EC135 Technical data

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The data set forth i n this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.This document is property of EUROCOPTER, no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. EUROCOPTER 2010

Table of Content

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

1.1 News, Highlights and Main Improvements............................................................................................. 8

2 General Characteristics............................................................................................................................. 11

2.1 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 Basel ine Air craft Definit ion ........................................................................................................... 15

4 Recommended Miss ion Conf igurations .................................................................................................. 17

4.1 Emergency Medical Services (EMS) ................................................................................................... 194.1.1 EMS - Glass Cockpit (Air Ambulance Technology) .............................................................................................................. 20

4.1.2 EMS - Glass Cockpit (Aerolite) ............................................................................................................................................. 30

4.2 Disaster Management.......................................................................................................................... 414.2.1 Disaster Management (Air Ambulance Technology) ............................................................................................................42

4.2.2 Disaster Management (Aerolite) ........................................................................................................................................... 55

4.3 Corporate............................................................................................................................................. 694.3.1 Mission Parameter ................................................................................................................................................................ 70

4.3.2 Basic Mission Configuration .................................................................................................................................................70

4.3.3 Further Available Equipment ................................................................................................................................................ 73

4.3.4 Material and Color Definition ................................................................................................................................................ 76

4.3.5 Performance Data.................................................................................................................................................................77

4.4 Executive ............................................................................................................................................. 794.4.1 Mission Parameter ................................................................................................................................................................ 80



4.4.4 Material and Color Definition ................................................................................................................................................ 86


4.5 HERMS.............................................................................................................................................. 894.5.1 Mission Parameter ................................................................................................................................................................ 90




4.6 Utility .................................................................................................................................................... 974.6.1 Mission Parameter ................................................................................................................................................................ 98


4.6.3 Further Available Equipment .............................................................................................................................................. 101

4.6.4 Performance Data............................................................................................................................................................... 105

4.7 Offshore - Oil and Gas ....................................................................................................................... 1074.7.1 Mission Parameter.............................................................................................................................................................. 108

4.7.2 Basic Mission Configuration ............................................................................................................................................... 108

4.7.3 Further Available Equipment .............................................................................................................................................. 112

4.7.4 Performance Data............................................................................................................................................................... 115


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The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.This document is property of EUROCOPTER, no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. EUROCOPTER 2010

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Table of Content

5 Further Product Information ................................................................................................................... 117

5.1 Avionics.............................................................................................................................................. 117

5.1.1 VFR Solutions..................................................................................................................................................................... 1175.1.2 IFR with Conventional Instrumentation............................................................................................................................... 119

5.1.3 IFR Solutions with Glass Cockpit (MEGHAS) .................................................................................................................... 119

5.2 Antenna Layouts ................................................................................................................................ 1225.2.1 Typical VFR Antenna Layout .............................................................................................................................................. 122

5.2.2 Typical IFR Antenna Layout ............................................................................................................................................... 122

5.3 General Options - Overview............................................................................................................... 123

5.4 Police ................................................................................................................................................. 1285.4.1 Aircraft Parameter .............................................................................................................................................................. 129

5.4.2 Typical Components of a Police Configuration................................................................................................................... 129

5.5 NVG Certification ............................................................................................................................... 131

5.6 Additional Available Equipment.......................................................................................................... 132

5.7 Equipment Required to Comply with JAR-OPS 3 .............................................................................. 132

6 Main Performance .................................................................................................................................... 133

7 Support information................................................................................................................................. 151

7.1 Assets ................................................................................................................................................ 151

7.2 Inspection Program............................................................................................................................ 151

7.3 Main Components.............................................................................................................................. 153

7.4 Eurocopter Maintenance Support Programs...................................................................................... 154

7.4.1 Standard Support ............................................................................................................................................................... 1547.4.2 Standard Exchange ............................................................................................................................................................ 154

7.4.3 Repair with Guaranteed TAT .............................................................................................................................................. 155

7.4.4 Guaranteed DMC (Repair by the Hour).............................................................................................................................. 155

7.4.5 Unscheduled Maintenance Insurance Plan (UMIP)............................................................................................................ 155

7.4.6 Parts by the Hour (PBH)..................................................................................................................................................... 155

7.5 Engine Maintenance Program............................................................................................................ 1557.5.1 Pratt & Whitney................................................................................................................................................................... 155

7.5.2 Turbomeca ......................................................................................................................................................................... 157

7.6 Training .............................................................................................................................................. 158

7.7 Training Means .................................................................................................................................. 159

7.8 Technical Support .............................................................................................................................. 1627.9 Technical Publications ....................................................................................................................... 162

7.10 T.I.P.I (Technical Information Publication on Internet) ..................................................................... 162

7.10.1 Description........................................................................................................................................................................ 162

7.10.2 Main Features................................................................................................................................................................... 163

8 List of Abbreviat ions ............................................................................................................................... 165


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Technical Data

Manufacturers notes

EUROCOPTERs policy is one of on-going product enhancement which means that alterations indefinition, 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 ascertaining

with 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, MARMS and Stylence are trade marks of the EUROCOPTER

group.


