EC 135 Technical data

EC 135Technical Data

135.02.101.01.E 1This document is the 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

Contents

Page

FOREWORD 3

GENERAL CHARACTERISTICS 5

EC 135 - STANDARD AIRCRAFT DEFINITION 9

OPTIONAL EQUIPMENT

• GENERAL OPTIONAL EQUIPMENT 15

• VIP OUTFITS 22

• EMS OUTFITS 26

RADIO COMMUNICATION / NAVIGATION EQUIPMENT

• SELECTION OF PINAO CODES 27

• PACKAGES DESCRIPTIONS 30

• HEADSETS AND HELMET 37

EQUIPMENT COMPATIBILITY 39

MAIN PERFORMANCE 45



Intentionally left blank



FOREWORD

PURPOSE OF DOCUMENT

This document gives a technical overview of the EC135 standard sales and its possible additionalequipment. The mandatory equipment for a Cat A or JAR OPS 3 certifications is already included inthe “PINAO” avionics packages. For any more in-depth technical information, please refer to theEC135 type specification (135.02.102.01 E)

PRIORITY

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.

IMPORTANT NOTES

■■■■ Eurocopter’s policy is one of on-going product enhancement which means thatalterations in definition, weights, dimensions or performance may be made at any timewithout notice being included in those documents that have already been issued.

■■■■ The data set forth in this document are general in nature and for informationpurposes only. They may vary with conditions. For performance data and operatinglimitations, reference must be made to the approved flight manual and all appropriatedocuments.



GENERAL CHARACTERISTICS

EXTERNAL DIMENSIONS



INTERNAL DIMENSIONS

Floor area VolumeCabin 3.15 m² 33.91 ft² Cabin 3.80 m³ 134.20 ft³Cockpit (pilot side) 1.15 m² 12.38 ft² Cockpit (pilot side) 1.00 m³ 35.31 ft³Baggage compartment 1.20 m² 12.92 ft² Baggage compartment 1.10 m³ 38.84 ft³

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



LAYOUT (Alternatives)

� Passenger transport: � 1 or 2 pilots + 6 or 5 passengers (standard version)� 1 or 2 pilots + 5 or 4 passengers (VIP advanced package-version)� 1 or 2 pilots + 7 or 6 passengers (option)

� Casualty evacuation: � 1 pilot + 1 litter + 3 seats for doctor and attendants(2nd litter in stowed position possible)

� 1 Pilot + 2 litters + 2 seats for doctor and attendant� 2 pilots + 1 litter + 3 seats for doctor and attendants

(2nd litter in stowed position possible)� 2 pilots + 2 litters + 2 seats for doctor and attendant

WEIGHTSkg lb.

� Empty weight, basic version, wet 1,490 3,285� Pilot 80 176� Useful load 1,265 2,789� Maximum take-off weight 2,835 6,250� Maximum take-off weight with external load 2,900 6,400

ENGINES

- 2 Pratt & Whitney turbine engines: new PW206B2 with 30 sec-rating.or

- 2 Turbomeca turbine engines: new ARRIUS 2B2 with 30 sec-rating.(for deliveries after Sept. 2002)

Engine ratings (thermodynamic limits per engine at SL, ISA):

PW206B2 kW ch shp• 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) 463 630 621• Maximum Continuous Power (MCP) 419 570 562

ARRIUS 2B2 kW ch shp• 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) 452 615 606• Maximum Continuous Power (MCP) 426 579 571



MAIN TRANSMISSION

Main transmission 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 353 1 x 480 1 x 473

Twin engine operation• Take-Off Power (TOP) 2 x 308 2 x 419 2 x 413• Maximum Continuous Power (MCP) 2 x 283 2 x 385 2 x 380

FUEL CAPACITIES

Usable Fuel Unusable Fuel Total

(lb) (kg) (l) (lb.) (kg) (lb.) (kg)

Main Tank 989.0 448.6 560.8 7.5 3.4 996.5 452.0

Supply Tank 193.6 87.8 109.8 9.3 4.2 202.8 92.0

Total 1,182.6 536.4 670.5 16.8 7.6 1,199.3 544.0

Note:• From the helicopter with S/N (Serial Number) 250 onwards, a new fuel tank version with 700 l

usable fuel (i.e. 560 kg / 1,235 lb.) is due to be available.• Fuel density used is 0.8 kg/litre.



EC 135 - STANDARD AIRCRAFT DEFINITION

GeneralCrashworthy fuselageTail boom with fixed horizontal stabiliser and two end-platesVertical fin with faired-in FenestronUpper deck with fittings for main gearbox, engines, hydraulic and cooling systemCowlings for main transmission and enginesSkid-type landing gear with skid protectors, capable of taking ground-handling wheelsLong boarding steps, LH and RHMaintenance built-in steps and gripsExterior painting (single colour)

Cockpit, Cabin and Cargo CompartmentOne-level cabin and cargo compartment floor with integrated railsGlazed canopyTwo hinged cockpit doors (with sliding window and map case in pilot's door)Two wide passenger sliding doorsTwo rear hinged clam-shell doorsLongitudinally adjustable crash resistant pilot and copilot seats with head rest and 4-point

safety belts with automatic locking systemFive upholstered crash resistant passenger seats with head rests and three-point safety

belts with automatic locking system (three seats facing aft and two seats facing forward)Cabin boarding grips (LH and RH)Interior panelling with integrated basic sound insulationFlight controls (pilot side)Engine controls with manual engine back-up system at pilot's collective pitch leverInstrument panel with extension on pilot's side and glare shieldRam-air and electrical ventilating system for cockpit and cabinHeadset holder in the cockpit, rotatableHeadset holder in the cabinPortable fire extinguisherStowage net for first aid kit at the LH rear clam-shell doorFlash light (torch)Mobile tie-down rings (4ea)



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 Management Display (VEMD) with indication of:* Torque* Engine parameters (N1-RPM, oil pressure, oil temperature, Turbine Outlet Temperature (TOT), engine/FADEC rep EEC failure and 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 temperature)* Dual ammeter (generator)* Ammeter (battery)* Dual voltmeter* Outside Air Temperature (OAT)* Parameters of optional equipment (e.g. mast moment)* Engine cycle counter (on flight report page)

• Clock (2”)• Magnetic compass• Triple (rotor and engines) RPM-indicator (2”)• Standard instruments: **

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

• Warning unit:- Engine fire warning with fuel emergency shut-off- Warning lights- Aural warning (for each warning, rotor RPM, fire 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.

