet Hermès1 4 tie-down fitting in cargo compartment Hermès1 Package tray in cargo compartment Hermès1 Enhanced sound proofing kit Hermès1 Interior lining Hermès1 2nd portable fire extinguisher Hermès1 Map cases on instrument panel glare shield Hermès1 Landing gear Hermès (instead of standard landing gear)1 Passenger Service Unit (PSU) Hermès1 Tailboom LED light Hermès1 Cargo compartment lighting Hermès1 Emergency lights Hermès1 Door handles for cocpit doors Hermès1 Door handles for sliding doors Hermès1 Door handles for clam-shell doors Hermès1 Tinted windows for cockpit doors Hermès1 Tinted windows for passenger cabin Hermès1 Leather coating for control outlets Hermès1 Front cabinet Hermès1 Tinted front windshields1 High visibility paint for main rotor blades Hermès1 Exterior painting Hermès1 Air conditioning system Hermès1 Tinted sun shades for cockpit windshield roof section Hermès1 Separation wall for cabin / cargo compartment Hermès1 Bleed air heating system Hermès1 Separation wall for cockpit /cabin Hermès1 Special painted interior Hermès1 Height adjustable pilot seat Hermès

instead of standard pilot seat1 Height adjustable copilot seat Hermès

instead of standard pilot seat1 4 passenger seats Hermès1 First aid kit Hermèsa



Technical Data

Avionics



Total: 1,936.1 4,269.1


General Equipment

Mission Equipment


Weight[lb]






Dual (4xSMD45)1 AV Pack DP IFR GC G430, interconnection / wiring1 08-16063-A L2341-007-54 Fixed provisions for ANR 0.5 1.16 08-18060-A L2315-001-73 Headset AHX34-04 ANR LEMO 28 VDC (Bose), low impe-

dance1.8 4.0

2 08-18061-A L2341-007-67 Headset Adapter cable crew GLENAIR/LEMO ANR 0.2 0.44 08-18061-A L2341-007-68 Headset Adapter cable pax GLENAIR/LEMO ANR 0.4 0.91 08-21014-C L3441-090-04 Radar altimeter KRA 405 B (Honeywell) 3.5 7.71 08-53002-B L2212-400-00 MEGHAS Sensor Kit 17.0 37.51 08-54001-C L3411-001-00 Copilot pitot static system 1.5 3.31 08-72001-B L2212-001-00 Digital Automatic Flight Control System - DAFCS 27.0 59.5


Weight[lb]

1 05-22007-B L7924-001-00 Fuzz burners for engines 1.2 2.61 05-23006-B L7165-002-00 Engine compressor wash kit 2.5 5.51 05-25016-D L7161-001-10 Sand filter system, fixed provisions 11.3 24.91 05-25016-D L7161-001-20 Sand filter system, detachable parts 26.2 57.81 05-26012-B L1241-001-00 Anti-corrosion protection 5.2 11.51 05-34003-B L2576-002-00 Dampers for avionics compartment 1.8 4.01 05-39008-B L3113-004-20 Illuminated chart holder for copilot side 0.9 2.01 05-81033-B L2812-001-00 Self sealing fuel supply tanks 4.5 9.91 05-85008-C L2843-001-00 Fuel management system (Fuel flow meters) 1.2 2.61 05-95001-C L1321-001-00 Cover kit for helicopter GSE GSE1 05-97001-C L6201-001-30 Accelerometers for Track and Balance system 0.0 0.0


Weight[lb]

1 06-46001-B L3344-001-00 Strobe lights, white 1.4 3.1


Page 140 of 202 135.09.101.01

Technical Data

Interior Layout

Avionics


Maximum Range

The calculated maximum range for the mission below is 227.0 nm (421 km).


Weight[lb]

1 07-50027-B L5231-002-00 Extended opening fasteners for clam-shell doors 0.3 0.7


Weight[lb]


7.3 16.1


20.5 45.2


0.5 1.1

1 08-15507-B L2315-092-00 IRIDIUM satellite phone AEROPHONE (Aerodata) incl. cockpit dial panel

4.7 10.4




b.Requires L2571-001-00 Radar radome RDR2000.

6.6 14.61 08-35007-C L3442-881-00 TAS 620 (Avidyne) interface with GNS430 0.2 0.41 08-35007-C L2327-001-01 Traffic Advisory System TAS 620 (Avidyne)c


9.5 20.91 08-46040-A L3168-092-07 Digital moving Map EURONAV IV+ -RN6 (Euro Avionics),

interfaced with FCDSde

d.Requires L3443-010-00 Video Radar Unit (VRU).e.Approval for VFR only, maps and special options not included.

5.4 11.9



Mission Parameters




Contingency 5%


Temperature: ISA


Technical Data




Crew (2) 170 375

Passengers (4)a

a.Each passenger 85 kg / 187 lb.

340 750

Reserve fuel 66 146


Trip fuel 379 836



0 50 100 150 200 250 300 350

0

200

400

600

800

Pay

load

[kg]

Range [nm]

4 Passengers @ 85kg


Page 142 of 202 135.09.101.01

Technical Data

4.7 Utility

The EC135 offers numerous possibilities to utility operators. With the best ratio between maximumtakeoff weight and useful load in its class, the EC135 carries out all kinds of utility missions with a ma-ximum external cargo hook capacity of 1,300 kg. The Vehicle and Engine Multifunction Display(VEMD®) allows pilots to concentrate on the mission ahead: an acoustic warning informs them whenthe engine is reaching its first limitation, which in turn reduces pilot workload.

The EC135's design and large horizontal stabilizer provide stability for sling load operations. The Fe-nestron® tail rotor ensures safety for personnel on ground and helps pilots avoid obstacles when lan-ding or maneuvering. And last but not least, the EC135 has the lowest direct operating cost in its class,making it the cheapest twin engine helicopter to operate!

Some examples of utility missions that the EC135 can perform:• Sling load operations• Fire fighting• Hoisting• Cargo transportation• Power Line inspections• Wind turbine maintenance and inspections• News Gathering

Figure 4.34: EC135 used for maintenance of windmill parks


Technical Data

4.7.1 Mission ParameterFlight Rules: VFR (Night)Instrumentation: ConventionalCat-A: Yes

Cargo (Hook) Operation

Pax Transport


Baseline Aircraft



General Equipment

Pilots 1

Pilots 1

Pax 6


Weight[lb]



Weight[lb]

1 05-03007-C L2562-001-00 First aid kita 1.5 3.31 05-12001-B L5232-001-00 Multifunction handle on the main gear box cowling

(LH and RH)0.6 1.3

1 05-22007-B L7924-001-00 Fuzz burners for engines 1.2 2.61 05-22008-C L2621-001-00 Engine fire extinguishing system 3.6 7.91 05-22014-A L5371-001-00 Engine outlet heat protection 1.2 2.61 05-31026-C L2514-002-00 Tinted sun shades for cockpit windshield roof section 1.9 4.21 05-33001-B L3113-001-00 Slant panel 0.8 1.81 05-33002-B L3113-004-00 Center console 2.2 4.91 05-41004-C L2104-100-00 Bleed air heating system 6.6 14.6


Page 144 of 202 135.09.101.01

Technical Data

Mission Equipment

Interior Layout

Avionics

Subtotal: 165.1 364.03% Weight margin: 5.0 10.9


Total: 1,646.9 3,631.4

1 05-44002-B L2122-001-00 Ventilation extruder without copilot I-panel extension 0.3 0.71 05-61010-B L2433-003-00 Battery, type "Saft", ULM, 27 Ah, 24 V






Weight[lb]

1 06-45023-B L3343-003-00 Landing & search light, 450 W 3.1 6.81 06-65004-B L2625-003-00 2nd portable fire extinguisher 2.8 6.21 06-67044-B L2563-801-06 ELT C406-N HM (Artex) incl. NAV. opt. 3.3 7.3


Weight[lb]

1 07-27001-B L2522-001-00 3 forward passenger seats, facing backwards 37.4 82.51 07-27001-B L2522-002-00 2 rear passenger seats, facing forward 22.2 49.01 07-60015-B L2514-014-00 Variable tie-down net 3.3 7.3


Weight[lb]


pilot and copilot1 Transponder (Mode S) GTX 330 (Garmin)1 Avionics/Radio master switches (Special EUROCOPTER®)1 GPS/NAV/COM GNS 430 (Garmin), pilot,

incl. annunciator/switch MD 411 4'' Artificial horizon GH14-391, pilot (Honeywell)1 Gyro Magnetic Heading System KCS 55 A (Honeywell)

incl. KG-102A, KMT-112, KA-21B with HSI KI-525A, pilot1 AV Pack SP VFR, interconnection / wiring1 08-21014-C L3441-090-04 Radar altimeter KRA 405 B (Honeywell) 3.5 7.71 08-21014-C L3441-092-03 Radar altimeter indicator KNI 416 (Honeywell) 1.2 2.61 08-51013-B L3425-806-51 2” stand-by horizon AI 804 DC (Goodrich),


1 08-71002-C L2217-001-10 VFR SAS (VFR pitch/roll Stability Augmentation System) 5.6 12.3


Weight[lb]


Technical Data


General Equipment


Weight[lb]

1 05-02016-C L1111-002-00 Two-color exterior painting instead of single color painting 1.5 3.31 05-12002-B L2551-003-00 Additional 4 tie-down fittings for airline attachment rails 0.6 1.31 05-21015-B L8541-001-10 Wire strike protection system, fixed provisions 3.3 7.31 05-21015-B L8541-001-20 Wire strike protection system, detachable partsa

a.The protective capability is degraded with the simultaneous fitment of: cargo hook mirror.

8.2 18.11 05-22014-A L5611-002-00 Tinted front windshields 1.2 2.61 05-23006-B L7165-002-00 Engine compressor wash kit 3.2 7.11 05-25016-D L7161-001-10 Sand filter system, fixed provisions 11.3 24.91 05-25016-D L7161-001-20 Sand filter system, detachable parts 26.2 57.81 05-26012-B L1241-001-00 Anti-corrosion protection 5.5 12.11 05-31025-B L5211-002-00 Sliding windows in sliding doors 1.9 4.21 05-31026-C L5621-001-00 Tinted window for cockpit doors 0.0 0.01 05-31027-B L5633-001-10 Window in clam-shell door, LH 0.8 1.81 05-31027-B L5633-001-20 Window in clam-shell door, RH 0.8 1.81 05-31045-A L5211-001-11 Lockable sliding window in copilots' door 0.1 0.21 05-31045-A L5211-001-12 Lockable sliding window in pilots' door 0.1 0.21 05-31086-A L5211-002-01 Ram air deflectors sliding doorsb


0.4 0.91 05-31098-A L5211-001-01 Ram air deflectors cockpit doors 0.6 1.31 05-32007-B L3042-001-00 Windshield wiper system 5.0 11.01 05-34002-B L2576-001-00 Avionics compartment 4.2 9.31 05-39006-B L2514-003-01 Map case in copilot door 0.5 1.11 05-39007-B L3111-001-10 Map cases on instrument panel glare shield 0.6 1.31 05-39008-B L3113-004-10 Illuminated chart holder for pilot side 1.0 2.21 05-42041-A L2105-005-00 Air conditioning system 55.0 121.31 05-71001-C L6351-002-00 Rotor brake system 5.3 11.71 05-81032-C L2818-100-10 Internal long range fuel tank system, fixed provisions 2.6 5.71 05-81032-C L2818-100-20 Internal long range fuel tank system, detachable partsc

c.No simultaneous fitment with a stretcher.