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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 Fenestronwith 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 Fh. 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 engines,in 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.

Figure 1.1: Example of the EC135


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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 loading 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 simplifiesengine and torque monitoring. Being relieved from the instrument scan without missing vital informati-on, the pilot/s can dedicate more of his/their attention to the mission.

Figure 1.2: View from rear into the empty cabin


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Technical Data

Conventional instrumentation (analog instruments)

Glass cockp it instrumentation (MEGHAS / FCDS)

Figure 1.3: Conventional instrumentation (analog instruments)

Figure 1.4: Glass Cockpit Instrumentation (MEGHAS / FCDS)


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1.1 News, Highlights and Main Improvements

New basic ventilating system

A new and improved basic ventilating system is now 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 system

A new air conditioning system is now available. The new features 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 1.5: New outlets of airconditioning system


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Technical Data

2 General Characteristics

2.1 Exterior Dimensions


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2.2 Interior Dimensions

2.3 Possible Cabin Arrangement (Seats & Equipment as Option)

Passenger transpor t

EMS mission

Floor area Volume

Cabin & baggage compartment 4.35 m 46.83 ft 4.90 m 173.04 ftCockpit (pilot side) 1.15 m 12.38 ft 1.00 m 35.31 ft

Total (undivided) 5.50 m 59.21 ft 5.90 m 208.35 ft

Standard Corporate Executive Hermes

Pilots Passengers Pilpts Passengers Pilots Passengers Pilots Passengers1 6/7 1 (5) / 6 / (7) 1 5 / (6) 1 5

2 5/6 2 (4) / 5 / (6) 2 4 / (5) 2 4

Pilot Litter seats for doctor ans attendants

1 1 up to 4

1 2 up to 3

2 1 up to 32 2 up to 2


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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 shp ch

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

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


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Technical Data

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, hy-draulic and cooling system

Cowlings for main transmission and engine Skid-type landing gear with skid protectors, capable of ta-

king 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 integra-ted 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 copi-

lot seats with head rest and 4-point safety belts with auto-matic 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 pi-lot's collective pitch lever

Instrument panel with extension on pilot's side and glareshield

Ram-air and electrical ventilating system for cockpit andcabin

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 Multifunction Display (VEMD) withindication of: Torque Engine parameters (N1-RPM (for P&W) orN1-RPM

(for TM), oil pressure, oil temperature, Turbine OutletTemperature (TOT), engine/FADEC rep EEC failureand parameter code messages, self diagnoses)

FLI (First Limit Indicator) for TQ, TOT, N1 (for P&W)or N1 (for TM) as analogue display

Main transmission parameters (oil pressure, oil tem-perature)

Dual ammeter (generator) Ammeter (battery) Dual voltmeter Outside Air Temperature (OAT) Automatic in flight power check Parameters of optional equipment (e.g. internal long

range fuel tank)

Clock (2") Magnetic compass Engine cycle counter (on flight report page) Triple (rotor and engines) RPM-indicator (2") Standard instruments: (single pilot)a

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, pilotside

Static pressure crossover system Air Data computer

a.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.

POWER PLANT

Two PRATT & WHITNEY PW206B2 turbine engines orTwo TURBOMECA ARRIUS 2B2 turbine enginesThese 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


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Technical Data

4 Recommended Mission Configurations

EUROCOPTER DEUTSCHLAND GMBHproposes the following favorite mission configurations forthe EC135. The created packages should be regarded as a first proposal to provide the customers witha first overview and to give a first impression about the EC135 and its multiple features.

Available miss ion configurat ions

The following recommended mission configurations are available:

EMS - Glass Cockpit

Disaster Management

Corporate

Executive

Herms 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 and Aerolite.

General structure

All 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 customers choice on top of therespective Basic Mission Configuration.

General rules for adding options to the basic mission configuration

Some 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 DEUTSCHLAND GMBH.