** If “MEGHAS instrumentation” is chosen as optional equipment, these standardinstruments are deleted(function included in MEGHAS) and the following back-up instruments are added:- altimeter (2”)- airspeed indicator (2”)



Power Plant

Two PRATT & WHITNEY PW206B2 turbine enginesor

Two TURBOMECA ARRIUS 2B2 turbine engines (for deliveries after Sept. 2002)These 2 engines are equipped with:

- fire detectors- electronic engine control (FADEC-BOX)- chip detectors with quick-disconnect plugs- overspeed system- twin-engine OEI-training mode

Oil cooling and lubricating system with thermostatic valveCrashworthy fuel system with a flexible bladder-type fuel main tank and supply tank

(split into two sections)Automatically controlled variable rotor speed systemFuel tank filler flap, lockable

Transmission System

Flat-shaped main gearbox with two stagesChip detector system with quick-disconnect plug (main gearbox)Redundant oil cooling and lubrication systemMain gearbox attachment with Anti-Resonance Isolation System (ARIS)Free wheel assemblies in the engine input drivesTail rotor drive shaftTail rotor gearbox with splash lubrication and oil level sight gaugeChip detector system with quick-disconnect plug (tail rotor gearbox)

Rotor and Flight Controls

Bearingless Main Rotor system (BMR), consisting of:- Rotor head/mast in one piece- Four fibre-reinforced composite main rotor blades with anti-erosion strips, control cuff, elastomeric lead-lag dampers and special blade tip paintingMain rotor control system with dual hydraulic boost systemElectrical trim system (cyclic)Basic provisions for an easy integration of a track and balance systemFenestron-type tail rotor with ten metal blades (asymmetric blade spacing) and statorTail rotor gearbox coverTail rotor control system with flexball cable and single hydraulic boosterYaw-SAS (Stability Augmentation System)



Electrical Installation

Power generation system:- Two 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 busLighting:- 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- Lights in the cabin and cargo compartment

Ground Handling Kit *

Two ground-handling wheelsBasic aircraft covers (short time)Main rotor blade tie-down lash bagsOil drain hosesFuel tank drain deviceKeys for cockpit doors, cabin doors, baggage compartment doors and tank flap

(one-key system)Battery keyCompass compensation keyLifting points



Documentation

Flight Manual ♣Pilots-Checklist ♣LogbookBattery Manual *Maintenance Manual ♣ *- Part 1: System Descriptions- Part 2: Maintenance ProceduresIllustrated Parts Catalogue incl. type relevant Ground Support Equipment ♣ *Wiring Diagram Manual ♣ *List Of Applicable Publications (LOAP) ♣ *Service Bulletins Catalogue ♣ *Engine Documentation * including:- Maintenance Manual- Illustrated Parts Catalogue (IPC)- Service BulletinsAvionics Manual (if avionics equipment is installed by Eurocopter) *

* not included in the standard helicopter empty weight.♣ documents revision service is available.



OPTIONAL EQUIPMENT

General optional equipmentWeight

Free Selectable Optional Equipment kg lb.L2122-001-00 Ventilation extruder without copilot I-panel extension 1.5 3.3L2432-001-00 Starter/generator (2 x 200 A, 28 V DC), instead of standard

generator+ 3.6 + 7.9

L3113-001-00 Slant panel 0.7 1.5L5232-001-00 Multifunction handle on the main gear box cowling (LH and RH) 1.2 2.6

Cockpit, Cabin and Cargo Compartment EquipmentL1111-002-00 Two-colour external painting instead of single colour painting ≈ 1.5 ≈ 3.3L1111-004-00 Multicolour external painting instead of single colour painting ≈ 5.0 ≈ 11.0L2512-002-02 Reversed copilot seat installation kit (position change on ground) 0.9 2.0L2512-002-11 Manual lock for safety harness of pilot seat 0.1 0.2L2512-002-21 Manual lock for safety harness of copilot seat 0.1 0.2L2512-003-10 Height adjustable pilot seat instead of standard pilot seat + 3.9 + 8.6L2512-003-20 Height adjustable copilot seat instead of standard copilot seat + 3.9 + 8.6L2512-006-00 Winch operator seat, turnable in flight instead of standard copilot

seat (not usable for piloting)+ 14.5 + 31.9

L2513-004-40 Quick detachable VIP carpet for passenger cabin 3.0 6.6L2513-200-00 Washable floor covering for cockpit 4.1 9.1L2513-210-00 Washable floor covering for cargo compartment 2.9 6.4L2513-220-00 Washable floor covering for cockpit, cabin and cargo

compartment11.8 26.0

L2513-300-00 Carpet for cockpit and cabin floor 7.0 15.4L2513-310-00 Carpet for cockpit, cabin and cargo compartment floor 9.5 20.9L2514-002-00 Tinted sun shades for cockpit windshield roof section 1.9 4.2L2514-003-01 Map case in copilot door 0.5 1.1L2515-003-10 Stowage unit behind pilots’ seats, fixed provisions 0.1 0.2L2515-003-21 Stowage unit behind pilot’s seat, detachable parts 2.6 5.7L2515-003-22 Stowage unit behind copilot’s seat, detachable parts 4.6 10.1L2522-004-10 Utility seats for 3 rear passengers, model eurocopter, fixed

provisions1.2 2.6

L2522-004-20 Utility seats for 3 rear passengers, model eurocopter,detachable parts (in addition to standard seat arrangement)

+ 8.7 + 19.2

L2522-008-00 Utility seats for 3 rear passengers, model aerolite(in addition to standard seat arrangement)

+ 13.8 + 30.4



Weight

Cockpit, Cabin and Cargo Compartment Equipment (contd.) kg lb.L2524-001-00 Cabin / cargo compartment separation wall incl. smoke detector

(avionics compartment required)2.8 6.2

L2524-002-00 Cockpit / cabin separation curtain 4.0 8.8L2524-021-00 Cabin / cargo compartment separation curtain incl. smoke detector

(avionics compartment required)2.3 5.1

L2524-030-10 IFR - training screen, fixed provisions 0.1 0.2L2524-030-20 IFR - training screen, detachable parts 1.2 2.6L2525-102-81 Executive kit comprising:

• Map case in copilot door• Retractable coat hooks in the rear cabin ceiling (2ea)• Ashtrays in the cabin (if demanded)• Ashtrays in pilot’s and copilot’s door (if demanded)• Covers for sliding door fairing LH/RH• Variable tie-down web for luggage securing• Map cases on I-panel glare shield• Map case in sliding door LH/RH

4.8 10.6

L2562-001-00 First aid kit 1.3 2.9L2562-001-10 First aid kit for DGAC certification 3.0 6.6L2566-001-00 Emergency hammer 0.2 0.4L2576-001-00 Avionics compartment 6.2 13.7L2581-001-00 Enhanced sound proofing kit 9.8 21.6L2625-003-00 2nd portable fire extinguisher 2.3 5.1L3111-001-00 10" copilot instrument panel with glare shield 2.7 5.9L3111-001-01 11" copilot instrument panel with glare shield 3.8 8.4L3111-001-03 7“ copilot instrument panel with glare shield 2.5 5.5L3111-001-10 Map cases on instrument panel glare shield 0.6 1.3L3113-004-00 Centre console 2.1 4.6L3113-004-10 Illuminated chart holder for pilot side 0.9 2.0L3113-004-20 Illuminated chart holder for copilot side 1.1 2.4L5621-001-00 Tinted window in cockpit doors 0.0 0.0L5632-001-00 Tinted windows for passenger cabin 0.0 0.0L8514-001-00 Multipurpose attachment hardpoints integrated in the cabin 1.3 2.9

Heating and ventilation equipmentL2104-003-00 Bleed air heating system: EMS-version 6.6 14.6L2104-100-00 Bleed air heating system 6.2 13.7L2105-001-00 Air conditioning system 58.8 129.6L2105-001-10 Air conditioning system for tropical environment 61.6 135.8