36.1 79.61 05-85008-C L2843-001-00 Fuel management system (Fuel flow meters) 1.2 2.61 05-92009-B L6611-001-10 Main rotor blade folding: basic kit 1.3 2.91 05-92009-B L6611-001-20 Main rotor blade folding: fixed provisions for ground

handling kitd

d.Requires L6611-001-10 Main rotor blade folding: basic kit

0.8 1.8



Page 146 of 202 135.09.101.01

Technical Data

Mission Equipment

Interior Layout


Weight[lb]



21.9 48.31 06-21017-C L8512-001-10 External hoist LH, fixed provisions 8.6 19.01 06-21017-C L8512-001-12 External hoist RH, fixed provisions 8.6 19.01 06-21017-C L8512-001-20 External hoist 50m, detachable parts



62.7 138.3

1 06-26011-C L8511-002-10 Cargo hook mirrors RH, fixed provisions 0.8 1.81 06-26011-C L8511-002-20 Cargo hook mirrors RH, detachable parts 3.9 8.61 06-27019-D L8511-001-10 Cargo hook system, fixed provisions 3.7 8.21 06-27019-D L8511-001-30 Cargo hook system, detachable parts 16.5 36.41 06-27027-A L8511-003-10 Cargo hook weighing system, fixed provisionsb

b.Requires L8511-001-10 Cargo hook system, fixed provisions.

0.2 0.41 06-27027-A L8511-003-20 Cargo hook weighing system, detachable parts 1.5 3.31 06-46001-B L3344-001-00 Strobe lights, white 1.4 3.11 06-61015-B L3215-001-10 Emergency floats, fixed provisions 7.8 17.21 06-61015-B L3215-001-21 Emergency floats, detachable parts 64.6 142.41 06-65002-B L2566-001-00 Emergency hammer 0.2 0.41 06-66008-C L3353-005-00 Emergency lightsc

c.Boarding step illumination is already part of this package and does not need to be selected separately.

2.9 6.41 06-66009-B L3322-001-00 Boarding step illumination 0.2 0.41 06-66010-B L3353-006-20 Illuminated signs "NO SMOKING/FASTEN SEAT BELT" 0.8 1.81 06-81009-B L8503-001-10 Fire extinguishing bucket attachment (Bambi Bucket),

fixed provisionsb0.8 1.8


Weight[lb]

1 07-15016-B L2512-003-10 Height adjustable pilot seat instead of standard pilot seat 1.8 4.01 07-15016-B L2512-003-20 Height adjustable copilot seat instead of standard

copilot seat1.8 4.0

1 07-30012-B L2581-001-00 Enhanced sound proofing kit 4.8 10.61 07-30013-B L2524-002-00 Separation curtain for cockpit / cabin 2.1 4.61 07-30015-B L2524-001-00 Separation wall for cabin / cargo compartmenta 4.4 9.71 07-30018-A L5213-003-00 Curtains for cabin windows (grey) 1.6 3.51 07-40005-B L2513-220-00 Washable floor covering for cockpit, cabin and

cargo compartment11.5 25.4

1 07-40017-A L8552-001-00 Sealed cabin floor 0.3 0.71 07-50026-B L5231-001-00 One-hand latching system for clam-shell doors 1.0 2.21 07-50027-B L5231-002-00 Extended opening fasteners for clam-shell doors 0.3 0.71 07-50028-A L5213-001-11 Sliding door fastener, intermediate and max. position, LH 1.0 2.21 07-50028-A L5213-001-12 Sliding door fastener, max. position, LH 0.4 0.91 07-50028-A L5213-001-21 Sliding door fastener, intermediate and max. position, RH 1.0 2.21 07-50028-A L5213-001-22 Sliding door fastener max. position, RH 0.4 0.91 07-50030-B L8512-003-00 Abrasion protection at sliding door 0.2 0.41 07-50034-B L5212-001-00 Jettisonable cockpit doors 1.2 2.61 07-50035-B L8504-813-00 Spoiler position for cockpit doors 1.1 2.41 07-50036-B L2514-012-00 Covers for sliding door fairing LH/RH 0.1 0.2


Technical Data

Avionics


1 07-50039-B L5211-010-00 Door catch system for cockpit doors 0.1 0.21 07-50039-B L5211-011-00 Door catch system for sliding doors 0.2 0.41 07-60014-B L2514-013-00 Map case in sliding doors LH/RH 1.4 3.11 07-74043-A BUL-30120-006-2 Stretcher "Ferno" foldable, LH/RH - BUL 17.0 37.51 07-74045-A AAT-30120-006-2 Stretcher "Rescue" foldable for Helicopter Floor, LH/RH - AAT 18.7 41.21 07-74057-A AEL-30120-013-1 Stretcher "Cirrus 1000" foldable, LH/RH, fix provisions - AEL 1.0 2.21 07-74057-A AEL-30120-013-2 Stretcher "Cirrus 1000" foldable, LH/RH,

detachable parts - AEL14.5 32.0

a.Requries L2576-001-00 Avionics compartment.


Weight[lb]

08-10021-A L2314-090-15 HF communication system HF9000 (Rockwell Collins), fixed provisions

7.3 16.1

08-10021-A L2314-090-25 HF communication system HF9000 (Rockwell Collins), detachable parts

20.5 45.2

08-12036-B L4322-090-04 Fixed provisions for tactical radio (antenna, power supply, ICS interface)

2.2 4.9

08-15028-B L2319-002-41 Fixed provisions for GSM phone (antenna, 28V DC, interface to ICS)

0.5 1.1

08-15523-A L2315-092-02 IRIDIUM satellite communication and tracking system Flightdeck (SkyConnect)

7.7 17.0

08-16061-A L2341-193-40 Digital Audio Control System ACP53 (NAT), PAX 3.6 7.908-25014-A L3169-092-02 Distance Measuring Equipment DME indicator KDI 572

(Honeywell)0.8 1.8

08-25014-A L3455-092-03 Distance Measuring Equipment DME KN 63 (Honeywell) 2.0 4.408-26010-B L3431-092-02 Marker beacon receiver/lights KR 21 (Honeywell) 0.9 2.008-35007-C L3442-881-00 TAS 620 (Avidyne) interface with GNS430 0.2 0.408-35007-C L2327-001-01 Traffic Advisory System TAS 620 (Avidyne) 9.5 20.9


Weight[lb]




0.8 1.8


0.3 0.7


Weight[lb]


Page 148 of 202 135.09.101.01

Technical Data




4.7.4.1 Maximum Range

The calculated maximum range for the mission below is 304.5 nm (564 km).



Weight[lb]



Weight[lb]


0.3 0.7


Weight[lb]


Mission Parameters




Temperature: ISA



a. Increased to 1647 kg / 3632 lb for passenger transport (pax seats installed).

1574 3471

Crew (1) 85 187

Payloadb

b. Decreased to 618 kg / 1363 lb for passenger transport (pax seats installed).

691 1524

Reserve fuel 65 143

Trip fuel 495 1092



Technical Data


0 50 100 150 200 250 300 350

0

200

400

600

800

1000

1200

Pay

load

[kg]

Range [nm]

Weight of seats (73kg)


Page 150 of 202 135.09.101.01

Technical Data

4.8 Offshore - Oil and Gas

For offshore operations, the EC135's panoramic visibility, exceptional maneuverability, range, twin-en-gine performance, safety, and large cabin make the helicopter perfectly suited for this sector's deman-ding operations. The powerful and reliable engines provide outstanding performance and vital powerreserves even in one-engine inoperative (OEI) scenarios. The EC135 features other safety aspects,such as energy-absorbing fuselage and seats and crash-resistant fuel cells. Its state-of-the-art avio-nics considerably reduce pilot workload, allowing them to focus on the mission ahead. The simple de-sign of the EC135 allows for fast and easy maintenance, thereby ensuring optimal dispatch availability.Finally, the EC135's proven technology enables pilots to perform safe and efficient flights, even in thepoorest weather conditions.

Safety and Comfort in MindThe EC135's spacious cabin offers outstanding visibility to both the pilot and its passengers. The latterwill appreciate the ample legroom and low in-flight vibration levels. In the standard configuration, theEC135 can accommodate 5 or 6 passengers plus 1 or 2 pilots. The desing of the EC135 is fully adaptedfor hoist operations with its flat cabin floor, specific landing gear and most of all, excellent OEI hoverperformance, which ensures optimal safety in case of an engine failure during operations.

Figure 4.36: EC135 in a typical offshore layout


Technical Data

4.8.1 Mission ParameterFlight Rules: IFR (Night)Instrumentation: Glass Cockpit (MEGHAS)Cat-A: Yes


Baseline Aircraft



General Equipment

Pilots 1 or 2

Pax 5


Weight[lb]



Weight[lb]

1 05-02016-C L1111-002-00 Two-color exterior painting instead of single color painting 1.5 3.31 05-03007-C L2562-001-00 First aid kita 1.5 3.31 05-12001-B L5232-001-00 Multifunction handle on the main gear box cowling

(LH and RH)0.6 1.3

1 05-22007-B L7924-001-00 Fuzz burners for engines 1.2 2.61 05-22008-C L2621-001-00 Engine fire extinguishing system 3.6 7.92 05-22014-A L5371-001-00 Engine outlet heat protection 2.4 5.31 05-23006-B L7165-002-00 Engine compressor wash kit 3.2 7.11 05-26012-B L1241-001-00 Anti-corrosion protection 5.2 11.51 05-30003-A L2565-002-00 Flash light copilot side 0.2 0.41 05-31026-C L2514-002-00 Tinted sun shades for cockpit windshield roof section 1.9 4.21 05-33001-B L3113-001-00 Slant panel 0.8 1.81 05-33002-B L3113-004-00 Center console 2.2 4.91 05-34002-B L2576-001-00 Avionics compartment 4.2 9.31 05-37016-C L6701-001-00 Copilot flight controls 6.0 13.21 05-38010-B L3111-001-04 7" copilot instrument panel with glare shield 2.7 6.01 05-39006-B L2514-003-01 Map case in copilot door 0.5 1.11 05-39007-B L3111-001-10 Map cases on instrument panel glare shield 0.6 1.31 05-39008-B L3113-004-10 Illuminated chart holder for pilot side 1.0 2.21 05-41004-C L2104-100-00 Bleed air heating system 6.6 14.61 05-61010-B L2433-006-00 Battery, type "Saft", ULM, 40 Ah, 24 V


1 05-62010-C L2420-005-00 AC system (50 VA) 1.9 4.2


Page 152 of 202 135.09.101.01

Technical Data

Mission Equipment

Interior Layout


3.6 7.9




Weight[lb]

1 06-12008-C L3217-001-00 Reinforced rear landing gear cross tube 1.0 2.21 06-45023-B L3343-003-00 Landing & search light, 450 W 3.1 6.81 06-61015-B L3215-001-10 Emergency floats, fixed provisions 7.8 17.21 06-61015-B L3215-001-21 Emergency floats, detachable parts 64.6 142.41 06-66008-C L3353-005-00 Emergency lights 2.9 6.41 06-66017-B L3353-010-00 HEEL System (Helicopter Emergency Egress Lighting) 5.4 11.91 06-67044-B L2563-801-06 ELT C406-N HM (Artex) incl. NAV. opt. 3.3 7.3


Weight[lb]

1 07-27001-B L2522-001-00 3 forward passenger seats, facing backwards 37.4 82.51 07-27001-B L2522-002-00 2 rear passenger seats, facing forward 22.2 49.01 07-40005-B L2513-220-00 Washable floor covering for cockpit, cabin and

cargo compartment11.5 25.4

1 07-40017-A L8552-001-00 Sealed cabin floor 0.3 0.71 07-50034-B L5212-001-00 Jettisonable cockpit doors 1.2 2.61 07-60015-B L2514-014-00 Variable tie-down net 3.3 7.3


Weight[lb]


Technical Data

Avionics



Total: 1,881.6 4,149.0


Weight[lb]