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: Sand filter system or inlet barrier filter system External hoist Sliding door fastener (for each side of the helicopter) Lashing points Stretcher type Headsets Headset adapter cable crew Headset adapter cable pax


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Technical Data

Performance calculation

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

EUROCOPTER DEUTSCHLAND GmbH takes no responsibility for the correctness of this informationas far as the applicability to the receiving partys 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 ind ividual configurations / equipment

Chapter 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 shows

a 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 DEUTSCHLAND GMBH to receivefurther information.


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Technical Data

4.1.1 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.

4.1.1.1 Mission parameter

Figure 4.2: EMS Kit - Air Ambulance Technology STC

Flight rules: IFR Instrumentation: Glass Cockpit (MEGHAS)

Cat-A: Yes

JAR-OPS 3a Yes

a.The offered equipment package is derived from the conditions stated in JAR-OPS 3 Amendment 5. This package does notcover oxygen equipment and equipment required for over water operations. As the national operating rule may differ from theJAR-OPS 3 Amendment 5, the operator shall contact himself his national authority to assure that the planned equipment con-figuration is acceptable for the intended kind of operation.

Pilots 1 or 2

Medics 2

Patient 1

FWD


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Technical Data

Interior layout

Qty DocRef ComRef Title Weight

[kg]

Weight

[lb]

1 07-70044-A AAT-30100-002-2 EMS Kit - Air Ambulance Technology (AAT) 212.7 468.9

1 Oxygen Station 3x3,0 lt. 200 bar, front RH - AAT

1 Monitor & Defibrillator Corpuls C3 - GS

1 Suction Pump LCSU 3 - Laerdal

2 Infusion System Perfusor Space - Braun

1 Respirator Medumat Transport - Weinmann

3 Oxygen Cylinder 3,0 lt. Aluminium/Carbon - Luxfer

1 Blood Glucose Meter Omnitest Plus - Braun

1 Medical Floor (Universal) - AAT

1 Medical Seat slidable & swivelling, front RH - AAT

1 Medical Seat slidable, aft RH - AAT

1 Stretcher "Blue Mattress", LH - AAT

1 Medical Equipment Carrier, aft LH - AAT

1 Accessories - AAT

1 Retainer for Monitor & Defibrillator GS Corpuls C3 - AAT

1 Retainer for Monitor & Defibrillator GS Corpuls C3 (only monitor)- AAT

1 Retainer for Respirator Weinmann Medumat Transport - AAT

2 Retainer for Infusion System Braun Perfusor Space - AAT

1 Retainer for Suction Pump Laerdal LCSU 3 - AAT

1 Medical Cabinet with 3 drawer, front center - AAT

1 Rescue Bag with internal belt system - Tyromont

1 Vacuum Mattress - Tyromont

1 Emergency Backpack incl. DIN13232-N contents - Weinmann

1 Respiration Backpack incl. contents - Weinmann

1 Cervical Collar Set Perfit ACE & Mini Perfit ACE - Ambu

1 Installation, Certifcation & Documentation - AAT


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Technical Data

Interior layout

Avionics

1 06-21017-D L8512-001-20 External hoist 50m, detachable parts (incl. 1 week winch opera-tor training)

59.2 130.5


62.7 138.2

1 06-26011-C L8511-002-10 Cargo hook mirrors RH, fixed provisions 0.8 1.8

1 06-26011-C L8511-002-20 Cargo hook mirrors RH, detachable parts 3.9 8.6

1 06-27022-B L8511-005-10 Dual cargo hook system, fixed provisions 4.3 9.5

1 06-27022-B L8511-005-20 Dual cargo hook system, detachable parts 21.5 47.4

1 06-27027-A L8511-003-10 Cargo hook weighing system, fixed provisions 0.2 0.4

1 06-27027-A L8511-003-20 Cargo hook weighing system, detachable parts 1.5 3.3

1 06-31012-B L8531-001-00 External loudspeaker system with siren 11.2 24.7

1 06-42038-A L3347-010-00 4 additional landing lights 8.5 18.7

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

1 06-61015-B L3215-001-10 Emergency floats, fixed provisions 7.8 17.2

1 06-61015-B L3215-001-21 Emergency floats, detachable parts 64.6 142.4

1 06-65002-B L2566-001-00 Emergency hammer 0.2 0.4

a.Excludes L3217-001-00 Reinforced rear landing gear cross tube. Emergency floatation system for the medium height landinggear on request.

b.Requires L5213-001-11 Sliding door fastener, intermediate and max. position, LH or L5213-001-12 Sliding door fastener, max.position, LH.