Weight

Landing Gear and Associated Equipment kg lb.L3215-001-10 Emergency floats, fixed provisions + 8.8 + 19.4L3215-001-21 Emergency floats, detachable parts 49.6 109.3L3216-001-10 High landing gear instead of standard landing gear + 29.2 + 64.4L3217-001-10 Reinforced rear landing gear cross tube 1.1 2.4L3272-001-10 Snow skids, fixed provisions 0.1 0.2L3272-001-20 Snow skids, detachable parts 19.4 42.8L3273-001-00 Lengthened skids 8.3 18.3L3274-001-10 Settling protectors, fixed provisions 2.1 4.6L3274-001-20 Settling protectors, detachable parts 10.2 22.5

Landing and Search Lights incl. Illumination EquipmentL3322-001-00 Boarding step illumination 0.2 0.4L3343-003-00 Landing & search light, 450 W 3.4 7.5L3343-006-00 Landing & search light, 400/200 W, NVG compatible 4.3 9.5L3344-001-00 Strobe lights (white flash lights) 1.4 3.1L3346-100-10 Search light SX16, front installation, fixed provisions 7.9 17.4L3346-100-20 Search light SX16, front installation, detachable parts

(without vendor parts)4.8 10.6

L3346-300-10 Search light SX16, LH multi function step mounted, fixedprovisions

3.8 8.4

L3346-300-20 Search light SX16, LH multi function step mounted, detachableparts, (without vendor parts)

9.1 20.1

L3346-500-10 Search light SX16, vendor parts 20.4 45.0L3346-500-20 Search light SX16, with infrared filter, vendor parts 27.6 60.8L3353-005-00 Emergency lights (boarding step illumination and

illuminated exit signs)3.0 6.6

L3353-006-20 Illuminated signs "NO SMOKING/FASTEN SEAT BELT" 0.3 0.7L3353-007-00 Illuminated sign "SWITCH-OFF MOBILE PHONE" 0.2 0.4



Weight

General Mission Equipment kg lb.L2212-001-00 Digital Automatic Flight Control System (DAFCS) 38.5 84.9L2212-300-00 MEGHAS sensor kit, consisting of:

• AHRS (1st and 2nd system)• Air Data System (1st and 2nd system)• “Pelican” rack

22.1 48.7

L2217-001-10 VFR SAS (VFR pitch/roll Stability Augmentation System) 8.5 18.7L2217-001-50 IFR SAS (IFR pitch/roll Stability Augmentation System) 12.2 26.9L2420-002-00 AC (Alternating Current) system 3.2 7.1L2420-003-00 Dual AC (Alternating Current) system 4.3 9.5L2433-001-00 Battery, type “Varta”, 25 Ah, 24 V instead of standard battery + 8.0 + 17.6L2433-002-00 Battery, type "Saft", 26 Ah, 24 V instead of standard battery + 9.0 + 19.8L2433-005-00 Battery, type “Varta”, 40 Ah, 24 V instead of standard battery + 19.4 + 42.8L2551-003-00 Additional 4 tie-down fittings for airline attachment rails 0.6 1.3L2621-001-00 Engine fire extinguishing system 3.8 8.4L2812-001-00 Self sealing fuel supply tanks 4.2 9.3L2818-100-10 Internal long range fuel tank system, fixed provisions 3.2 7.1L2818-100-20 Internal long range fuel tank, detachable parts 30.3 66.8L3042-001-00 Windshield wiper system 4.9 10.8L3043-001-00 Windshield wiper system with windscreen washing device 8.8 19.4L3411-001-00 Copilot pitot static system (electrically heated) 1.3 2.6L5211-001-00 Sliding window in copilot door 0.1 0.2L5211-002-00 Sliding windows in sliding doors 0.2 0.4L5211-004-10 Securing device for complete opening of pilot door 0.8 1.8L5211-004-20 Securing device for complete opening of copilot door 0.8 1.8L5213-001-11 Sliding door fastener, intermediate and max. position, LH 1.0 2.2L5213-001-12 Sliding door fastener max. position, LH 0.4 0.9L5213-001-21 Sliding door fastener, intermediate and max. position, RH 1.1 2.4L5213-001-22 Sliding door fastener max. position, RH 0.4 0.9L5231-001-00 One-hand latching system for clam-shell doors 1.5 3.3L5231-002-00 Extended opening fasteners for clam-shell doors 0.2 0.4L5633-001-10 Window in clam-shell door, LH 0.6 1.3L5633-001-20 Window in clam-shell door, RH 0.6 1.3



Weight

General Mission Equipment (contd. 1) kg lb.L6201-001-30 Accelerometers (for track and balancing system) 0.0 0.0L6201-002-10 Optical tracker (Chadwick Helmuth), fixed provisions 0.1 0.2L6201-002-20 Optical tracker (Chadwick Helmuth), detachable parts 0.6 1.3L6344-001-00 Mast moment system 1.0 2.2L6351-001-00 Rotor brake system 4.8 10.6L6701-001-00 Copilot flight controls 7.1 15.7L6721-001-00 Covers for copilot flight controls 0.5 1.1L7161-001-00 Sand filter system 37.1 81.8L7165-002-00 Engine compressor washing device 1.8 4.0L7924-001-00 Fuzz burners for engines 1.0 2.2L8511-001-10 Cargo hook system, fixed provisions 2.9 6.4L8511-001-30 Cargo hook system, detachable parts 16.2 35.7L8511-002-10 Cargo hook mirrors, fixed provisions 0.7 1.5L8511-002-20 Cargo hook mirrors, detachable parts 4.2 9.3L8512-001-10 External hoist, fixed provisions 9.6 21.2L8512-001-20 External hoist, detachable parts, (incl. 1 week winch operator

training)62.8 138.5

L8521-301-00 Folding stretcher Ferno / aerolite-type, model 12-2/16G modified 14.0 30.9 L8521-301-20 Installation device for one stretcher type Ferno / aerolite-type

(model 12-2/16G modified) in full or half length7.0 15.4

L8521-431-10 Two attachment rails for universal apparatus in sliding door post 3.5 7.7L8521-432-10 Two airline attachment rails in LH passenger cabin ceiling 1.0 2.2L8522-320-00 Folding stretcher type Bucher-Leichtbau (16 G) 12.1 26.7L8522-350-00 Installation device for one stretcher type Bucher-Leichtbau (16 G)

in full only5.0 11.0

L8522-720-01 EMS stowage box 9.7 21.4L8531-001-00 External loudspeaker system with siren 11.0 24.3L8532-002-30 Multifunction step LH for standard landing gear

(instead of boarding step)+ 6.7 +14.8

L8532-002-40 Multifunction step RH for standard landing gear(instead of boarding step)

+ 3.7 + 8.2

L8541-001-10 Wire strike protection system, fixed provisions 3.3 7.3L8541-001-20 Wire strike protection system, detachable parts 8.2 18.1

Handling and Picketing EquipmentL1321-001-00 Tie-down and covering kit (long-term outside helicopter parking) GSE GSEL6611-001-10 Main rotor blade folding: basic kit 1.3 2.9L6611-001-20 Main rotor blade folding: fixed provisions for ground handling kit 0.7 1.5L6611-001-30 Main rotor blade folding: ground handling kit GSE GSEL8544-001-00 Lashing points (wind speeds up to 40 kts) 3.8 8.4L8544-002-00 Lashing points (wind speeds up to 100 kts)

(weight of GSE: 24.9 kg)0.7 1.5



The following listed items can be offered at customer’s request but are not necessarily kept on stock.Availability, certification status and compatibility with other equipment items must be checked individually.