Dual (4xSMD45)1 AV Pack DP IFR GC G430, interconnection / wiring1 08-16061-A L2341-006-63 Voice alert generation for DACS (NAT) 0.0 0.01 08-21014-C L3441-090-04 Radar altimeter KRA 405 B (Honeywell) 3.5 7.71 08-31019-B L2571-001-00 Radar radome for RDR 2000 2.0 4.41 08-31019-B L3443-090-02 Color weather radar RDR 2000 (Honeywell) 6.6 14.61 08-53002-B L2212-400-00 MEGHAS Sensor Kit 17.0 37.51 08-53004-B L3424-000-00 AHRS Free Steering Mode 0.5 1.11 08-54001-C L3411-001-00 Copilot pitot static system 1.5 3.31 08-65004-B L3443-010-00 Video Radar Unit (VRU) 5.0 11.01 08-72001-B L2212-001-00 Digital Automatic Flight Control System - DAFCS 27.0 59.51 08-83007-C L2321-009-00 M'ARMS Cockpit Voice and Flight Data Recorder (CVFDR)

and M'ARMS Usage Monitoring System (UMS), ground station not included

16.9 37.3


Page 154 of 202 135.09.101.01

Technical Data


General Equipment

Mission Equipment


Weight[lb]



8.2 18.11 05-22014-A L5611-002-00 Tinted front windshields 1.2 2.61 05-25016-D L7161-001-10 Sand filter system, fixed provisions 11.3 24.91 05-25016-D L7161-001-20 Sand filter system, detachable parts 26.2 57.81 05-31025-B L5211-002-00 Sliding windows in sliding doors 1.9 4.21 05-31026-C L5621-001-00 Tinted window for cockpit doors 0.0 0.01 05-31027-B L5633-001-10 Window in clam-shell door, LH 0.8 1.81 05-31027-B L5633-001-20 Window in clam-shell door, RH 0.8 1.81 05-31028-C L2524-030-10 IFR - training screen, fixed provisions 0.1 0.21 05-31028-C L2524-030-20 IFR - training screen, detachable parts 1.6 3.51 05-31045-A L5211-001-11 Lockable sliding window in copilots' door 0.1 0.21 05-31045-A L5211-001-12 Lockable sliding window in pilots' door 0.1 0.21 05-31086-A L5211-002-01 Ram air deflectors sliding doorsb


0.4 0.91 05-31098-A L5211-001-01 Ram air deflectors cockpit doors 0.6 1.31 05-32007-B L3042-001-00 Windshield wiper system 5.0 11.01 05-34003-B L2576-002-00 Dampers for avionics compartment 1.8 4.01 05-37017-B L6721-001-00 Covers for copilot flight controls -2.5 -5.51 05-39008-B L3113-004-20 Illuminated chart holder for copilot side 0.9 2.01 05-42041-A L2105-005-00 Air conditioning system 55.0 121.31 05-81032-C L2818-100-10 Internal long range fuel tank system, fixed provisions 2.6 5.71 05-81032-C L2818-100-20 Internal long range fuel tank system, detachable partsc

c.No simultaneous fitment with a stretcher.

36.1 79.61 05-85008-C L2843-001-00 Fuel management system (Fuel flow meters) 1.2 2.61 05-92009-B L6611-001-10 Main rotor blade folding: basic kit 1.3 2.91 05-92009-B L6611-001-20 Main rotor blade folding: fixed provisions for ground

handling kitd


0.8 1.8



Weight[lb]

1 06-11021-B L3274-001-10 Settling protectors, fixed provisions 1.9 4.21 06-11021-B L3274-001-20 Settling protectors, detachable parts 7.9 17.41 06-11022-C L3272-001-10 Snow skids, fixed provisions 0.9 2.01 06-11022-C L3272-001-20 Snow skids, detachable partsa 21.9 48.31 06-21017-C L8512-001-10 External hoist LH, fixed provisions 8.6 19.01 06-21017-C L8512-001-12 External hoist RH, fixed provisions 8.6 19.0


Technical Data

Interior Layout

Avionics


59.2 130.5


62.7 138.3

1 06-26011-C L8511-002-10 Cargo hook mirrors RH, fixed provisions 0.8 1.81 06-26011-C L8511-002-20 Cargo hook mirrors RH, detachable parts 3.9 8.61 06-27019-D L8511-001-10 Cargo hook system, fixed provisions 3.7 8.21 06-27019-D L8511-001-30 Cargo hook system, detachable parts 16.5 36.41 06-27027-A L8511-003-10 Cargo hook weighing system, fixed provisionsb 0.2 0.41 06-27027-A L8511-003-20 Cargo hook weighing system, detachable parts 1.5 3.31 06-31012-B L8531-001-00 External loudspeaker system with siren 11.5 25.41 06-46001-B L3344-001-00 Strobe lights, white 1.4 3.11 06-65002-C L2566-001-00 Emergency hammer 0.2 0.41 06-65004-B L2625-003-00 2nd portable fire extinguisher 2.8 6.21 06-66010-B L3353-006-20 Illuminated signs "NO SMOKING/FASTEN SEAT BELT" 0.8 1.8

a.No simultaneous fitment with settling protectors.b.Requires L8511-001-10 Cargo hook system, fixed provisions.


Weight[lb]

1 07-15016-B L2512-003-10 Height adjustable pilot seat instead of standard pilot seat 1.8 4.01 07-15016-B L2512-003-20 Height adjustable copilot seat instead of standard copilot seat 1.8 4.01 07-30012-B L2581-001-00 Enhanced sound proofing kit 4.8 10.61 07-30013-B L2524-002-00 Separation curtain for cockpit / cabin 2.1 4.61 07-30015-B L2524-001-00 Separation wall for cabin / cargo compartment 4.4 9.71 07-30018-A L5213-003-00 Curtains for cabin windows (grey) 1.6 3.51 07-50025-C L5211-004-00 Securing device for complete opening of cockpit doors 0.8 1.81 07-50026-B L5231-001-00 One-hand latching system for clam-shell doors 1.0 2.21 07-50027-B L5231-002-00 Extended opening fasteners for clam-shell doors 0.3 0.71 07-50028-A L5213-001-12 Sliding door fastener, max. position, LH 0.4 0.91 07-50028-A L5213-001-22 Sliding door fastener max. position, RH 0.4 0.91 07-50030-B L8512-003-00 Abrasion protection at sliding door 0.2 0.41 07-50036-B L2514-012-00 Covers for sliding door fairing LH/RH 0.1 0.21 07-50039-B L5211-010-00 Door catch system for cockpit doors 0.1 0.21 07-50039-B L5211-011-00 Door catch system for sliding doors 0.2 0.41 07-74043-A BUL-30120-006-2 Stretcher "Ferno" foldable, LH/RH - BUL 17.0 37.51 07-74045-A AAT-30120-006-2 Stretcher "Rescue" foldable for Helicopter Floor, LH/RH - AAT 18.7 41.21 07-74057-A AEL-30120-013-1 Stretcher "Cirrus 1000" foldable, LH/RH, fix provisions - AEL 1.0 2.21 07-74057-A AEL-30120-013-2 Stretcher "Cirrus 1000" foldable, LH/RH,

detachable parts - AEL14.5 32.0


Weight[lb]


7.3 16.1


20.5 45.2

1 08-12036-B L4322-090-04 Fixed provisions for tactical radio (antenna, power supply, ICS interface)

2.2 4.9


0.5 1.1


Weight[lb]


Page 156 of 202 135.09.101.01

Technical Data


Required adapter cables for the above listed Headsets (L2315-001-10 -L2315-001-72)



7.7 17.0

1 08-16061-A L2341-193-40 Digital Audio Control System ACP53 (NAT), PAX 3.6 7.91 08-17032-A L2331-003-00 Cabin loudspeaker 1.7 3.71 08-24015-C L3452-092-09 ADF control unit CDF-552 (Chelton/Wulfsberg) 1.2 2.61 08-24015-C L3452-092-17 ADF receiver DF-431B, (Chelton/Wulfsberg)a 9.6 21.21 08-35007-B L3442-881-00 TAS 620 (Avidyne) interface with GNS430 0.2 0.41 08-35007-C L2327-001-01 Traffic Advisory System TAS 620 (Avidyne)b 9.5 20.91 08-46040-A L3168-092-07 Digital moving map EURONAV IV+ -RN6 (Euro Avionics),

interfaced with FCDSc5.4 11.9

a.Requires L3452-092-09 ADF control unit CDF-552 (Chelton/Wulfsberg).b.Requires L3442-881-00 TAS 620 (Avidyne) interface with GNS430c.Approval for VFR only, maps and special options not included.


Weight[lb]




0.8 1.8


0.3 0.7


Weight[lb]



Weight[lb]


0.3 0.7


Weight[lb]



Weight[lb]


Technical Data


4.8.4.1 Radius of Action


Mission profile• Take-off in SL (max 2910 kg)• Climb flight AEO-MCP from SL to 3000ft with VY (65 KIAS)• Level flight in 3000ft with VBR• Descent from 3000ft to SL with R/D of -1000 fpm (80 KIAS)• Landing and takeoff (with same number of PAX) in SL• Climb flight AEO-MCP from SL to 3000ft with VY (65KIAS)• Level flight in 3000ft with VBR• Descent from 3000ft to SL with R/D of -1000 fpm (80 KIAS)• Landing in SL

Mission Parameters

Drag relevant equipment installed: Emergency Floats


Contigency fuel: 10%


Temperature: ISA



Crew (1) 85 187

Passengers (4) 380 838

Reserve fuel 70 154


Trip fuel 445 981



Page 158 of 202 135.09.101.01

Technical Data


0 20 40 60 80 100 120 140

0

200

400

600

800

Pay

load

[kg]


4 Passengers @ 95kg


Technical Data

Blank


Page 160 of 202 135.09.101.01

Technical Data

5 Further Product Information

In addition to the presented configurations / equipment in chapter 4 there is a wide range of further op-tions and mission equipment which is available on request. This chapter provides an insight of specialmission equipment, choices of avionics systems, etc.

5.1 News, highlights and main improvements

New basic ventilating systemApproximately in the 4th quarter of 2009 a new and improved basic ventilating system will be available.The main improvements are:• Brushless blower• Pilots‘ air outlets in the instrument panel will be independent from simultaneous display cooling ca-

pability.

New air conditioning systemApproximately in the 4th quarter of 2009 a new air conditioning system will be available. The new fea-tures and improvements are:• Mechanically driven compressor• Dual evaporator / dual zone system• Sufficient cooling capacity for extreme climates• Increased airflow• Up-to-date effective and lightweight automotive components

Figure 5.38: New outlets of airconditioning system


Technical Data

Inlet Barrier Filter systemFrom 2010 on an Inlet Barrier Filter system (IBF1) will be available for the EC135.

Medium height landing gearA new designed medium height landing gear is available on request. This new option now completesthe range of available landing gears for the EC135.

1.The IBF system is protected by a registered patent of EUROCOPTER.

Standard landing geara

a.Part of baseline aircraft.

Medium landing gear High landing gear

Height: 0.4 m / 1.3 ftWidth: 2.0 m / 6.6 ft

Height: 0.5 m / 1.7 ftWidth: 2.1 m / 6.9 ftΔ Weight: 4.6 kg / 10.1 lbs

Height: 0.7 m / 2.3 ftWidth: 2.3 m / 7.6 ftΔ Weight: 26.0 kg / 57.3 lbs

Figure 5.39: Landing gear options


Page 162 of 202 135.09.101.01

Technical Data

5.2 Avionics

EUROCOPTER® offers a wide range of modular avionics solutions. Starting from VFR to IFR, conven-tional to Glass Cockpit (MEGHAS), single to dual pilot solutions. For special mission equipment likedigital moving map, EOS cameras, etc. a large single SMD for copilot instrument panel is available. Inaddition NVG friendly solutions can be offered on request.

The following avionics layouts give a short overview about the avionics variety of the EC135.