Qty DocRef ComRef Title Weight[kg]

Weight[lb]

1 07-15016-B L2512-003-10 Height adjustable pilot seat instead of standard pilot seat 1.8 4.0

1 07-15016-B L2512-003-20 Height adjustable copilot seat instead of standard copilot seat 1.8 4.0

1 07-30012-B L2581-001-00 Enhanced sound proofing kit 4.8 10.6

1 07-50028-A L5213-001-11 Sliding door fastener, intermediate and max. position, LH 1.0 2.2

1 07-50028-A L5213-001-12 Sliding door fastener, max. position, LH 0.4 0.9

1 07-50028-A L5213-001-21 Sliding door fastener, intermediate and max. position, RH 1.0 2.2

1 07-50028-A L5213-001-22 Sliding door fastener, max. position, RH 0.4 0.9

1 07-50034-B L5212-001-00 Jettisonable cockpit doors 1.2 2.6

1 07-50036-B L2514-012-00 Covers for sliding door fairing LH/RH 0.1 0.2

1 07-50039-B L5211-010-00 Door catch system for cockpit doors 0.1 0.2

1 07-50039-B L5211-011-00 Door catch system for sliding doors 0.2 0.4

1 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 pro-visions

7.3 16.1

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

20.5 45.2

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

0.5 1.1

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

7.7 17.0


Weight[lb]


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Technical Data

Headsets and adapter cable

In any case EUROCOPTER DEUTSCHLAND GMBHadapter cables are required to connect any typeof headset or helmet to the aircraft intercom system. Furthermore EUROCOPTER DEUTSCHLANDGMBHprovides different headset types for customers choice.

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

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

1 08-16061-B L2341-006-63 Voice alert generation for DACS (NAT) 0.0 0.0

1 08-24015-C L3452-092-09 ADF control unit CDF-552 (Chelton Wulfsberg) 1.2 2.6

1 08-24015-C L3452-092-17 ADF receiver DF-431B (Chelton/Wulfsberg) 9.6 21.2

1 08-31019-B L2571-001-00 Radar radome for RDR 2000 2.0 4.4

1 08-31019-B L3443-090-02 Color weather radar RDR 2000 (Honeywell) 6.6 14.6

1 08-35007-D L2327-001-01 Traffic Advisory System TAS 620 (Avidyne) 9.5 20.9

1 08-35007-D L3442-881-00 TAS 620 (Avidyne) interface with GNS430 0.2 0.4

1 08-53004-B L3424-000-00 AHRS Free steering mode 0.5 1.1

1 08-81033-A L2321-013-00 M'ARMS Cockpit Voice and Flight Data Recorder (CVFDR),ground station not included

15.7 34.6

1 08-80003-A L2321-013-30 CVFDR read out kita GSE GSE

1 08-80004-A L2321-013-40 MFDAU tool kitb

GSE GSEa.Recommended 1 per customer if CVFDR is selected (PGS software included).b.Recommended 1 per fleet customer (> 3 H/C) if CVFDR is selected.


Weight[lb]

1 08-18018-C L2315-001-10 Headset H 10-76 (David Clark), low impedance 0.6 1.3

1 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 0.2

1 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 0.2

1 08-18061-A L2341-007-68 Headset Adapter cable pax GLENAIR/LEMO ANR 0.1 0.2

1 08-16063-A L2341-007-54 Fixed provisions for ANR 0.5 1.1


Weight[lb]


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Technical Data

Figure 4.3: Mission TOW versus range diagram

0 40 80 120 160 200 240 280 3

2300

2400

2500

2600

2700

2800

2900

PlannedTOW[

kg]

Range [nm]

Fuel Quantity 560 kg


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135.10.101.01 E Page 31 of 168


Technical Data

4.1.2.2 Basic Mission Configuration

4.1.2.2.1Mandato ry Items

Baseline aircraft

General equipment

Mission equipment

Interior layout


Weight[lb]

1 00-10002-A L0000-002-00 EC135 Baseline Aircraft 135.10.100.01 E 1,455.0 3,207.7

1 00-10002-A L0000-003-02 2 Pratt & Whitney PW206B2 turbine engines 0.0 0.0

00-10002-A L0000-003-01 2 Turbomeca ARRIUS 2B2 turbine engines 0.0 0.0

Subtotal: 1,455.0 3,207.7

1.5% Weigh t margin: 21.8 48.1

Subtotal (incl. margin): 1,476.8 3,255.8


Weight[lb]