Weight

Customer Request Equipment kg lb.L1111-005-00 Special detail paintings (markings, letters, logos) on requestL1111-006-00 Matching painting of externally installed optional equipment on requestL2321-007-00 M’ARMSTM Cockpit Voice and Flight Data Recorder (CVFDR),

JAR OPS III compliant17.3 38.1

L2321-009-00 M’ARMSTM Cockpit Voice and Flight Data Recorder (CVFDR) andUsage Monitoring System (UMS), JAR OPS III compliant(ground station not included)

18.3 40.4

L3171-001-00 M’ARMSTM Usage Monitoring System (UMS), JAR OPS IIIcompliant, (ground station not included)

5.3 11.7

L8503-001-10 Fire extinguishing bucket attachment (Bambi Bucket), fixedprovisions(cargo hook system required)

0.7 1.5

L8534-000-11 Rope-down device for 2 persons, fixed provisions LH 3.4 7.5L8534-000-12 Rope-down device for 2 persons, detachable parts LH1) 8.5 18.7L8534-000-21 Rope-down device for 2 persons, fixed provisions RH 3.4 7.5L8534-000-22 Rope-down device for 2 persons, detachable parts RH1) 8.5 18.7L8551-001-10 Light armour protection kit, cockpit and cabin, fixed provisions 1.0 2.2L8551-001-20 Light armour protection kit, cockpit and cabin, detachable parts 127.0 280.0

1) operation cannot be civil certified.

Broadcast, Thermal Imaging and TV Surveillance EquipmentSeveral systems are available on request.



Weight

NVG Compatible Equipment kg lb.

L2524-003-00 Cockpit / cabin separation curtain, NVG version 4.0 8.8

L3111-002-21 NVG painting for cabin and cargo compartment 0.2 0.4L3312-003-00 NVG compatible standard cockpit layout 0.2 0.4L3347-002-00 Additional NVG friendly external lighting kit, comprising position

and anti-collision lights0.4 0.9

L5213-003-00 Curtains for cabin windows (grey) 1.5 3.3

Note:For NVG compatible landing and searchlights, refer to § 5.1 Landing and search lights.

General remarks about NVG

If NVG flights are requested, three important factors must be considered:

• The switching-off of non-NVG compatible lights and instrumentation (crash risks).• The non-compliance with local civil regulations (NVG flights may be forbidden).• The different level of vision provided by NVG compatible lighting.

Requirements and checklist for building up a NVG compatible configuration

• General compatibility requirements

A NVG compatible cockpit is possible only with a MEGHAS avionics solution and only with filteredgoggles.

• Checklist for NVG compatible configuration

The following points must be checked and fulfilled:

� The cockpit must be fully NVG compatible, which means− The avionics solution must be NVG compatible,− The NVG compatible cockpit layout (option L3312-003-00) is required,− The customer must be advised about NVG compatibility status of its BFE (Buyer Furnished

Equipment).

� The cabin lighting must not negatively affect NVG compatibility, which means− The NVG compatible cockpit/cabin separation curtain (option L2524-003-00) is required.

Otherwise, the customer must be advised that all cabin lighting must be switched off duringNVG flights.

� The external lights must be fully NVG compatible, which means− The additional NVG compatible external lighting kit (option L3347-002-00) is required.

Otherwise, the customer must be advised that all non-NVG compatible lighting must beswitched off during NVG flights.

� If the customer lands in NVG mode, the NVG compatible landing & searchlight, 400/200 W(option L3343-006-00) is required.

� If the customer needs a NVG compatible SX16 searchlight, the SX16 with infrared filter (optionL3346-500-20) is required.



VIP Outfits

1. VIP Package 1 (Basic Package; 5 seat arrangement) L2526-100-01Weight of the complete package 1: + 54.3 kg / + 119.7 lb.

This installation offers corporate comfort and is characterised by:- Five passenger seats fitted with leather or combination of leather and fabric

(three rearward facing and two forward facing),- Cabinet with armrest (wood and leather finish), between the two rear passenger

seats- Pilot and copilot seats co-ordinated with passenger seats,- Cockpit, cabin and cargo compartment floors fitted with a VIP carpet,- Special colour of the interior outfit (painted).

Sold as complete package, only. To meet individual requirements a customerspecific VIP package can be created using the VIP table shown in paragraph 3.

2. VIP Package 2 (Advanced Package; 4 seat arrangement) L2526-200-00Weight of the complete package 2: + 69.3 kg / + 152.8 lb.

This installation offers first class comfort and is characterised by:- Four passenger seats upholstered with leather or combination of leather and fabric

(two rearward facing and two forward facing),- Cabinet (wood and leather finish), between the two front passenger seats,- Cabinet with armrest (wood and leather finish), between the two rear passenger seats,- Pilot and copilot seats co-ordinated with passenger seats,- Cockpit, cabin and cargo compartment floors fitted with a VIP carpet,- Cockpit and cabin panels and doors upholstered in leather.

Sold as complete package, only. To meet individual requirements a customerspecific VIP package can be created using the VIP table shown in paragraph 3.

Note:The VIP seats are installed and delivered instead of the standard seats. The given weights represent theweight difference compared to the standard aircraft.



3 Creation of a specific VIP packageOnly 1 Item per line can be selected. The VIP seats are installed and delivered instead of the standard seats. The givenweights represent the weight difference compared to the standard aircraft.

For information: the items included in package 1 are noticed with:

the items included in package 2 are noticed with:

COCKPIT VIP pilot seat(L2525-101-11)+1.2 kg / + 2.6 lb.

VIP pilot seatheight adjustable(L2525-101-71)+ 4.3 kg / + 9.5 lb.

VIP copilot seat(L2525-101-21)+1.2 kg / + 2.6 lb.

VIP copilot seatheight adjustable(L2525-101-76)+ 4.3 kg / + 9.5 lb.

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VIP carpet(L2525-101-50)5,7 kg / 12,6 lb.

FWD. PAX CABIN 2 VIP passenger seats,front(L2525-202-13)+ 7.7 kg / + 17 lb.

3 VIP passengerseats, front*(L2525-102-13)+ 8.9 kg / + 19.6 lb.

Front Cabinet, flat *(L2526-212-601)14,4 kg / 31,7 lb.

Front Cabinet,middle incl.2nd fire extinguisherfor cabin *(L2526-212-601 +L2526-112-63 +L2625-003-50)23,4 kg / 51,7 lb.

Front Cabinet, high incl.2nd fire extinguisher forcabin and illuminatedsigns *(L2526-212-601 +L2526-112-64 +L2625-003-50 +L3353-006-20)29,4 kg / 64,9 lb.

Table for front cabinet(L2526-112-61)3,0 kg / 6,6 lb.

Cooling box for frontcabinet(L2526-112-62)2,5 kg / 5,5 lb.Illumination system forfront cabinet, middle /high(L2526-112-10)2,0 kg / 6,6 lb.

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VIP-

seat

)

VIP carpet(L2525-102-50)5,6 kg / 12,3 lb.



REAR PAXCABIN

2 VIP seats, rear(L2525-102-23)+ 4.9 kg / + 10.8 lb.

Rear cabinet withArmrest(L2526-112-710)14,0 kg / 30,8 lb.

Rear cabinet, flat(L2526-312-701)12,5 kg / 27,5 lb.