5.2.1 VFR Solutions

Single Pilot Dual Pilot / Single Dual Pilot

Figure 5.40: Conventional Instrumentation with Garmin GNS430

VLOCGPS

AUTOOBS

WPTCDI OBS

INTG TERM APR MSG

G

Honeywell

44

2 2

NR

HIGH

CAUTION

MASTER

HI NR

ON

FRESH AIR

N

S

EW

3

612

1521

2430

33

HDGCOURSE

NAV HDG

KING

GS GS

XMSNOIL P

EMEROFF

SW 1

ACTIVECARGO

TEMP SMOKE

LOWFUEL 2

BAT

LOWFUEL 1 OFF

EMER

SW 2

ACTIVEA.TRIMAP

RPM

BAT

ROTOR

DISCH

FRESH AIR

AIR-SPEED

20

40

60

80

100120

140

160

1800

KNOTS

CALL SIGN555

50

45

40

35

30

25

20

15

101234

5678910

11 12ENG

ROTOR

N2

% RPM50

607080

0

90

100

110120

R

OFF1

SCROLL

OFF2

RESET

SELECT

+

-

ENTER

-

+BRT

OAT -888.8 X >8888 XX NE 888 XXX

HOOK 8888 X

XMSN OILENG1 OIL ENG2 OIL

-888.8 GEM XX -888.8

88.8 888 88 999 88.8 888

LANE 4 FAILED -> PRESS OFF2 LEFT

-10

-8

-6

-4

-20

2

4

ENG1 ENG2

TRQ101%

TRQ 65%

N1 83%

T4570°C

N1 90%

T4650°C

TOP4nm30s

MM LMT

ON

XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX

XXXXXXXXXXXXXXXXXXXXXXXXXXXXXX

XXXXXXXXXXXXXXXXXXXX

OFF

SCROLL

DT

RESET

100

END 8h 88min FUEL XX AUX

48 480 45FF1888XXX

FF2888XXX

20VE

FLIGHT

IDLE

FLIGHT

IDLE

NORM

OFF

OFF

NORMON

OFF

TRAINSELENG I ENG II

OFF

ON

FADEC

FADEC

ARM

OFF

OFFOFF OFF

RESET

GEN IIRESET

GEN IRESET

MSTRBAT

+

+

+100 FEET

970

ALTI TUDE

DOWN

UP

VERTICAL SPEED

FIT/MINX1000

ISO

VHF1

CALL

ICS

TXNORM

EMER

BK-UP

VOX

ISOCALL

TX

VHF2 TAC1 TAC2 FM UHF

ADFMKRDME2DME1NAV2NAV1

SAT PA

ISO

VHF1

CALL

ICS

TXNORM

EMER

BK-UP

VOX

ISOCALL

TX



SAT PA

IDPUSHVOL

PWR VOL

PUSH

SQ

VLOC

COM

C

VV

C

PUSHC/V

GARMIN GNS 430

GPSDEFAULTNAV

PUSHCRSR

PROCFPLMSGOBSCDI

ENTCLR

MENUD

RNG

PUNC

CLR

CRSR

STARTSTOP

IDENT ON

STBY OFF

GARMIN

VFR

0 1 2 3 4 5 6 7 8 9

ALT

ALT FLIGHT TIME01:23:201200

GTX 330

ICS

RX ICS

PTTPRESET

MIN

ICS

RX ICS

PTTPRESET

MIN

- +

CCW CW

SLAVE FREE

VLOCGPS

AUTOOBS

WPTCDI OBS

INTG TERM APR MSG

G

Honeywell

44

2 2

G

Honeywell

44

2 2

NR

HIGH

CAUTION

MASTER

HI NR

ON

CALL SIGN

N

S

EW

3

612

1521

2430

33

HDGCOURSE

NAV HDG

KING

GS GS333

3024

21 15

126

TO

FR

GS

NAV

NS

E

W

3

612

1521

24 30

33

KING

ADF

XMSNOIL P

EMEROFF

SW 1

ACTIVECARGO

TEMP SMOKE

LOWFUEL 2

BAT

LOWFUEL 1 OFF

EMER

SW 2

ACTIVEA.TRIMAP

RPM

BAT

ROTOR

DISCH

FRESH AIR

FRESH AIR

AIR-SPEED

20

40

60

80

100120

140

160

1800

KNOTS

CALL SIGN

+

+

+100 FEET

970

ALTI TUDE

DOWN

UP

VERTICAL SPEED

FIT/MINX1000

+

+

+100 FEET

970

ALTI TUDE

DOWN

UP

VERTICAL SPEED

FIT/MINX1000

555

50

45

40

35

30

25

20

15

101234

5678910

11 12ENG

ROTOR

N2

% RPM50

607080

0

90

100

110120

R

OFF1

SCROLL

OFF2

RESET

SELECT

+

-

ENTER

-

+BRT

OAT -888.8 X >8888 XX NE 888 XXX

HOOK 8888 X


-888.8 GEM XX -888.8

88.8 888 88 999 88.8 888


-10

-8

-6

-4

-20

2

4

ENG1 ENG2

TRQ101%

TRQ 65%

N1 83%

T4570°C

N1 90%

T4650°C

TOP4nm30s

MM LMT

ON




OFF

SCROLL

DT

RESET

100


48 480 45FF1888XXX

FF2888XXX

20VE

FLIGHT

IDLE

FLIGHT

IDLE

NORM

OFF

OFF

NORMON

OFF


OFF

ON

FADEC

FADEC

ARM

OFF

OFFOFF OFF

RESET

GEN IIRESET

GEN IRESET

MSTRBAT

80

60

100

20

40

AIR-SPEED

120

140

160

180

KNOTS

0

ISO

VHF1

CALL

ICS

TXNORM

EMER

BK-UP

VOX

ISOCALL

TX



SAT PA

ISO

VHF1

CALL

ICS

TXNORM

EMER

BK-UP

VOX

ISOCALL

TX



SAT PA

IDPUSHVOL

PWR VOL

PUSH

SQ

VLOC

COM

C

VV

C

PUSHC/V

GARMIN GNS 430

GPSDEFAULTNAV

PUSHCRSR

PROCFPLMSGOBSCDI

ENTCLR

MENUD

RNG

PUNC

CLR

CRSR

STARTSTOP

IDENT ON

STBY

OFF

GARMIN

VFR

0 1 2 3 4 5 6 7 8 9

ALT


GTX 330

ICS

RX ICS

PTTPRESET

MIN

ICS

RX ICS

PTTPRESET

MIN

- +

CCW CW

SLAVE FREE


Technical Data

5.2.2 IFR with Conventional Instrumentation

5.2.3 IFR Solutions with Glass Cockpit (MEGHAS)

Figure 5.41: FR solution with Conventional Instrumentation and dual Garmin GNS430

VLOCGPS

AUTOOBS

WPTCDI OBS

INTG TERM APR MSG

VLOCGPS

AUTOOBS

WPTCDI OBS

INTG TERM APR MSG

G

Honeywell

44

2 2

G

Honeywell

44

2 2

NR

HIGH

CAUTION

MASTER

HI NR

ON

NMH2

KT

RNV

MIN

OFF

N1HLD

N2

KING

LHMOA T S

SEN

CALL SIGN

XMSNOIL P

EMEROFF

SW 1

ACTIVECARGO

TEMP SMOKE

LOWFUEL 2

BAT

LOWFUEL 1 OFF

EMER

SW 2

ACTIVEA.TRIMAP

RPM

BAT

ROTOR

DISCH

FRESH AIR

FRESH AIR

AIR-SPEED

20

40

60

80

100120

140

160

1800

KNOTS

CALL SIGN

+

+

+100 FEET

970

ALTI TUDE

DOWN

UP

VERTICAL SPEED

FIT/MINX1000

+

+

+100 FEET

970

ALTI TUDE

DOWN

UP

VERTICAL SPEED

FIT/MINX1000

555

50

45

40

35

30

25

20

15

10

1234

5678910

11 12ENG

ROTOR

N2

% RPM50

607080

0

90

100

110120

R

OFF1

SCROLL

OFF2

RESET

SELECT

+

-

ENTER

-

+BRT

OAT -888.8 X >8888 XX NE 888 XXX

HOOK 8888 X


-888.8 GEM XX -888.8

88.8 888 88 999 88.8 888


-10

-8

-6

-4

-20

2

4

ENG1 ENG2

TRQ101%

TRQ 65%

N1 83%

T4570°C

N1 90%

T4650°C

TOP4nm30s

MM LMT

ON




OFF

SCROLL

DT

RESET

100


48 480 45FF1888XXX

FF2888XXX

10

10

20

20

OFF

P U L L

C A GE

RO

20VE

FLIGHT

IDLE

FLIGHT

IDLE

NORM

OFF

OFF

NORMON

OFF


OFF

ON

FADEC

FADEC

ARM

OFF

OFFOFF OFF

RESET

GEN IIRESET

GEN IRESET

MSTRBAT

80

60

100

20

40

AIR-SPEED

120

140

160

180

KNOTS

0

N

S

EW

3

612

1521

2430

33

HDG

ADF

GS OFF

COURSE

COMPA

SS

NAV

NAV

COMPA

SS

COURSE

GS OFF

ADF

HDG

33

3024

21 15

126

3

W E

S

N

ISO

VHF1

CALL

ICS

TXNORM

EMER

BK-UP

VOX

ISOCALL

TX



SAT PA

ISO

VHF1

CALL

ICS

TXNORM

EMER

BK-UP

VOX

ISOCALL

TX



SAT PA

IDPUSHVOL

PWR VOL

PUSH

SQ

VLOC

COM

C

VV

C

PUSHC/V

GARMIN GNS 430

GPSDEFAULTNAV

PUSHCRSR

PROCFPLMSGOBSCDI

ENTCLR

MENUD

RNG

IDPUSHVOL

PWR VOL

PUSH

SQ

VLOC

COM

C

VV

C

PUSHC/V

GARMIN GNS 430

GPSDEFAULTNAV

PUSHCRSR

PROCFPLMSGOBSCDI

ENTCLR

MENUD

RNG

PUNC

CLR

CRSR

STARTSTOP

IDENT ON

STBY

OFF

GARMIN

VFR

0 1 2 3 4 5 6 7 8 9

ALT


GTX 330

ICS

RX ICS

PTTPRESET

MIN

ICS

RX ICS

PTTPRESET

MIN

USE OF GPS 1 LIMITED TO VFR ONLY

Dual Pilot / Single Dual Pilot Flite Line Dual Pilot / Single Dual Pilot Dual Garmin GNS430

Figure 5.42: IFR solution with Glass Cockpit (MEGHAS)