1 05-03007-C L2562-001-00 First aid kit 1.5 3.3

1 05-22008-C L2621-001-00 Engine fire extinguishing system 3.6 7.9

1 05-30003-A L2565-002-00 Flashlight copilot side 0.2 0.4

1 05-33001-B L3113-001-00 Slant panel 0.8 1.8

1 05-33002-B L3113-004-00 Center console 2.2 4.9

1 05-34002-B L2576-001-00 Avionics compartment 4.2 9.3

1 05-37016-C L6701-001-00 Copilot flight controls 7.2 15.9

1 05-38010-B L3111-001-04 7" copilot instrument panel with glare shield 2.7 6.0

1 05-39006-B L2514-003-01 Map case in copilot door 0.5 1.1

1 05-39007-B L3111-001-10 Map cases on instrument panel glare shield 0.6 1.3

1 05-39008-B L3113-004-10 Illuminated chart holder for pilot side 1.0 2.2

1 05-41004-C L2104-003-00 Bleed air heating system: EMS-version 7.0 15.4

1 05-61010-B L2433-006-00 Battery, type "Saft", ULM, 40 Ah, 24 V instead of standardbattery

16.6 36.6

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

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

3.6 7.9


Weight[lb]

1 06-12008-C L3217-001-00 Reinforced rear landing gear cross tube 1.0 2.2

1 06-45023-B L3343-003-00 Landing & search light, 450 W 3.1 6.8

1 06-67044-B L2563-801-06 ELT C406-N HM (Artex) incl. NAV option 3.3 7.3


Weight[lb]

1 07-70047-A AEL-30100-005-2 EMS Kit - Aerolite (AEL) 216.2 476.61 Integral Floor, fix provisions - AEL

1 Integral Floor, detachable parts - AEL


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Technical Data

Mission equipment

Interior layout

Avionics


[kg]

Weight

[lb]

1 06-11021-B L3274-001-10 Settling protectors, fixed provisions 1.9 4.2

1 06-11021-B L3274-001-20 Settling protectors, detachable parts 7.9 17.4

1 06-65004-B L2625-003-00 2ndportable fire extinguisher 2.8 6.2

1 06-66009-B L3322-001-00 Boarding step illumination 0.2 0.4


Weight[lb]

1 07-30013-B L2524-002-00 Separation curtain for cockpit / cabin 2.1 4.6

1 07-40005-B L2513-200-00 Washable floor covering for cockpit 3.9 8.6

1 07-50025-C L5211-004-00 Securing device for complete opening of cockpit doors 0.8 1.8

1 07-50026-B L5231-001-00 One-hand latching system for clam-shell doors 1.0 2.2

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


Weight[lb]

1 08-12036-C L4322-090-04 Fixed provisions for tactical radio (antenna, power supply, ICSinterface)

3.0 6.6

1 08-16061-B L2341-193-40 Digital Audio Control System ACP53 (NAT), PAX 2.0 4.4

1 08-46040-A L3168-092-07 Digital moving map EURONAV IV+ - RN6 (EuroAvionics), inter-faced with FCDS 5.6 12.3

1 08-65004-B L3443-010-00 Video Radar Unit (VRU) 5.0 11.0

Subt otal: 49.2 108.5

3% Weight margin: 1.5 3.3

Subtotal (incl. margin): 50.7 111.7

Total: 1,941.3 4,279.7


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Technical Data

4.1.2.3 Further Available Equipment

General equipment

Mission equipment


Weight[lb]

1 05-12002-B L2551-003-00 Additional 4 tie-down fittings for airline attachment rails 0.6 1.3

1 05-21015-B L8541-001-10 Wire strike protection system, fixed provisions 3.3 7.3

1 05-21015-B L8541-001-20 Wire strike protection system, detachable parts 8.2 18.1

1 05-23006-B L7165-002-00 Engine compressor wash kit 3.2 7.1

1 05-25016-D L7161-001-10 Sand filter system, fixed provisions 11.3 24.9

1 05-25016-D L7161-001-20 Sand filter system, detachable parts 26.2 57.8

1 05-25023-B L7163-001-00 Inlet Barrier Filter Systema

a.Currently available with Pratt & Whitney engines. For Tubomeca engines on request.