Rear cabinet, high(L2526-312-701 +L2526-112-75)14,5 kg / 32,0 lb.

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Armrests in rearwindow niche, LH/RH(L2525-102-62)0,8 kg / 1,8 lb.

CARGOCOMPARTMENT

VIP carpet(L2525-103-10)5,1 kg / 11,2 lb.

GENERALINTERIOR

Special paintedinterior(L2525-100-35)1,5 kg / 3,3 lb.

Leather coveredinterior(L2525-112-35)16,1 kg / 35,5 lb.

Executive kit(L2525-102-81)5,4 kg / 11,9 lb.

Copilot controls covers(painted in harmonywith carpet)(L6721-001-00 +L2525-101-65)0,7 kg / 1,5 lb.

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Cabin entertainmentsystem(on request)

GROUNDSUPPORT

EQUIPMENT

Fabric protection coverfor 1 VIP pilot seat(L2525-111-50)

Fabric protection coverfor 1 VIP pax seat(L2525-112-91)

Plastic protection coverfor cockpit carpet(L2525-111-60)Plastic protection coverfor cabin carpet(L2525-112-92)

Note:The VIP seats are installed and delivered instead of the standard seats. The given weights represent the weight differencecompared to the standard aircraft.



HIGHLYRECOMMENDED

ITEMS

Air conditioning system(L2105-001-00)58,0 kg / 127,9 lb.

Air conditioning system for tropicalenvironment+ Special ducting for front passenger seats(L2105-001-10 + L2525-112-46)63,0 kg / 138,7 lb.

Enhanced soundproofing kit(L2581-001-00)9,8 kg / 21,6 lb.

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Pax / cargo compartmentseparation wall +Avionics compartment(L2524-001-00 +L2576-001-00)10,0 kg / 22,1 lb.

Note:The VIP seats are installed and delivered instead of the standard seats. The given weights represent the weight differencecompared to the standard aircraft.



EMS Outfits

For further information as well as description of the content of the different packages please refer tothe EC135 EMS-Brochure (135 EMS 02.101.01 E).

Weight 2)

kg lb.L8524-000-03 EMS Outfit Package I 83.0 183.0

--- Additional Suitable EMS Equipment and Apparatus for IndividualChoice

refer to EMS-Brochure

L8523-000-03 EMS Outfit Package II 150.0 331.0



L8522-000-03 EMS Outfit Package III 152.0 335.0



L8521-000-04 EMS Outfit Package IV 130.0 287.0



L8521-000-05 EMS Outfit Package V 132.0 291.0



2) for all EMS-packages the complete standard passenger seating weight (60.5 kg / 133.4 lb.) has to besubtracted.

Note: The EMS seats are installed and delivered instead of the standard seats.



RADIO COMMUNICATION / NAVIGATION EQUIPMENT

1. Selection of an avionics package function of operational needs (PINAO code)

A/ Asses your operational needs and corresponding PINAO code, with the help of thefollowing table

Pilot (single/dual) P one two one/two1 2 3

VFR/IFR I VFR IFR0 1

Day/night N day night0 1

Cat A A yes no1 0

JAR OPS 3 O yes no1 0

P I N A O

B/ With this code you will find the required avionics package in the following table.

One PINAO code may lead to different avionics solutions.

Key words and package weights are indicated in the following table to simplify theselection.

C/ A reference to the page corresponding to the chosen solution is also given for selectionof possible additional equipment.

NOTE- “VFR day” is included in all solutions.- NVG compatible MEGHAS versions can be offered on request.- Others requested additional equipment for JAR OPS 3 above 10,000 ft and over water are not covered by

the PINAO code.- For more details about the different avionics solutions (contents and layout) please refer to the brochure

“EC 135 AVIONICS Mission Packages” (135 AVIONICS 02.101.01 E).



COMPLETECODE

Based on solutionnumber

Key words Completeweight

(kg)

Completeweight(lbs)

seepage

10000 Solution 1 Basic conventional 29,8 65,8 2710001 Solution 1 Basic conventional 33,1 73,1 2710010 Solution 1 Basic conventional 46,6 103,0 2710011 Solution 1 Basic conventional 49,9 110,3 2710100 Solution 1 Basic conventional 29,8 65,8 2710101 Solution 1 Basic conventional 46,1 101,9 2710110 Solution 1 Basic conventional 46,6 103,0 2710111 Solution 1 Basic conventional 51,2 113,1 27

Solution 9 Glass cockpit, SPIFR 1st step 169,3 374,1 3211000Solution 10 Glass cockpit, SPIFR upper end, NMS capability 176,8 390,6 33Solution 9 Glass cockpit, SPIFR 1st step 172,6 381,4 3211001Solution 10 Glass cockpit, SPIFR upper end, NMS capability 180,1 397,9 33Solution 9 Glass cockpit, SPIFR 1st step 173,1 382,5 3211010Solution 10 Glass cockpit, SPIFR upper end, NMS capability 180,6 399,0 33Solution 9 Glass cockpit, SPIFR 1st step 176,4 389,7 3211011Solution 10 Glass cockpit, SPIFR upper end, NMS capability 183,9 406,3 33Solution 9 Glass cockpit, SPIFR 1st step 169,3 374,1 3211100Solution 10 Glass cockpit, SPIFR upper end, NMS capability 176,8 390,6 33Solution 9 Glass cockpit, SPIFR 1st step 172,6 381,4 3211101Solution 10 Glass cockpit, SPIFR upper end, NMS capability 180,1 397,9 33Solution 9 Glass cockpit, SPIFR 1st step 173,1 382,5 3211110Solution 10 Glass cockpit, SPIFR upper end, NMS capability 180,6 399,0 33Solution 9 Glass cockpit, SPIFR 1st step 176,4 389,7 3211111Solution 10 Glass cockpit, SPIFR upper end, NMS capability 183,9 406,3 33

20000 Solution 1 Basic conventional 47,9 105,8 2720001 Solution 1 Basic conventional 51,2 113,1 2720010 Solution 1 Basic conventional 64,7 143,0 2720011 Solution 1 Basic conventional 68,0 150,2 2720100 Solution 1 Basic conventional 47,9 105,8 2720101 Solution 1 Basic conventional 61,9 136,8 2720110 Solution 1 Basic conventional 64,7 143,0 2720111 Solution 1 Basic conventional 71,3 157,5 27

Solution 3 Conventional, few extensions possible 111,1 245,5 28Solution 4 Conventional, upper end 122,7 271,1 29Solution 7 Glass cockpit, 1st step 154,6 341,6 3021000Solution 8 Glass cockpit, upper end, NMS capability 162,2 358,4 31Solution 3 Conventional, few extensions possible 116,4 257,2 28Solution 4 Conventional, upper end 128,0 282,8 29Solution 7 Glass cockpit, 1st step 157,9 348,9 3021001Solution 8 Glass cockpit, upper end, NMS capability 165,5 365,7 31Solution 3 Conventional, few extensions possible 121,2 267,8 28Solution 4 Conventional, upper end 132,8 293,4 29Solution 7 Glass cockpit, 1st step 161,0 355,7 30

21010

Solution 8 Glass cockpit, upper end, NMS capability 168,6 372,5 31



COMPLETECODE

Based on Solutionnumber

Key words Completeweight

(kg)