DH

CRS

BARO

TST ND

NAVSOURCE

POS

EXT PFD STD

PUNC

CLR

CRSR

STARTSTOP

IDENT ON

STBY OFF

GARMIN

VFR

0 1 2 3 4 5 6 7 8 9

ALT


GTX 330

ISO

VHF1

CALLICS

TXNORM

EMER

BK-UP

VOX

ISOCALL

TX



SAT PA

ISO

VHF1

CALLICS

TXNORM

EMER

BK-UP

VOX

ISOCALL

TX



SAT PA

ICS

RX ICS

PTTPRESET

MIN

ICS

RX ICS

PTTPRESET

MIN

N

1 2

AHRS

N

1 2

ADC

N

1 2

FCDM

L R

MASTER

N

1 2

ICP

DH

CRS

BARO

TST ND

NAVSOURCE

POS

EXT PFD STD

COM/NAVWULFSBERG

117.300

112.800

RADON BRG

PWR

ACT

2

MODEVOL TUNE

COM/NAVWULFSBERG

117.300

112.800

RADON BRG

PWR

ACT

2

MODEVOL TUNE

HI NR

ON

NR

HIGH

CAUTION

MASTER

FRESH AIR

XMSNOIL P

EMEROFF

SW 1

ACTIVECARGO

TEMP SMOKE

LOWFUEL 2

BAT

LOWFUEL 1 OFF

EMER

SW 2

ACTIVEA.TRIMAP

RPM

BAT

ROTOR

DISCH

555

50

45

40

35

30

25

20

15

10

1234

5678910

11 12 01

2

3

6

7

8

9ALT

1013MB

1 0 0 0

100 FEE

ENG

ROTOR

N2

% RPM50

607080

0

90

100

110120

R

180

160

140120 100

80

60

4020

10

10

20

20

OFF

P U L L

C A GE

RO

OFF1

SCROLL

OFF2

RESET

SELECT

+

-

ENTER

-

+BRT

ON




OFF

SCROLL

DT

RESET

100


48 480 45FF1888XXX

FF2888XXX LANE 4 FAILED -> PRESS OFF2 LEFT

-10

-8

-6

-4

-20

2

4

ENG1 ENG2

TRQ101%

TRQ 65%

N1 83%

T4570°C

N1 90%

T4650°C

TOP4nm30s

MM LMT

OAT -888.8 X >8888 XX NE 888 XXX

HOOK 8888 X


-888.8 GEM XX -888.8

88.8 888 88 999 88.8 888

FLIGHT

IDLE

FLIGHT

IDLE

NORM

OFF

OFF

NORMON

OFF


OFF

ONON

FADEC

FADEC

ARM

OFF

OFFOFF OFF

RESET

GEN IIRESET

GEN IRESET

MSTRBAT

DME 2

HOLDHOLD

DME 1

BRT

OFF

MLS 1

AZ 359

23

12,6 NM8,0 MN

GS

GS

N3

6

12

15S21

24

30

33

W E

ADF 2

280

260

240

220

250

200

M.205

20

10

10

20

HDG VS ASEL

25500

24500M

DH200

250

250 0020

80

00

29.92

BRT

OFF

CALL SIGN

FRESH AIR

FRESH AIR

CALL SIGN

BRT+ BRT- CTR- CTR+

X

5000 M

FRESH AIR

FRESH AIR

CALL SIGN

BRT

OFF

MLS 1

AZ 359

23

12,6 NM8,0 MN

GS

GS

N3

6

12

15S21

24

30

33

W E

ADF 2

280

260

240

220

250

200

M.205

20

10

10

20

HDG VS ASEL

25500

24500M

DH200

250

250 0020

80

00

29.92

BRT

OFF

DH

CRS

BARO

TST ND

NAVSOURCE

POS

EXT PFD STD

DH

CRS

BARO

TST ND

NAVSOURCE

POS

EXT PFD STD

ISO

VHF1

CALL

ICS

TXNORM

EMER

BK-UP

VOX

ISOCALL

TX



SAT PA

ISO

VHF1

CALL

ICS

TXNORM

EMER

BK-UP

VOX

ISOCALL

TX



SAT PA

IDPUSHVOL

PWR VOL

PUSH

SQ

VLOC

COM

C

VV

C

PUSHC/V

GARMIN GNS 430

GPSDEFAULTNAV

PUSHCRSR

PROCFPLMSGOBSCDI

ENTCLR

MENUD

RNG

IDPUSHVOL

PWR VOL

PUSH

SQ

VLOC

COM

C

VV

C

PUSHC/V

GARMIN GNS 430

GPSDEFAULTNAV

PUSHCRSR

PROCFPLMSGOBSCDI

ENTCLR

MENUD

RNG

PUNC

CLR

CRSR

STARTSTOP

IDENT ON

STBY OFF

GARMIN

VFR

0 1 2 3 4 5 6 7 8 9

ALT


GTX 330

ICS

RX ICS

PTTPRESET

MIN

ICS

RX ICS

PTTPRESET

MIN

N

1 2

AHRS

N

1 2

ADC

N

1 2

FCDM

L R

MASTER

N

1 2

ICP


INTG

OBSAPR

TERMMSG

WPT

DME 2

HOLDHOLD

DME 1

FRESH AIR

XMSNOIL P

EMEROFF

SW 1

ACTIVECARGO

TEMP SMOKE

LOWFUEL 2

BAT

LOWFUEL 1 OFF

EMER

SW 2

ACTIVEA.TRIMAP

RPM

BAT

ROTOR

DISCH

555

50

45

40

35

30

25

20

15

10

1234

5678910

11 12 01

2

3

6

7

8

9ALT

1013MB

1 0 0 0

100 FEE

ENG

ROTOR

N2

% RPM50

607080

0

90

100

110120

R

180

160

140120 100

80

60

4020

10

10

20

20

OFF

P U L L

C A GE

RO

OFF1

SCROLL

OFF2

RESET

SELECT

+

-

ENTER

-

+BRT

ON




OFF

SCROLL

DT

RESET

100


48 480 45FF1888XXX


-10

-8

-6

-4

-20

2

4

ENG1 ENG2

TRQ101%

TRQ 65%

N1 83%

T4570°C

N1 90%

T4650°C

TOP4nm30s

MM LMT

OAT -888.8 X >8888 XX NE 888 XXX

HOOK 8888 X


-888.8 GEM XX -888.8

88.8 888 88 999 88.8 888

FLIGHT

IDLE

FLIGHT

IDLE

NORM

OFF

OFF

NORMON

OFF


OFF

ONON

FADEC

FADEC

ARM

OFF

OFFOFF OFF

RESET

GEN IIRESET

GEN IRESET

MSTRBAT

BRT

OFF

MLS 1

AZ 359

23

12,6 NM8,0 MN

GS

GS

N3

6

12

15S21

24

30

33

W E

ADF 2

280

260

240

220

250

200

M.205

20

10

10

20

HDG VS ASEL

25500

24500M

DH200

250

250 0020

80

00

29.92

BRT

OFF

CALL SIGN

A O M HLT

SENS

NR

HIGH

CAUTION

MASTER

HI NR

ON

FRESH AIR

FRESH AIR

CALL SIGN

BRT+ BRT- CTR- CTR+

X

5000 M

FRESH AIR

FRESH AIR

CALL SIGN

BRT

OFF

MLS 1

AZ 359

23

12,6 NM8,0 MN

GS

GS

N3

6

12

15S21

24

30

33

W E

ADF 2

280

260

240

220

250

200

M.205

20

10

10

20

HDG VS ASEL

25500

24500M

DH200

250

250 0020

80

00

29.92

BRT

OFF


Page 164 of 202 135.09.101.01

Technical Data

Dual Pilot / Single Dual Pilot FMS

Figure 5.43: IFR solution with Glass Cockpit (MEGHAS) and FMS

Single Pilot Flite Line Single Pilot Dual Garmin GNS430

Figure 5.44: Single Pilot IFR solutions with Glass Cockpit (MEGHAS)