27.0 59.5

1 05-26012-B L1241-001-00 Anti-corrosion protection 5.5 12.1

1 05-31025-C L5211-002-01 Ram air deflectors sliding doors 0.4 0.9

1 05-31026-C L5621-001-00 Tinted window for cockpit doors 0.0 0.0

1 05-31028-C L2524-030-10 IFR - training screen, fixed provisions 0.1 0.2

1 05-31028-C L2524-030-20 IFR - training screen, detachable parts 1.6 3.5

1 05-31045-A L5211-001-11 Lockable sliding window in copilots door 0.1 0.2

1 05-31045-A L5211-001-12 Lockable sliding window in pilots door 0.1 0.2

1 05-31098-A L5211-001-01 Ram air deflectors cockpit doors 0.6 1.3

1 05-31118-A L5611-002-00 Tinted front windshields 0.0 0.0

1 05-32007-B L3042-001-00 Windshield wiper system 5.0 11.0

1 05-34003-B L2576-002-00 Dampers for avionics compartment 1.8 4.0

1 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 2.0

1 05-42041-A L2105-005-00 Air conditioning systemb

b.L2122-005-00 Ventilation enhancement for cockpit already part of the air conditioning system.

55.0 121.3

1 05-44011-A L2122-005-00 Ventilation enhancement for cockpit 2.8 6.2

1 05-85008-C L2843-001-00 Fuel management system (Fuel flow meters) 1.2 2.6

1 05-92009-B L6611-001-10 Main rotor blade folding: basic kit 1.3 2.9

1 05-92009-B L6611-001-20 Main rotor blade folding: fixed provisions for ground handling kit 0.8 1.8

1 05-92009-B L6611-001-30 Main rotor blade folding: ground handling kit GSE GSE

1 05-93007-C L8544-002-00 Lashing points (wind speeds up to 100 kts) 0.7 1.5

1 05-93008-B L8544-001-00 Lashing points (wind speeds up to 40 kts) 2.4 5.3

1 05-95001-C L1321-001-00 Cover kit for helicopter GSE GSE

1 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 0.2

1 05-97002-C L6201-002-20 Optical tracker (Chadwick Helmuth), detachable parts 0.7 1.5


Weight[lb]

1 06-11022-C L3272-001-10 Snow skids, fixed provisions 0.9 2.0

1 06-11022-C L3272-001-20 Snow skids, detachable parts 21.9 48.3

1 06-12018-A L3214-001-00 Medium height landing gear (instead of standard landing gear)a 4.6 10.1

1 06-21017-D L8512-001-10 External hoist LH, fixed provisionsb 8.6 19.0


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Technical Data

Interior layout

Avionics


59.2 130.5


62.7 138.2

1 06-26011-C L8511-002-10 Cargo hook mirrors RH, fixed provisions 0.8 1.8

1 06-26011-C L8511-002-20 Cargo hook mirrors RH, detachable parts 3.9 8.6

1 06-27022-B L8511-005-10 Dual cargo hook system, fixed provisions 4.3 9.5

1 06-27022-B L8511-005-20 Dual cargo hook system, detachable parts 21.5 47.4



1 06-31012-B L8531-001-00 External loudspeaker system with siren 11.2 24.7







b.Requires L5213-001-11 Sliding door fastener, intermediate and max. position, LH or L5213-001-12 Sliding door fastener, max.position, LH.


Weight[lb]




1 07-50028-A L5213-001-11 Sliding door fastener, intermediate and max. position, LH 1.0 2.2

1 07-50028-A L5213-001-12 Sliding door fastener, max. position, LH 0.4 0.9

1 07-50028-A L5213-001-21 Sliding door fastener, intermediate and max. position, RH 1.0 2.2

1 07-50028-A L5213-001-22 Sliding door fastener, max. position, RH 0.4 0.9







Weight[lb]

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

7.3 16.1

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

20.5 45.2


0.5 1.1


7.7 17.0


Weight[lb]


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135.10.101.01 E Page 37 of 168


Technical Data






1 08-24015-C L3452-092-09 ADF control unit CDF-552 (Chelton Wulfsberg) 1.2 2.6

1 08-24015-C L3452-092-17 ADF receiver DF-431B (Chelton/Wulfsberg) 9.6 21.2

1 08-31019-B L2571-001-00 Radar radome for RDR 2000 2.0 4.4

1 08-31019-B L3443-090-02 Color weather radar RDR 2000 (Honeywell) 6.6 14.6





15.7 34.6


1 08-80004-A L2321-013-40 MFDAU tool kitb

GSE GSEa.Recommended 1 per customer if CVFDR is selected (PGS software included).b.Recommended 1 per fleet customer (> 3 H/C) if CVFDR is selected.