Completeweight(lbs)

seepage

Solution 3 Conventional, few extensions possible 124,5 275,1 28Solution 4 Conventional, upper end 136,1 300,7 29Solution 7 Glass cockpit, 1st step 164,3 363,0 30

21011

Solution 8 Glass cockpit, upper end, NMS capability 171,9 379,8 31Solution 3 Conventional, few extensions possible 111,1 245,5 28Solution 4 Conventional, upper end 122,7 271,1 29Solution 7 Glass cockpit, 1st step 154,6 341,6 30

21100


21101


21110


21111

Solution 8 Glass cockpit, upper end, NMS capability 171,9 379,8 3130000 Solution 1 Basic conventional 47,9 105,8 2730001 Solution 1 Basic conventional 51,2 113,1 2730010 Solution 1 Basic conventional 61,5 135,9 2730011 Solution 1 Basic conventional 64,8 143,2 2730100 Solution 1 Basic conventional 47,9 105,8 2730101 Solution 1 Basic conventional 61,9 136,8 2730110 Solution 1 Basic conventional 64,7 143,0 2730111 Solution 1 Basic conventional 71,3 157,5 27

Solution 7 with AFCS Glass cockpit, 1st step 185,7 410,3 3031000 Solution 8 with AFCS Glass cockpit, upper end, NMS capability 193,3 427,1 31Solution 7 with AFCS Glass cockpit, 1st step 189,0 417,6 3031001 Solution 8 with AFCS Glass cockpit, upper end, NMS capability 196,6 434,4 31Solution 7 with AFCS Glass cockpit, 1st step 189,5 418,7 3031010 Solution 8 with AFCS Glass cockpit, upper end, NMS capability 197,1 435,5 31Solution 7 with AFCS Glass cockpit, 1st step 192,8 426,0 3031011 Solution 8 with AFCS Glass cockpit, upper end, NMS capability 200,4 442,8 31Solution 7 with AFCS Glass cockpit, 1st step 185,7 410,3 3031100 Solution 8 with AFCS Glass cockpit, upper end, NMS capability 193,3 427,1 31Solution 7 with AFCS Glass cockpit, 1st step 189,0 417,6 3031101 Solution 8 with AFCS Glass cockpit, upper end, NMS capability 196,6 434,4 31Solution 7 with AFCS Glass cockpit, 1st step 189,5 418,7 3031110 Solution 8 with AFCS Glass cockpit, upper end, NMS capability 197,1 435,5 31Solution 7 with AFCS Glass cockpit, 1st step 192,8 426,0 3031111 Solution 8 with AFCS Glass cockpit, upper end, NMS capability 200,4 442,8 31



2. Packages descriptions (NB: All packages with PINAO 30xxx are identical to those with PINAO 20xxx of this page)

PINAO code based on avionics solution 1Minimum required equipment

Wei

ght

(kg)

Wei

ght

(lbs)

1000

0

1000

1

1001

0

1001

1

1010

0

1010

1

1011

0

1011

1

2000

0

2000

1

2001

0

2001

1

2010

0

2010

1

2011

0

2011

1

Avionics solution 1 L2300-001-02 25,9 57,2 X X X X X X X X X X X X X X X

AC System L2420-002-00 3,2 7,1 X X X X X X X X X X X X X X X X

Slant panel L3113-001-00 0,7 1,5 X X X X X X X X X X X X X X X X

2” std-by horizon AI 804 DC with battery L3425-802-52 5,5 12,2 X X X X X X X X X X

Radar Altimeter KRA 405B / KNI 416 L3441-002-00 4,3 9,5 X X X X X X X X X

ELT C406-2 HM (ARTEX) 3 frequencies L2563-090-05 2,0 4,4 X X X X X X X X

Dual controls copilot L6701-001-00 7,1 15,7 X X X X X X X X

Copilot I-Panel extension 10" (*) L3111-001-00 3,0 6,6 X X X X X X X X

4" Artificial Horizon, 2nd Sys.GH 14 - 391 L3425-091-02 2,5 5,5 X X X X X X X X

RMI / CDI, KI 229 / KI 204 L3166-091-04L3167-091-02

3,0 6,6 X X X X X X X X

2nd indicators System packages 3"instruments:(UNITED INSTRUMENTS)

L3412-002-00 2,5 5,5 X X X X X X X

2nd directional Gyro (3” unslaved indic. 205 1BL L3421-091-02 2,0 4,4 X X

Copilot static system L3411-001-00 1,3 2,9 X X

Search & Landing light (450 W) L3343-003-00 3,2 7,1 X X X X X X X X X X

First aid kit L2562-001-00 1,3 2,6 X X X X X X X X

Engine fire extinguishing L2621-001-00 3,8 8,4 X X X X X X X X

(*) or enlarged version if combination of other optional equipment requires itPossible add-ons

2” std-by horizon AI 804 DC with battery L3425-802-52 6,4 14,1 X X X X X XRadar Altimeter KRA 405B / KNI 416 L3441-002-00 4,3 9,5 X X X X X X2” std-by altimeter (instead of Radar altimeter KRA405B / KNI 416)

L3111-100-00 0,7 1,5 X

2nd indicators System packages 2" instruments(instead of 3" indicator System)

L3412-003-00 1,6 3,5 X X X X X X X X

Comm. Control Sys. 2nd st AS 3100-XX (BECKER) ON REQUEST 1,6 3,5 X X X X X X X X X X X X X X X XComm. Control Syst.,3rd station AS 3100-XX(BECKER) (in passenger cabin)

ON REQUEST 2,9 6,4 X X X X X X X X X X X X X X X X

HF Com.syst. F 990/KFS 594 L2313-008-00 12,5 27,6 X X X X X X X X X X X X X X X X 4) 5)

Tactical FM Radio Teledux 9 (AEG) 2m or 4m ON REQUEST 5,0 11,0 X X X X X X X X X X X X X X X X 3) 4) 5) 14)Tactical FM Radio GM 900 (MOTOROLA) ON REQUEST 4,0 8,8 X X X X X X X X X X X X X X X X 3) 5) 14)

Tactical FM Radio MCS 2000 (MOTOROLA) ON REQUEST 3,5 7,7 X X X X X X X X X X X X X X X X 3) 5) 14)

Tactical FM Radio Tac / Com II (NAT) VHF-low,VHF-high, UHF

ON REQUEST TBC TBC X X X X X X X X X X X X X X X X 4) 5) 14)

VHF / UHF - AM / FM Transceiver ARC 210 ON REQUEST 10,0 22,1 X X X X X X X X X X X X X X X X 4) 5) 14)DME KN 63 / KDI 572 (HONEYWELL) L3455-092-03/

L3169-092-023,6 8,0 X X X X X X X X X X X X X X X X

Marker Beacon KR 21 (HONEYWELL) L3431-092-02 0,9 2,0 X X X X X X X X X X X X X X X XDirection Finder Chelton DF931 (stand alone) ON REQUEST 7,7 17,0 X X X X X X X X X X X X X X X X 9) 14)

Stand alone SAR DF 517 (BECKER) L2313-010-03 2,8 6,2 X X X X X X X X X X X X X X X X 9) 14)VHF NAV/COM/GPS with annunciation/switch2nd sys. GNS 430 (GARMIN)/ MD 41

L3442-092-00 7,8 17,2 X X X X X X X X X X X X X X X X

Stormscope WX 1000 + (GOODRICH) L3443-090-04 6,2 13,7 X X X X X X X X X X X X X X X X 9)Colour weather radar RDR2000 (HONEYWELL)(radome included)