P

I

L

C

IL

P

Z CLR

1 2 3

4 A B C D E F GH I J K L M NO P Q R S T UV W X Y

FREQ

INIT REF

NPAOFSTPOSMSGFAIL

DEP ARR

BRTFIXHOLD

PROG EXECLEGSRTENEXTPREVMENU

SP/±0.987

65

FUEL MARK

DH

CRS

BARO

TST ND

NAVSOURCE

POS

EXT PFD STD

DH

CRS

BARO

TST ND

NAVSOURCE

POS

EXT PFD STD

ISO

VHF1

CALL

ICS

RX ICS

ICS

TXNORM

EMER

BK-UP

PTTPRESET

MIN

VOX

ISOCALL

TX

VHF2 TAC1

NAV1 NAV2 DME1 DME2 MKR ADF

COM/NAVWULFSBERG

117.300

112.800

RADON BRG

PWR

ACT

2

MODEVOL TUNE

N

1 2

AHRS

N

1 2

ADC

N

1 2

FCDM

L R

MASTER

N

1 2

ICP

ISO

VHF1

CALL

ICS

RX ICS

ICS

TXNORM

EMER

BK-UP

PTTPRESET

MIN

VOX

ISOCALL

TX

VHF2 TAC1

NAV1 NAV2 DME1 DME2 MKR ADF

FRESH AIR

FRESH AIR

CALL SIGN

BRT+ BRT- CTR- CTR+

X

5000 M

FRESH AIR

FRESH AIR

CALL SIGN

BRT

OFF

MLS 1

AZ 359

23

12,6 NM8,0 MN

GS

GS

N3

6

12

15S21

24

30

33

W E

ADF 2

280

260

240

220

250

200

M.205

20

10

10

20

HDG VS ASEL

25500

24500M

DH200

250

250 0020

80

00

29.92

BRT

OFF

NR

HIGH

CAUTION

MASTER

NMS

DISCON

MKR

HINPA

HI NR

ON

555

50

45

40

35

30

25

20

15

10

1234

5678910

11 12 01

2

3

6

7

8

9ALT

1013MB

1 0 0 0

100 FEE

ENG

ROTOR

N2

% RPM50

607080

0

90

100

110120

R

180

160

140120 100

80

60

4020

10

10

20

20

OFF

P U L L

C A GE

RO

OFF1

SCROLL

OFF2

RESET

SELECT

+

-

ENTER

-

+BRT

ON




OFF

SCROLL

DT

RESET

100


48 480 45FF1888XXX


-10

-8

-6

-4

-20

2

4

ENG1 ENG2

TRQ101%

TRQ 65%

N1 83%

T4570°C

N1 90%

T4650°C

TOP4nm30s

OAT -888.8 X >8888 XX NE 888 XXX

HOOK 8888 X


-888.8 GEM XX -888.8

88.8 888 88 999 88.8 888

MM LMT

FLIGHT

IDLE

FLIGHT

IDLE

NORM

OFF

OFF

NORMON

OFF


OFF

ONON

FADEC

FADEC

ARM

OFF

OFFOFF OFF

RESET

GEN IIRESET

GEN IRESET

MSTRBAT

XMSNOIL P

EMEROFF

SW 1

ACTIVECARGO

TEMP SMOKE

LOWFUEL 2

BAT

LOWFUEL 1 OFF

EMER

SW 2

ACTIVEA.TRIMAP

RPM

BAT

ROTOR

DISCH

BRT

OFF

MLS 1

AZ 359

23

12,6 NM8,0 MN

GS

GS

N3

6

12

15S21

24

30

33

W E

ADF 2

280

260

240

220

250

200

M.205

20

10

10

20

HDG VS ASEL

25500

24500M

DH200

250

250 0020

80

00

29.92

BRT

OFF

FRESH AIR

CALL SIGN

DH

CRS

BARO

TST ND

NAVSOURCE

POS

EXT PFD STD

PUNC

CLR

CRSR

STARTSTOP

IDENT ON

STBY

OFF

GARMIN

VFR

0 1 2 3 4 5 6 7 8 9

ALT


GTX 330

ISO

VHF1

CALL

ICS

TXNORM

EMER

BK-UP

VOX

ISOCALL

TX



SAT PA

ISO

VHF1

CALL

ICS

TXNORM

EMER

BK-UP

VOX

ISOCALL

TX



SAT PA

ICS

RX ICS

PTTPRESET

MIN

ICS

RX ICS

PTTPRESET

MIN

N

1 2

AHRS

N

1 2

ADC

N

1 2

FCDM

L R

MASTER

N

1 2

ICP

AP A.TRIM

OFF OFF

A C

A C

APP

A C ON

IASVS

ON ON

ALT

ON

TEST

HDG ALT.A

INACTIVE GS

NAV

A C

DH

CRS

BARO

TST ND

NAVSOURCE

POS

EXT PFD STD

COM/NAVWULFSBERG

117.300

112.800

RADON BRG

PWR

ACT

2

MODEVOL TUNE

COM/NAVWULFSBERG

117.300

112.800

RADON BRG

PWR

ACT

2

MODEVOL TUNE

HI NR

ON

333

3024

21 15

126

TO

FR

GS

NAV

s

N

0W

OBS

NAV1 / HOLDINACTIVE

NAV 2

-12 RNV HLD FRQ KTS

NAV HOLD TTS

NM

NR

HIGH

CAUTION

MASTER

FRESH AIR

XMSNOIL P

EMEROFF

SW 1

ACTIVECARGO

TEMP SMOKE

LOWFUEL 2

BAT

LOWFUEL 1 OFF

EMER

SW 2

ACTIVEA.TRIMAP

RPM

BAT

ROTOR

DISCH

555

50

45

40

35

30

25

20

15

101234

5678910

11 12 01

2

3

6

7

8

9ALT

1013MB

1 0 0 0

100 FEE

ENG

ROTOR

N2

% RPM50

607080

0

90

100

110120

R

180

160

140120 100

80

60

4020

10

10

20

20

OFF

P U L L

C A GE

RO

OFF1

SCROLL

OFF2

RESET

SELECT

+

-

ENTER

-

+BRT

ON




OFF

SCROLL

DT

RESET

100


48 480 45FF1888XXX


-10

-8

-6

-4

-20

2

4

ENG1 ENG2

TRQ101%

TRQ 65%

N1 83%

T4570°C

N1 90%

T4650°C

TOP4nm30s

MM LMT

OAT -888.8 X >8888 XX NE 888 XXX

HOOK 8888 X


-888.8 GEM XX -888.8

88.8 888 88 999 88.8 888

FLIGHT

IDLE

FLIGHT

IDLE

NORM

OFF

OFF

NORMON

OFF


OFF

ONON

FADEC

FADEC

ARM

OFF

OFFOFF OFF

RESET

GEN IIRESET

GEN IRESET

MSTRBAT

FRESH AIR

FRESH AIR

DME 2

HOLDHOLD

DME 1

280

260

240

220

250

200

M.205

20

10

10

20

HDG VS ASEL

25500

24500M

DH200

250

250 0020

80

00

29.92

BRT

OFF

BRT

OFF

MLS 1

AZ 359

23

12,6 NM8,0 MN

GS

GS

N3

6

12

15S21

24

30

33

W E

ADF 2

CALL SIGN

NAV 2

NAV1 / HOLDINACTIVE

333

3024

21 15

126

TO

FR

GS

NAV

s

N

0W

OBS

INTG

OBSAPR

TERMMSG

WPT

DME 2

HOLDHOLD

DME 1

-12 RNV HLD FRQ KTS

NAV HOLD TTS

NM

FRESH AIR

XMSNOIL P

EMEROFF

SW 1

ACTIVECARGO

TEMP SMOKE

LOWFUEL 2

BAT

LOWFUEL 1 OFF

EMER

SW 2

ACTIVEA.TRIMAP

RPM

BAT

ROTOR

DISCH

555

50

45

40

35

30

25

20

15

101234

5678910

11 12 01

2

3

6

7

8

9ALT

1013MB

1 0 0 0

100 FEE

ENG

ROTOR

N2

% RPM50

607080

0

90

100

110120

R

180

160

140120 100

80

60

4020

10

10

20

20

OFF

P U L L

C A GE

RO

OFF1

SCROLL

OFF2

RESET

SELECT

+

-

ENTER

-

+BRT

ON




OFF

SCROLL

DT

RESET

100


48 480 45FF1888XXX


-10

-8

-6

-4

-20

2

4

ENG1 ENG2

TRQ101%

TRQ 65%

N1 83%

T4570°C

N1 90%

T4650°C

TOP4nm30s

MM LMT

OAT -888.8 X >8888 XX NE 888 XXX

HOOK 8888 X


-888.8 GEM XX -888.8

88.8 888 88 999 88.8 888

FLIGHT

IDLE

FLIGHT

IDLE

NORM

OFF

OFF

NORMON

OFF


OFF

ONON

FADEC

FADEC

ARM

OFF

OFFOFF OFF

RESET

GEN IIRESET

GEN IRESET

MSTRBAT

FRESH AIR

FRESH AIR

NR

HIGH

CAUTION

MASTER

HI NR

ON

280

260

240

220

250

200

M.205

20

10

10

20

HDG VS ASEL

25500

24500M

DH200

250

250 0020

80

00

29.92

BRT

OFF

BRT

OFF

MLS 1

AZ 359

23

12,6 NM8,0 MN

GS

GS

N3

6

12

15S21

24

30

33

W E

ADF 2

CALL SIGN

A O M HLT

SENS

DH

CRS

BARO

TST ND

NAVSOURCE

POS

EXT PFD STD

DH

CRS

BARO

TST ND

NAVSOURCE

POS

EXT PFD STD

ISO

VHF1

CALL

ICS

TXNORM

EMER

BK-UP

VOX

ISOCALL

TX



SAT PA

ISO

VHF1

CALL

ICS

TXNORM

EMER

BK-UP

VOX

ISOCALL

TX



SAT PA

IDPUSHVOL

PWR VOL

PUSH

SQ

VLOC

COM

C

VV

C

PUSHC/V

GARMIN GNS 430

GPSDEFAULTNAV

PUSHCRSR

PROCFPLMSGOBSCDI

ENTCLR

MENUD

RNG

IDPUSHVOL

PWR VOL

PUSH

SQ

VLOC

COM

C

VV

C

PUSHC/V

GARMIN GNS 430

GPSDEFAULTNAV

PUSHCRSR

PROCFPLMSGOBSCDI

ENTCLR

MENUD

RNG

PUNC

CLR

CRSR

STARTSTOP

IDENT ON

STBY

OFF

GARMIN

VFR

0 1 2 3 4 5 6 7 8 9

ALT


GTX 330

ICS

RX ICS

PTTPRESET

MIN

ICS

RX ICS

PTTPRESET

MIN

N

1 2

AHRS

N

1 2

ADC

N

1 2

FCDM

L R

MASTER

N

1 2

ICP

AP A.TRIM

OFF OFF

A C

A C

APP

A C ON

IASVS

ON ON

ALT

ON

TEST

HDG ALT.A

INACTIVE GS

NAV

A C



Technical Data

5.3 Antenna layouts

5.3.1 Typical VFR antenna layout

1. ELT antenna2. ATC antenna3. VOR antenna4. VHF 1 antenna5. GPS antenna

Figure 5.45: Typical VFR antenna layout


Page 166 of 202 135.09.101.01

Technical Data

5.3.2 Typical IFR antenna layout

1. ELT antenna2. VHF 2 antenna3. VOR antenna4. VHF 1 antenna5. GPS antenna6. ADF antenna (if required)7. Radar altimeter antenna8. ATC antenna9. Marker antenna10. DME antenna

Figure 5.46: Typical IFR antenna layout


Technical Data

5.4 Police

Whatever action the law enforcement mission requires, the EC135 offers the perfect solution. With itscompact size and shrouded tail rotor, the EC135 can land in confined areas. Its wide, unobstructedcabin offers increased visibility for observation operations. Mission flexibility, low noise, reduced main-tenance, operational costs and higher availability are among the many reasons why so many policeoperators have already chosen the EC135 for their daily operations.

The efficiency multiplierEurocopter has developed a wide range of equipment for the EC135 to meet the requirements of policeforces around the world. The cabin is night vision goggle (NVG) compatible, and can be configured witha state-of-the-art avionics glass cockpit. In addition, the wide, unobstructed cabin, with its flat floor andmultipurpose rails, allows operators to quickly and easily change configurations / mission equipment.

In accordance with the requirements of many police forces around the world, a wide range of equip-ment has been developed to ensure flexibility and support missions like:• Observation and command• Airborne surveillance• Pursuit• Border Patrol• Police escort• Rapid transportation of special equipment and units.


Page 168 of 202 135.09.101.01

Technical Data

5.4.1 Aircraft ParameterFlight Rules: IFRInstrumentation: Glass Cockpit (MEGHAS)Cat-A: Yes

Surveillance

Intervention

5.4.2 Typical components of a police configuration

HD EOS camera systemAvailable features:• HD Camera with zoom lens • Easy to operate • Stabilized turret• IR-Sensor • Hand controller• Geo Package with embedded GPS-Purge Kit for maintenance • Moving map interface • Laser range finder

EOS Operator consoleAvailable features:• Quick and easy installation and deinstallation• Integrated solution for controlling EOS system, search light SX16 as well as downlink system• Different monitor sizes available for displaying EOS or moving map images • Ergonomic design adjustable to individual needs• Low weight

Pilots 1 or 2

Operator 1

Pilots 1 or 2

Pax 5 (or 6)


Technical Data

Digital down-link systemAvailable features:• Large bandwidth• Different frequency ranges• 2 audio channels• Integrated encryption • High data rate

Search light SX16Available features:• IR Filter (IFCO)• Search light slaving to EOS camera

External loudspeaker systemAvailable features:• Sound pressure of 126dB at a distance of 8m and 90dB at a distance of 200m• Signal generator for two different siren sounds

Rope-down deviceAvailable features:• External installation• Rope-down possibility for tow persons from each side of the aircraft• Designed for fast roping and rappelling• Fixed provisions of external hoist can be used• RIA for improved clearance to the landing gear

Digital Moving Map System1

Available features:• Full color maps• Current position is constantly updated• Selection between north-up or track-up mode• Presentation of flight plan• Interface to FMS to exchange flight plans

Compatible maps2:• Scanned maps of any make or scale• Satellite maps• Arial photo maps• Maritime maps for offshore• All maps meet the WGS-84 GPS• Terrain elevation data

1.Approval for VFR only.2.Maps and special options not included in the EuroNav Moving Map system. To be purchased directly at EuroAvionics

(http://www.euroavionics.com)


Page 170 of 202 135.09.101.01

Technical Data

Weather and search radarAvailable features:• Color radar system with vertical profile• Ranges: 10, 20, 30, 80, 160 and 240 nm• System provides radar stabilization input for combined pitch, roll and tilt angles of up ±30°• Horizontal scanning angle 90°/100°

Tactical radiosFixed provisions for customer preferred radios

5.5 Additional available equipment

This chapter illustrates some optional highlights which are available on request. The EC135 is the re-ference helicopter with its wide breadth of available options. This document shows a synopsis of thewhole capability of this aircraft. If any mission equipment cannot be found in the technical data pleasedo not hesitate to contact EUROCOPTER® to receive further information.

Equipment on request:• High landing gear• High visibility painting for rotor blades• NVG friendly equipment• NVG certification• IR Flasher• HF System• Direction Finder• EGPWS System

5.6 Equipment required to comply with JAR-OPS 3

Basically EUROCOPTER® is able to deliver an equipment package which is derived from JAR-OPS 3Amendment 3. As the national operating rules may differ from the JAR-OPS 3 Amendment 3, the ope-rator has to contact its national authority to assure that the planned equipment configuration is ac-ceptable for the intended kind of operation.


Technical Data

Blank


Page 172 of 202 135.09.100.01

Technical Data

6 Main Performance

The following performance values and figures refer to an EC135, equipped with average productionengines.

Unless otherwise specified, the values and figures refer to a clean helicopter at Sea Level (SL), in In-ternational Standard Atmosphere (ISA) and zero wind condition.