Weight[lb]


1 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


0.8 1.8


0.3 0.7


Weight[lb]




Weight[lb]


0.3 0.7


Weight[lb]





Weight[lb]


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Page 40 of 168 135.10.101.01 E

Technical Data


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Technical Data

Search and rescue

Intervention

4.2.1.2 Basic Mission Configuration

4.2.1.2.1Mandato ry Items

Baseline aircraft

General equipment

Pilots 1 or 2

Medics 2

Patient 1

Pilots 1 or 2

Pax 6FWD


Weight[lb]

1 00-10002-A L0000-002-00 EC135 Baseline Aircraft 135.10.100.01 E 1,455.0 3,207.7

1 00-10002-A L0000-003-02 2 Pratt & Whitney PW206B2 turbine engines 0.0 0.0

1 00-10002-A L0000-003-01 2 Turbomeca ARRIUS 2B2 turbine engines 0.0 0.0

Subtotal: 1,455.0 3,207.7

1.5% Weigh t margin: 21.8 48.1

Subtotal (incl. margin): 1,476.8 3,255.8


Weight[lb]

1 05-03007-C L2562-001-00 First aid kit 1.5 3.3

1 05-22008-C L2621-001-00 Engine fire extinguishing system 3.6 7.9

1 05-30003-A L2565-002-00 Flashlight copilot side 0.2 0.4

1 05-33001-B L3113-001-00 Slant panel 0.8 1.8

1 05-33002-B L3113-004-00 Center console 2.2 4.9

1 05-34002-B L2576-001-00 Avionics compartment 4.2 9.3

1 05-37016-C L6701-001-00 Copilot flight controls 7.2 15.91 05-38010-B L3111-001-04 7" copilot instrument panel with glare shield 2.7 6.0

1 05-39006-B L2514-003-01 Map case in copilot door 0.5 1.1


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Technical Data

Avionics

4.2.1.2.2Recommended Items

General equipment

Mission equipment


[kg]

Weight

[lb]

1 08-00434-A L2300-011-07 AV PACK DP IFR GC G430Wa

a.The system installation is not approved for WAAS navigation functions (e.g. LPV, LP, LNAV/VNAV and LNAV+V approaches)therefore such functions are deactivated. Starting mid 2010 and in the USA only, WAAS LPV approaches capability will beproposed by American Eurocopter as an STC.

75.3 166.0

1 Digital Audio Control System (NAT), incl. AMU50, ACP53 pilotand copilot

1 Transponder (Mode S) GTX330 (Garmin)

1 Distance Measuring Equipment DME 4000 (Rockwell-Collins)

1 Marker beacon receiver/lights KR 21 (Honeywell)

1 Avionics/Radio master switches (Special Eurocopter)

1 GPS/NAV/COM GNS 430Wa (Garmin), pilot, interfaced withFCDS

1 GPS/NAV/COM GNS 430Wa(Garmin), copilot, interfaced withFCDS

1 2 stand-by horizon AI 804 DC (Goodrich) with emergency bat-tery

1 MEGHAS - Flight Control Display System (FCDS) - Dual(4xSMD45)

1 AV PACK DP IFR GC G430 interconnection / wiring

1 08-21014-C L3441-090-04 Radar altimeter KRA 405 B (Honeywell) 3.5 7.7

1 08-53002-B L2212-400-00 MEGHAS sensor kit 17.0 37.5

1 08-54001-C L3411-001-00 Copilot pitot static system 1.5 3.3

1 08-72001-B L2212-001-00 Digital Automatic Flight Control System - DAFCS 27.0 59.5

Subtotal : 368.7 812.8

3% Weigh t margin: 11.1 24.4

Subtotal (incl. margin): 379.8 837.2


Weight[lb]

1 05-02016-D L1111-002-00 Enhanced exterior painting instead of standard painting 1.5 3.3

1 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 2.6

1 05-22014-A L5371-001-00 Engine outlet heat protection 1.2 2.6

1 05-31026-C L2514-002-00 Tinted sun shades for cockpit windshield roof section 1.9 4.2

1 05-36007-B L8532-002-30 Multifunction step LH (instead of std. boarding step) 4.9 10.8

1 05-71001-C L6351-002-00 Rotor brake system 3.6 7.9


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 17.4

1 06-24009-C L8534-002-11 External rope-down device for 2 persons, fixed provisions LH 4.1 9.0


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Technical Data

Mission equipment

Interior layout

Avionics


[kg]

Weight

[lb]



1 06-12018-A L3214-001-00 Medium height landing gear (instead of standard landing gear)a


4.6 10.1










Weight[lb]




1 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 2.2

1 07-50030-B L8512-003-00 Abrasion protection at sliding door 0.2 0.4







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


0.5 1.1


7.7 17.0




1 08-46040-A L3168-092-07 Digital moving map EURONAV IV+ - RN6 (EuroAvionics), inter-faced with FCDS

5.6 12.3


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135.10.101.01 E Page 49 of 168


Technical Data







15.7 34.6


1 08-80004-A L2321-013-40 MFDAU tool kitb GSE GSE

a.Recommended 1 per customer if CVFDR is selected (PGS software included).b.Recommended 1 per fleet customer (> 3 H/C) if CVFDRis selected.