L3443-090-02/L2571-001-00

14,0 30,9 X3)

X3)

X3)

X3)

X3)

X3)

X3)

X3)

X7)

X7)

X7)

X7)

X7)

X7)

X7)

X7)

8) 9)

Colour weather radar RDR2100 (HONEYWELL)(radome included)

L3443-090-06/L2571-001-00

14,0 30,9 X3)

X3)

X3)

X3)

X3)

X3)

X3)

X3)

X7)

X7)

X7)

X7)

X7)

X7)

X7)

X7)

8) 9)

Colour weather search radar ON REQUEST TBC TBC 9)Moving map DKG3 (Dornier, basic version) L3168-090-01 3,2 7,1 X X X X X X X X X X X X X X X X 14)Stand alone Moving Map System Euro Nav III(Euro Avionics):

L3168-092-03 10,0 22,1 X X X X X X X X X X X X X X X X 4) 5) 9)14)

ELT 100 HM (ARTEX) L2563-801-02 2,0 4,4 X or X or X or X or X or X or X or X orELT C406-2 HM (ARTEX) 3 frequencies L2563-090-05 2,1 4,6 X X X X X X X X

ELT C406-2 HM (ARTEX) 3 frequenc Nav. Option L2563-821-52 2,1 4,6 X or X or X or X or X or X or X or X or

ELT JE 290 (JOLLIET) L2563-808-01 2,1 4,6 X or X or X or X or X or X or X or X or

or) can be selected instead of the corresponding equipment installedwithin minimum PINAO package3) LH instrument panel extension has to be checked.4) Requirement of avionics compartment has to be checked5) Requirement of centre console has to be checked7) Copilot altimeter, airspeed indicator and vertical speed indicator requiredsize 2” instead of 3”.

8) Requires RVG 801 E for antenna stabilisation if no SAS is installed 9) Stand alone system; physical integration has to be checked 14) Tactical mission equipment can not be certified by German Civil Aviation Authorities.Eurocopter will ensure that the equipment is compatible with the basic helicopter and willassist the customer in obtaining certification or acceptance approval in his country.



PINAO code based onavionics solution 3Minimum requirement equipment

Wei

ght

(kg)

Wei

ght

(lbs)

2100

0

2100

1

2101

0

2101

1

2110

0

2110

1

2111

0

2111

1

Avionics solution 3 L2300-003-02 55,4 122,4 X X X X X X X XDual controls, copilot L6701-001-00 7,1 15,7 X X X X X X X X

Copilot I-panel extension 10“ (*) L3111-001-00 3,0 6,6 X X X X X X X X

Slant panel L3113-001-00 0,7 1,5 X X X X X X X X

Copilot static system L3411-001-00 1,3 2,9 X X X X X X X X

Bleed air heating (**) L2104-100-00 6,6 14,6 X X X X X X X X

Search & Landing light (450W) L3343-003-00 3,2 7,1 X X X X X X X X

Sliding window in copilot door L5211-001-00 0,1 0,2 X X X X X X X X

Windshield wiper L3042-001-00 4,9 10,8 X X X X X X X X

25 Ah battery (*) L2433-001-00 8,0 17,7 X X X X X X X X

200 A starter generators L2432-001-00 3,6 8,0 X X X X X X X X

Dual AC System L2420-003-00 6,3 13,9 X X X X X X X X

IFR pitch/roll SAS L2217-001-50 10,0 22,1 X X X X X X X

Map case on I-Panel glare shield L3111-001-10 0,4 0,9 X X X X X X X X

Map case in copilot door L2514-003-01 0,5 1,1 X X X X X X X X

Radar Altimeter KRA 405B / KNI 416 (HONEYWELL) L3441-002-00 4,3 9,5 X X X X

ELT C406-2 HM (ARTEX) 3 frequencies L2563-090-05 2,0 4,4 X X X X

2nd directional Gyro (3” unslaved indicator) 205 1BL(Goodrich)

L3421-091-02 2,0 4,4 X X X X X X

First aid kit L2562-001-00 1,3 2,9 X X X X

Engine fire extinguishing L2621-001-00 3,8 8,4 X X X X(*) or enlarged version if combination of other optional equipment requires it (**) Select L2104-003-00 instead for EMS helicopters

Possible add-onsRadar Altimeter KRA 405B / KNI 416 (HONEYWELL) L3441-002-00 4,3 9,5 X X X X

Exchange of KI206/KI229 to KPI552 HSI on copilot side ON REQUEST +1,0 +2,2 X X X X X X X X

Comm. Control Syst., 3rd station AS 3100-XX(BECKER) (in passenger cabin)

ON REQUEST 2,9 6,4 X X X X X X X X

HF Communication system KHF 990/KFS 594(HONEYWELL)

L2313-008-00 12,5 27,6 X X X X X X X X 4) 5)

Tactical FM Radio Teledux 9 (AEG) 2m or 4m ON REQUEST 5,0 11,0 X X X X X X X X 3) 4) 5) 14)

Tactical FM Radio GM 900 (MOTOROLA) ON REQUEST 4,0 8,8 X X X X X X X X 3) 5) 14)

Tactical FM Radio MCS 2000 (MOTOROLA) ON REQUEST 3,5 7,7 X X X X X X X X 3) 5) 14)


ON REQUEST TBC TBC X X X X X X X X 4) 5) 14)

VHF / UHF - AM / FM Transceiver ARC 210(Rockwell & Collins) Not civil certified

ON REQUEST 10,0 22,1 X X X X X X X X 4) 5) 14)

ADF / ADF Adapter (KR 87/KDA 692) ON REQUEST 4,7 10,4 X X X X X X X X 15)

Direction Finder Chelton DF931 stand alone ON REQUEST 7,7 17,0 X X X X X X X X 9) 14)

Stand alone SAR DF 517 (BECKER) L2313-010-03 2,8 6,2 X X X X X X X 9) 14)

Stormscope WX 1000 + (GOODRICH) L3443-090-04 6,2 13,7 X X X X X X X 9)

Moving Map Kneeboard DKG 3 (Dornier, basic version) L3168-090-01 3,2 7,1 X X X X X X X X 14)

Stand alone Moving Map System Euro Nav III(Euro Avionics)

L3168-092-03 10,0 22,1 X X X X X X X X 4) 5) 9) 14)

ELT 100 HM (ARTEX) L2563-801-02 2,0 4,4 X or X or X or X or


ELT C406-2 HM (ARTEX) 3 freque Nav. Option L2563-821-52 2,1 4,6 X or X or X or X or

ELT JE 290 (JOLLIET) L2563-808-01 2,1 4,6 X or X or X or X or

or) can be selected instead of the corresponding equipmentinstalled within minimum PINAO package 3) BFE required 4) Requirement of avionics compartment has to be checked 5) Requirement of centre console has to be checked 9) Stand alone system; physical integration has to be checked

14) Tactical mission equipment can not be certified by German Civil AviationAuthorities. Eurocopter will ensure that the equipment is compatible with the basichelicopter and will assist the customer in obtaining certification or acceptanceapproval in his country. 15) should be checked with customer airport landing requirements



PINAO code based onavionics solution 4

Minimum requirement equipment

Wei

ght (

kg)

Wei

ght (

lbs)