Performance on 2 engines (AEO) Pratt & Whitney PW206B2

Gross Weight kglb

2,7206,000

2,8356,250

2,9106,415

• Maximum speed (VNE) km/hkts

278150

259140

259140

• Maximum cruising speed (VH) km/hkts

257139

256138

254137

• Fuel consumption at fast cruise speed kg/hlb/h

234.5517

234.5517

234.5517

• Economical cruising speed km/hkts

226122

228123

230124

• Fuel consumption at economicalcruising speed

kg/hlb/h

200.5442

204.5451

208.5460

• Fuel consumption at 65 KIAS kg/hlb/h

158.5349.5

162357

164.5363

• Rate of climb, TOP, SL, ISA m/sft/min

8.91,750

8.11,600

7.61,500

• Hover ceiling IGE (4 ft AGL), TOP,no wind or headwind, ISA + 20°C

mft

4,14013,600

3,655a

12,000a3,045b

10,000b


mft

3,09510,150

2,6958,850

2,4358,000

• Hover ceiling OGE, TOP, ISA mft

3,43011,050

2,6858,800

2,0106,600

• Hover ceiling OGE, TOP, ISA +20°C mft

2,2107,250

1,7855,580

1,4804,850

• Service ceiling, MCP,(climb reserve 200 ft/min), ISA

mft

5,15516,900

3,655a

12,000a3,045b

10,000b

• Maximum range (without fuel reserve at economical cruise speed)

• standard fuel tank configuration (560 kg)

• long range fuel tank configuration (730 kg)

kmnmkmnm

645348850459

640345840454

635342835451

Table 6.7: Performance on 2 engines (AEO) Pratt & Whitney PW206B2


Technical Data

Performance on 1 engine (OEI) Pratt & Whitney PW206B2

• Maximum endurance (without fuel reserve at 65 KIAS

• standard fuel tank configuration (560 kg)• long range fuel tank configuration (730 kg)

h:minh:min

3:434:55

3:384:49

3:354:45

a.12,000 ft pressure altitude certification limitb.10,000 ft pressure altitude certification limit

Gross Weight kglb

2,7206,000

2,8356,250

2,9106,415

Table 6.7: Performance on 2 engines (AEO) Pratt & Whitney PW206B2

Gross Weight kglb

2,7206,000

2,8356,250

2,9106,415

• Service ceiling with 100 ft/min climb reserve, MCP OEI-power, ISA

mft

3,27510,750

2,9259,600

2,7158,900

• Service ceiling with 100 ft/min climb reserve, MCP OEI-power, ISA + 20°C

mft

2,3757,800

1,9656,450

1,7105,600

• Rate of climb, MCP OEI-power, SL m/sft/min

1.9375

1.4275

1.1215

• Max. temperatur for CAT A, take-off from clear heliport at SL

°C +50 +46 +43

• Max. gross weight hover IGE (4ft AGL), SL, ISA, no wind, 2 min OEI power

kglb

2,8706,325

• Max. gross weight hover IGE (4ft AGL), SL,ISA +20°C, no wind, 2 min OEI power

kglb

2,6755,885

• Max. gross weight hover OGE, SL,ISA, no wind, 30 sec OEI power

kglb

2,6655,875

• Max. gross weight hover OGE, SLISA +20°C, no wind, 30 sec OEI power

kglb

2,5855,687

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

kglb

2,9106,415

• Max. gross weight CAT A, VTOL, SL,ISA +20°C

kglb

2,8456,270

Table 6.8: Performance on 1 engine (OEI) Pratt & Whitney PW206B2


Page 174 of 202 135.09.101.01

Technical Data

Performance on 2 engines (AEO) Turbomeca Arrius 2B2

Gross Weight kglb

2,7206,000

2,8356,250

2,9106,415

• Maximum speed (VNE) km/hkts

278150

259140

259140

• Maximum cruising speed (VH) km/hkts

257139

256138

254137

• Fuel consumption at fast cruise speed kg/hlb/h

234.5517

234.5517

234.5517

• Economical cruising speed km/hkts

237128

239129

240130

• Fuel consumption at economicalcruising speed

kg/hlb/h

215474

219483

221487

• Fuel consumption at 65 KIAS kg/hlb/h

167.5369

170.5376

173381

• Rate of climb, TOP, SL, ISA m/sft/min

8.91,750

8.11,600

7.61,500

• Hover ceiling IGE (4 ft AGL), TOP,no wind or headwind, ISA

mft

4,32514,200

3,655a

12,000a3,045b

10,000b


mft

3,08011,050

2,6708,750

2,3957,850

• Hover ceiling OGE, TOP, ISA mft

3,43011,050

2,6858,800

2,0106,600

• Hover ceiling OGE, TOP, ISA +20°C mft

2,1757,150

1,7405,700

1,4504,750

• Service ceiling, MCP,(climb reserve 200 ft/min), ISA

mft

5,15516,900

3,655a

12,000a3,045b

10,000b

• Maximum range (without fuel reserve at economical cruise speed)

• standard fuel tank configuration (560 kg)

• long range fuel tank configuration (730 kg)

kmnmkmnm

630340825446

625337820443

620334815440

• Maximum endurance (without fuel reserve at 65 KIAS

• standard fuel tank configuration (560 kg)• long range fuel tank configuration (730 kg)

h:minh:min

3:294:36

3:264:32

3:234:28

Table 6.9: Performance on 2 engines (AEO) Turbomeca Arrius 2B2

a.12,000 ft pressure altitude certification limitb.10,000 ft pressure altitude certification limit


Technical Data

Performance on 1 engine (OEI) Turbomeca Arrius 2B2

OPERATING LIMITATIONS (valid for both versions, EC135 P2i and EC135 T2i)The helicopter can be operated within the following altitude and temperature limitations (according tothe Flight Manual):

Gross Weight kglb

2,7206,000

2,8356,250

2,9106,415

• Service ceiling with 100 ft/min climb reserve, MCP OEI-power, ISA

mft

3,52011,550

3,18510,450

2,9559,700

• Service ceiling with 100 ft/min climb reserve, MCP OEI-power, ISA + 20°C

mft

2,5008,200

2,0706,800

1,7955,900

• Rate of climb, MCP OEI-power, SL m/sft/min

1.9375

1.4275

1.1215

• Max. temperatur for CAT A, take-off from clear heliport at SL

°C +50 +47 +43.5

• Max. gross weight hover IGE (4ft AGL), SL, ISA, no wind, 2 min OEI power

kglb

2,8706,325

• Max. gross weight hover IGE (4ft AGL), SL,ISA +20°C, no wind, 2 min OEI power

kglb

2,6905,930

• Max. gross weight hover OGE, SL,ISA, no wind, 30 sec OEI power

kglb

2,6655,875

• Max. gross weight hover OGE, SLISA +20°C, no wind, 30 sec OEI power

kglb

2,6155,765

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

kglb

2,9106,415

• Max. gross weight CAT A, VTOL, SL,ISA +20°C

kglb

2,8606,305

Table 6.10: Perfomance on 1 engine (OEI) Turbomeca Arrius 2B2

Gross Weight 2,720 kg6,000 lb

2,835 kg6,250 lb

2,910 kg6,415 lb

• Maximum operting altitude 6,095 m PA20,000 ft PA

3,655 m PA12,000 ft PA

3,045 m PA10,000 ft PA

• Maximum operating altitude for hover inground effect, takeoff and landing

4,570 m DA15,000ft DA

3,655 m PA12,000 ft PA

3,045 m PA10,000 ft PA

• Minimum temperature -35°C (-31°F)

• Maximum temperature ISA +39°C(max. +50°C / +122°F)

Table 6.11: Operating limitations


Page 176 of 202 135.09.101.01

Technical Data

Hover In Ground Effect (HIGE, TOP, no wind)with two PW206B2 engines


Technical Data

Hover In Ground Effect (HIGE, TOP, no wind)with two ARRIUS 2B2 engines


Page 178 of 202 135.09.101.01

Technical Data

Hover Out Of Ground Effect (HOGE, TOP)with two PW206B2 engines


Technical Data

Hover Out Of Ground Effect (HOGE, TOP)with two ARRIUS 2B2 engines


Page 180 of 202 135.09.101.01

Technical Data

Hover Out Of Ground Effect (HOGE, 30 sec OEI power)with one PW206B2 engine


Technical Data

Hover Out Of Ground Effect (HOGE, 2.0 min OEI power)with one PW206B2 engine


Page 182 of 202 135.09.101.01

Technical Data

Hover Out Of Ground Effect (HOGE, 30 sec OEI power)with one ARRIUS 2B2 eninge


Technical Data

Hover Out Of Ground Effect (HOGE, 2.0 min OEI power)with one ARRIUS 2B2 engine


Page 184 of 202 135.09.101.01

Technical Data

Maximum Cruising Speedwith two PW206B2 engines


Technical Data

Maximum Cruising Speedwith two ARRIUS 2B2 engines


Page 186 of 202 135.09.101.01

Technical Data

Maximum Rate Of Climb, TOPwith two PW206B2 engines


Technical Data

Maximum Rate Of Climb, TOPwith two ARRIUS 2B2 engines


Page 188 of 202 135.09.101.01

Technical Data

Payload / Rangewith two PW206B2 engines


Technical Data

Payload / Rangewith two ARRIUS 2B2 engines


Page 190 of 202 135.09.101.01

Technical Data

7 Support information

7.1 Assets

Proven reliability and availability based on experienceEUROCOPTER®'s helicopter production programs have developed a strong reputation world-wide forbeing fully committed to providing customers with operational, capable aircraft that achieve high availa-bility combined with cost-effective support systems. To achieve this record of performance, EURO-COPTER® has stressed the importance of working together with its customers to ensure constantfeedback 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 sa-fety.EUROCOPTER® has built and delivered EC135 helicopters for almost 10 years. More than 800helicopters are in service world wide. The total flight hours accumulated at the end of the year 2008are more than 1,261,274 Fh.

7.2 Inspection Programm

Airframe Inspection ProgrammThe Maintenance Program specifies the intervals between maintenance operations that are recom-mended by EUROCOPTER®, 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.

For the performance of the scheduled and unscheduled maintenance, EUROCOPTER® has classifiedthe maintenance tasks by the following three maintenance levels:

Organizational Level (O)This level comprises of tasks such as the daily servicing, pre-flight checks, visual inspections for con-dition, replacement of modular components and simple repairs. This work can be performed by trainedhelicopter mechanics with standard tools only (no special tools necessary).

Intermediate Level (I)This level comprises of tasks such as the daily servicing, pre-flight checks, visual inspections for con-dition, replacement of modular components and simple repairs. This work can be performed by trainedhelicopter mechanics with standard tools only (no special tools necessary).

Depot Level (D)This level comprises of tasks such as repairs OFF helicopter, overhaul of major components and heavyairframe repair. This work can be performed by OEM, authorized Repair Centers or EUROCOPTER®and requires the usage of special overhaul and repair tools, as well as test benches (if required) accor-ding to repair manuals or instructions.The maintenance tasks defined as O-and I-Level are described in the Aircraft Maintenance Manual(AMM) and can be conducted by operator's mechanics after successful completion of the relevant trai-ning courses.

The following table provides an overview of all Scheduled Airframe Inspections. Scheduled inspectionswith shorter time intervals are fully incorporated into those with longer time intervals, this means, thatfor example the Periodical Inspection contains the 12-Month Inspection.


Technical Data

All those "Estimated Mean Man Hours" mentioned here above refer only to the scheduled inspectionin accordance with the Master Servicing Manual (MSM) for the standard helicopter without optionalequipment. The announced Man Hours are without ground run and test flight, work preparation anddocumentation work as well as reworking and servicing.

Scheduled Airframe Inspection Maintenance Level Estimated Mean Man Hours

Pre-flight Check O - Level 0.5 hours

12-month inspection(max. exceedance by 3 month)

O - Level 25 hours

Intermediate inspection every 400 hours(max. exceedance by 40 hours)

O - Level 45 hours

Periodical inspection every 800 hours or 3years(max. exceedance by 80 hours or 3 month)

I - Level 79 hours

Supplementary Inspections according to ope-rating time(max. exceedance by 10%)

I - Level n/a

Conditional Inspections after specific operati-onal incidents(max. exceedance by 10%)

I - Level n/a

Table 7.12: Inspections

Scheduled Engine Maintenance for PW206B2

Periodic Inspections

Maintenance Level Estimated Mean Man Hour

12 month O - Level 1 hour

800 Hours O - Level 6 hours

Table 7.13: Pratt & Whitney

Scheduled Engine Maintenance for ARRIUS 2B2

Periodic Inspections

Maintenance Level Estimated Mean Man Hour

400 Hours Level 1 1,5 hour

800 Hours Level 1 4,0 hours

Table 7.14: Turbomeca


Page 192 of 135.09.101.01202

Technical Data

7.3 Main components

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

Note: list includes only components under 10,000 Fh. The figures can be changed

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 ser-vice for the next interval. A TBO is granted with a 10 % operational margin, limited at +300 hours. Allsubcomponents may have a Service Life limit, rated above the TBO limit.