Weight[lb]


1 08-18018-C L2315-001-11 Headset H 10-56 (David Clark), high impedance 0.6 1.3

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

0.8 1.8


0.8 1.8


0.3 0.7


Weight[lb]




Weight[lb]


0.3 0.7


Weight[lb]





Weight[lb]


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135.10.101.01 E Page 55 of 168


Technical Data

4.2.2 Disaster Management (Aerol ite)

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 quickly detachable for a fast mission configuration change.

4.2.2.1 Mission Parameter

Evacuation

Figure 4.11: Disaster Management Kit - Aerolite STC

Flight rules: IFR

Instrumentation: Glass Cockpit (MEGHAS)

Cat-A: Yes

JAR-OPS 3a Yes

a.The offered equipment package is derived from the conditions stated in JAR-OPS 3 Amendment 5. This package does notcover oxygen equipment and equipment required for over water operations. As the national operating rule may differ from theJAR-OPS 3 Amendment 5, the operator shall contact himself his national authority to assure that the planned equipment con-figuration is acceptable for the intended kind of operation.

Pilots 1 or 2

Medics 2

Patient 2


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135.10.101.01 E Page 57 of 168


Technical Data

Mission equipment

Interior layout

1 05-39007-B L3111-001-10 Map cases on instrument panel glare shield 0.6 1.3

1 05-39008-B L3113-004-10 Illuminated chart holder for pilot side 1.0 2.2

1 05-41004-C L2104-003-00 Bleed air heating system: EMS-version 7.0 15.4

1 05-61010-B L2433-006-00 Battery, type "Saft", ULM, 40 Ah, 24 V instead of standardbattery

16.6 36.6

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

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

3.6 7.9


Weight[lb]

1 06-12008-C L3217-001-00 Reinforced rear landing gear cross tube 1.0 2.2

1 06-45023-B L3343-003-00 Landing & search light, 450 W 3.1 6.8

1 06-67044-B L2563-801-06 ELT C406-N HM (Artex) incl. NAV option 3.3 7.3


Weight[lb]

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

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 07-70045-A AEL-30100-004-2 Disaster Management Kit - Aerolite (AEL) 101.2 223.1

1 Stretcher "Cirrus 1000" foldable, LH, fix provisions - AEL

1 Stretcher "Cirrus 1000" foldable, LH, detachable parts - AEL

1 Stretcher "Cirrus 1000" foldable, RH, fix provisions - AEL

1 Stretcher "Cirrus 1000" foldable, RH, detachable parts - AEL

1 Pax Seat stationary, front LH - AEL

1 Pax Seat stationary, front RH - AEL

1 Life Support Module, front center - AEL

1 Floor Frame for Pax Seats & Life Support Module - AEL1 Installation, Certification & Documentation - AEL

1 Oxygen Cylinder 3,0 lt. Aluminium/Carbon - Luxfer

1 Monitor & Defibrillator Argus Pro Life Care - Schiller

2 Infusion System Power Infuser - Zoll

1 Blood Glucose Meter Omnitest Plus - Braun

1 Respiration Backpack incl. contents - Weinmann

1 Emergency Backpack incl. DIN13232-N contents - Weinmann

2 Cervical Collar Set Perfit ACE & Mini Perfit ACE - Ambu


Weight[lb]


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Technical Data

Mission equipment

Interior layout

Avionics


[kg]

Weight

[lb]



1 06-12018-A L3214-001-00 Medium height landing gear (instead of standard landing gear)a


4.6 10.1










Weight[lb]




1 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 2.2

1 07-50030-B L8512-003-00 Abrasion protection at sliding door 0.2 0.4







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


0.5 1.1


7.7 17.0




1 08-46040-A L3168-092-07 Digital moving map EURONAV IV+ - RN6 (EuroAvionics), inter-faced with FCDS

5.6 12.3


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Technical Data







15.7 34.6


1 08-80004-A L2321-013-40 MFDAU tool kitb GSE GSE

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


Weight[lb]

1 08-18018-C L2315-001-10 Headset H 10-76 (David Clark), low

EC135 Technical data

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