Service Life Limited (SLL):The service life limit is an airworthiness limit. The component in question must be removed from servicewhen it reaches the limit indicated.

Main Components TBO as perMSM Rev. 8

SLL as perMSM Rev. 8

Fuel system: Motor Pump Cartridge 5,000 Fh

Ventilation / heating system:Blower drive motor ( depending on carbon brushes wear)

800 Fh

Starter / Generator 200 A 2,000 Fh

Portable fire extinguisher 10 years TSN10 years TSO

Main rotor blade damper 8,000 Fh or 6 years

Swash plate:Rings (control ring and bearing ring)

8,300 Fh

Mixing Lever Gear unit: bolt 8,700 Fh

Mixing Lever Gear unit: forked lever 9,000 Fh

Main Transmission 4,000 Fh

Main Transmission: pinions 8,000 Fh

Tail Rotor Gearbox 3,600 Fh

Tail Rotor Gearbox: bevel drive pinion 8,000 Fh

Tail Rotor Blade 8,000 Fh

Engine 3,500 Fh

Table 7.15: Main components


Technical Data

7.4 Eurocopter Maintenance Support Programs

EUROCOPTER® offers its clients a comprehensive array of repair and overhaul services to ensureavailability and costs control. This array of services ranges from basic OEM repair and overhaul ser-vices 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 custo-mers:• with a hig 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® offers the following flexible and mo-dular 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

On request, EUROCOPTER® is able to propose extensive services adapted to specific mission andcustomer expectations, as stock and maintenance management.

7.4.1 Classical SupportThe classical support consists of a comprehensive Initial Provisioning package to sustain aircraft ope-ration. This package includes Spare Parts, Tools, Test Equipment, etc..

The required level of operational availability determines the quantity and therefore the investment re-quired. With this support package the Customer bears the responsibility to monitor their repair; manageobsolescence and to procure the right mix and quantity of components and spare parts.

7.4.2 Maintencance, Repair and OverhaulEUROCOPTER® offers a complete range of industry-leading inspection, repair and overhaul capabi-lities for the full range of EUROCOPTER® helicopters, with guaranteed turn-around times and cost-effeciency.

Approved by the most stringent airworthiness authorities in the world, our industrial facilities ensure thehighest quality for the maintenance, repair and upgrading works. EUROCOPTER® Maintenance Re-pair and Overhaul covers the four major following areas:• Blades• Equipment• Dynamic component• Maintenance & upgrades


Page 194 of 135.09.101.01202

Technical Data

7.4.3 Standard ExchangeThe Standard Exchange consists in replacing a defective part with a serviceable and interchangeablepart within 48 hours subject to availability. This service is available for equipment, blades and dynamiccomponents.

7.4.4 Guaranteed DMC (Repair by the Hour)The Guaranteed DMC services offers guaranteed repair and overhaul TATs as well as guaranteed pri-ces. 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 bothhis scheduled as unscheduled maintenance expenses. The guaranteed DMC service is available fordynamic components, blades and basic equipment.

7.4.5 Unscheduled Maintenance Insurance Plan (UMIP)With the UMIP, EUROCOPTER® gives the customer the option to secure unscheduled maintenancecosts 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 within24H through Standard Exchange based on a dedicated inventory. This service is available for dynamiccomponents, 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 sametime guaranteed maintenance costs, reduced inventory and minimized helicopter downtime. This ser-vice is intended for Customers looking for total cost control and high level of aircraft readiness. Pricefor this service is calculated per flight hour.

The PBH sevice includes component unscheduled repairs component overhauls as well as Life Limitedpart replacement. Parts replacement is guaranteed within 24H trough Standard Exchange based on adedicated inventory. This service is available for dynamic components, blades and equipment.


Technical Data

7.5 Engine Maintenance program

7.5.1 Pratt & WhitneyWith over 4,500 P&WC engines on a "pay-by-the-hour" concept, the industry has demonstrated its con-fidence on the advantages of the following services:

Eagle Service Plan ®

Fleet Management Plan ®

e Business Customer Portal

7.5.1.1 PW206B2 Mean Time Between Overhaul (MTBO)

The PW206B2 engine can be overhauled as two (2) individual modules:1. Perform overhaul of the turbomachinery module every 3500 .2. Perform overhaul of the reduction gearbox module every 3500 hours.

No Hot-section inspection (HSI) is scheduled and, if necessary, component replacement will be on anon-condition basis.

The maintenance plan for the PW200 engine incorporates the following features:

The minimisation of scheduled maintenance in accordance with MSG-III style analysis.

Helicopter Engine Condition and Trend Monitoring (HECTM®) used to determine the economicalthreshold to perform refurbishment.

Repair development will continue during service of the PW200 engine with the objective of expandingon repair schemes currently contained in both the Maintenance Manual and Overhaul Manual. This willkeep engine maintenance costs, aircraft downtime, spare engine inventories and total operating coststo a minimum.

Accessories Time Between OverhaulEngine accessories are monitored, as defined by the Illustrated Parts Catalog, with a removal thresholdthat is based on the operator's experience, with the following exception: TBO recommendation for theFuel Management Module (FMM) is engine TBO plus 500 hours.

Periodic Inspection - TolerancesUnless otherwise stated, the tolerance for periodic or scheduled inspections are as follows:• Hourly Intervals tolerance: Ten percent (10%), or up to a maximum of 100 hours operating time,

whichever is less.• Calender Intervals tolerance: Ten percen (10%), or up to a maximum of 30 days calender time,

whichever is less.

Note:The tolerance is established for maintenance scheduling convenience only and must be approved bythe governing civil aviation authority. Subsequent intervals will be adjusted to re-establish the originalschedule. When an inspection is done more than 10% early, subsequent inspections will be advancedas required so as to not exceed the maximum tolerance. Concurrence and final approval of the inspec-tion interval tolerance by the governing civil aviation authority is the responsibility of the owner/opera-tor.


Page 196 of 135.09.101.01202

Technical Data

7.5.1.2 Service Life Limited (SLL) Components

Three components on the PW206B2 are cycle limited:

The compressor Turbine Disk is commercially supported to 15.000 cycles.

7.5.2 TurbomecaAlways looking to maximize your efficiency and reduce your costs, Turbomeca, the engine manufac-turer has developed an improved service offering.

Whatever the mission, wherever it may be, for business or pleasure, Turbomeca offers a range of ser-vices tailored to your needs.

Standard Exchange: reduces lead times an operational losses by allowing you to exchange the engineor module up for repairs or maintenance at a preferred rate. AOG: when you need the speed, efficien-cy, dedicated resources and clear plan of action, an AOG team and dedicated communication chan-nels are implemented the resolve the situation in the most efficient an timely fashion.

Help Line: a multi-skilled team is at you disposal 24/7 to answer questions and quickly implement ef-fective solutions for all your emergency situations.

Warranty: 3 years / 2500 h whichever comes first.

Tailored Support By the Hour ® "SBH" contracts: packages are customized and charged monthly ac-cording to the number of hours you fly, with no minimums. From basic engine support to fully compre-hensive care, SBH ® offers flexibility an ease of use for the coverage you need when you need ist (OHfor engines/modules/accessories, Life Limited Parts, standard exchange or rental system, modular orcomplete engine maintenance, FOD, ASH, on-site technical assistance, etc.)

Turbomeca Internet Web Site - TOOLS: fully interactive web site developed an programmed specifi-cally for your support needs.

Evironment: clean burning with no visible smoke or exhaust soot; the Arrius smoke number is one ofthe lowest in the industry.

Impeller 15,000 Cycles

Compressor Turbine Disk 10,000 Cycles

Power Turbine Disk 15,000 Cycles

Table 7.16: Service Life Limited Components


Technical Data

7.5.2.1 Time Between Major Overhauls

The initial TBO value of the ARRIUS 2B2 applicable to the engine / modules / accessories are :• Complete engine 3,500 hours • Module 01 (accessory & reduction gearbox) 3,500 hours• Module 02 (Gas generator) 3,500 hours• Fuel Control Unit 3,500 hours or 10 years (first occurs)

All Gas Generator parts can be replaced in the field through 20 Deep Maintenance procedures.

7.5.2.2 Life Limited Parts (LLP)

Certain components of the engine, failure of which is classified as an Hazardous effect according toEngine Regulation, have service Life Limits expressed in cycles (reference flight cycle). They areknown 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 partcan run before having to be withdrawn from service.

Cycles are calculated automatically by the Engine Electronic Control Unit. Average experienced rateis about 0,5 cycles / flight hour.

The Life-Limited Parts on the ARRIUS 2B2 are : • Centrifugal impeller 20,000 cycles • HP turbinbe disc 13,000 cycles • Power turbine disc 14,000 cycles


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Technical Data

7.6 Training

With more than 50 years of experience, the EUROCOPTER® training centers provide the most com-prehensive, 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 organisation such as Véritas,AFAQ…EUROCOPTER® training centers provide a wide range of courses and services, from basictraining up to preparation for the most sophisticated civil and military missions.

As part of the full range of services on offer, EUROCOPTER® also plays an active role in helicopterpilot development through its Ab Initio programs.

Centers are equipped with multimedia classrooms. This includes computers overhead projectors andstate-of-the-art means such as Computer Based Training (CBT), Computer Aided Instruction (CAI),and Avionics Trainer . Some centers also have self-learning laboratories.EUROCOPTER® has set upa network of 14 training centers. For detailed information refer to EUROCOPTER® specific publication.

Starting in 2009 training can be performed on EUROCOPTER® owned simulators FTD (Flight TrainingDevices) of hightest level according to EASA and JAA standards - based in Europe and North America.


Technical Data

EC135 Training Means (Overview)

7.7 Technical publications

EUROCOPTER® provides all the technical publications necessary for safely operating and maintai-ning its aircraft cost effectively.

The printed version of the Aircraft Maintenance Manual (AMM), the System Discription Section (SDS)and the Wiring Diagram Manual (WDM) are tailored to the configuration of your helicopter(s).EURO-COPTER® 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 Ma-nual (WDM), the Corrosion and Erosion Control Guide (CECG) and the Structural Repair Manual(SRM).

The component maintenance manual (CMM) is available on CD-ROM or hard copy, depending on theVendor.

Along with the INDOC CD-ROM, EUROCOPTER® provides a hard copy of the Airworthiness andTechnical Publication (Flight Manual, Pilots Check List, Master Servicing Manual …) as well as the Ser-vice Bulletin Catalogue.

The CD ROM is available in English, French or German; it includes the latest information and is upda-ted regulary.

Computer Based Training (CBT)

Computer AidedInstruction (CAI)

Avionics Trainer

Flight Simulators

• Pilot & mechanics self training

• Access via internet server

• Including testing module

• Teaching materialincl. smart board

• Avionics/Electrics• Flight Control• Hydraulics

• Avionics WorkloadTrainer

• Overhead Panel• Sight System with

37‘‘ monitor andCOTS data base

• 2 Flight SimulationDevices at EC in Germany and the US

• OEM High fidelity & EC135 specific FlightSimulation package

Table 7.17: Overview Training Means


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Technical Data

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

7.8.1 DescriptionT.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)• List of Master Minimum Equipment List (MMEL)• Service Life Limited Parts

7.8.2 Main features• Each time a publication is issued, the customer is automatically informed by an e-mail.• A small summary, already included in the e-mail, helps the customer to understand quickly the sub-

ject.• Small icons allow the customer to identify immediately the type of information received.• The download of the publication in pdf format is possible after logging on the T.I.P.I. website.• A keywords search tool is provided (aircraft family, type of publication, date of edition...).

Adress: www.eurocopter.com/techpubThe publications are available in English, French or German depending on the case.


Technical Data

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