2100

0

2100

1

2101

0

2101

1

2110

0

2110

1

2111

0

2111

1

Avionics solution 4 L2300-004-02 60,8 134,3 X X X X X X X XDual controls copilot L6701-001-00 7,1 15,7 X X X X X X X XCopilot I-Panel extension 10" (*) L3111-001-00 3,0 6,6 X X X X X X X XAvionics compartment L2576-001-00 6,2 13,7 X X X X X X X XSlant panel L3113-001-00 0,7 1,5 X X X X X X X XCopilot static system L3411-001-00 1,3 2,9 X X X X X X X XBleed air heating (**) L2104-100-00 6,6 14,6 X X X X X X X XSearch & Landing light (450W) L3343-003-00 3,2 7,1 X X X X X X X XCopilot door sliding window L5211-001-00 0,1 0,2 X X X X X X X XWindshield wiper L3042-001-00 4,9 10,8 X X X X X X X X25 Ah battery (*) L2433-001-00 8,0 17,7 X X X X X X X X200 A starter generators L2432-001-00 3,6 8,0 X X X X X X X XDual AC System L2420-003-00 6,3 13,9 X X X X X X X XIFR pitch/roll SAS L2217-001-50 10,0 22,1 X X X X X X X XMap case on I-Panel glare shield L3111-001-10 0,4 0,9 X X X X X X X XMap case in copilot door L2514-003-01 0,5 1,1 X X X X X X X XRadar Altimeter KRA 405B / KNI 416 L3441-002-00 4,3 9,5 X X X XELT C406-2 HM (ARTEX) 3 frequencies L2563-090-05 2,0 4,4 X X X X2nd directional Gyro (3” unslaved indicator) 205 1BL(BFGoodrich)

L3421-091-02 2,0 4,4 X X X X X X

First aid kit L2562-001-00 1,3 2,6 X X X XEngine fire extinguishing L2621-001-00 3,8 8,4 X X X X(*) or enlarged version if combination of other optional equipment requires it (**) Select L2104-003-00 instead for EMS helicopters

Possible add-onsRadar Altimeter KRA 405B / KNI 416 L3441-002-00 4,3 9,5 X X X XComm. Control Syst.,3rd stationAS 3100-XX (BECKER) (in cabin)


HF Communication system KHF 990/KFS 594 L2313-008-00 12,5 27,6 X X X X X X X X 4) 5)

Tactical FM Radio Teledux 9 (AEG) 2m or 4m ON REQUEST 5,0 11,0 X X X X X X X X 3) 4) 5) 14)

Tactical FM Radio GM 900 (MOTOROLA) ON REQUEST 4,0 8,8 X X X X X X X X 3) 5) 14)

Tactical FM Radio MCS 2000 (MOTOROLA) ON REQUEST 3,5 7,7 X X X X X X X X 3) 5) 14)


ON REQUEST TBC TBC X X X X X X X X 4) 5) 14)


ON REQUEST 10,0 22,1 X X X X X X X X 4) 5) 14)

ADF KDF 806 (incl. KFS 586A) L3452-092-03 5,8 12,8 X X X X X X X X 15)

Direction Finder Chelton DF931 (stand alone) ON REQUEST 7,7 17,0 9) 14)

Stand alone SAR DF 517 (BECKER) L2313-010-03 2,8 6,2 X X X X X X X X 9) 14)

GPS Course Deviatio Ind. 802100 (ETS / DAC) L3167-092-02 0,4 0,9 X X X X X X X

GPS indication on HSI KPI 552 pilot ON REQUEST 2,9 6,4 X X X X X X X X TRIMBLE required

GPS Nav Syst. 2101 Approach plus (TRIMBLE) L3442-092-14 2,3 5,1 X X X X X X X X

Stormscope WX 1000 + (GOODRICH) L3443-090-04 6,2 13,7 X X X X X X X X 9)


L3443-090-02/L2571-001-00

14,0 30,9 X X X X X X X X 9) In console


L3443-090-06/L2571-001-00

14,0 30,9 X X X X X X X X 9) In console

Colour weather search radar ON REQUEST TBC TBC TBC 9) In console

Moving Map DKG 3 (Dornier, basic version) L3168-090-01 3,2 7,1 X X X X X X X X 11) 14)

Stand alone Moving Map Euro Nav III (Euro Avionics): L3168-092-03 10,0 22,1 X X X X X X X X 4) 5) 9) 14)

ELT 100 HM (ARTEX) L2563-801-02 2,0 4,4 X or X or X or X or


ELT C406-2 HM (ARTEX) 3 frequencies Nav. Option L2563-821-52 2,1 4,6 X or X or X or X or 13)

ELT JE 290 (JOLLIET) L2563-808-01 2,1 4,6 X or X or X or X or

or) can be selected instead of the corresponding equipment installed withinminimum PINAO package 3) BFE required 4) Requirement of avionics compartment has to be checked5) Requirement of centre console has to be checked 9) Stand alone system; physical integration has to be checked

11) GPS required 13) ARINC 429 GPS required 14) Tactical mission equipment can not be certified by German Civil AviationAuthorities. Eurocopter will ensure that the equipment is compatible with thebasic helicopter and will assist the customer in obtaining certification oracceptance approval in his country. 15) should be checked with customer airport landing requirements



PINAO code based on avionics solution 7


Wei

ght

(kg)

Wei

ght

(lbs)

2100

0

2100

1

2101

0

2101

1

2110

0

2110

1

2111

0

2111

1

3100

0

3100

1

3101

0

3101

1

3110

0

3110

1

3111

0

3111

1

Avionics solution 7 L2300-007-02 66,8 147,6 X X X X X X X X X X X X X X X XDual controls copilot L6701-001-00 7,1 15,7 X X X X X X X X X X X X X X X XCopilot I-Panel extension 7" L3111-001-03 2,7 6,0 X X X X X X X X X X X X X X X XAvionics compartment L2576-001-00 6,2 13,7 X X X X X X X X X X X X X X X XSlant panel L3113-001-00 0,7 1,5 X X X X X X X X X X X X X X X XCentre console L3113-004-00 2,1 1,5 X X X X X X X X X X X X X X X XCopilot static system L3411-001-00 1,3 2,9 X X X X X X X X X X X X X X X XBleed air heating (**) L2104-100-00 6,6 14,6 X X X X X X X X X X X X X X X XSearch & Landing light (450W) L3343-003-00 3,2 7,1 X X X X X X X X X X X X X X X XCopilot door sliding window L5211-001-00 0,1 0,2 X X X X X X X X X X X X X X X XWindshield wiper L3042-001-00 4,9 10,8 X X X X X X X X X X X X X X X X40 Ah battery L2433-005-00 19,4 42,8 X X X X X X X X X X X X X X X X200 A starter generator L2432-001-00 3,6 8,0 X X X X X X X X X X X X X X X XAC System L2420-002-00 3,2 7,1 X X X X X X X X X X X X X X X XMap case on I-Panel glare shield L3111-001-10 0,4 0,9 X X X X X X X X X X X X X X X XMap case in copilot door L2514-003-01 0,5 1,1 X X X X X X X X X X X X X X X XMEGHAS sensor kit L2212-300-00 15,9 35,1 X X X X X X X X X X X X X X X XRadar Altimeter KRA 405B L3441-090-04 3,2 7,1 X X X X X X X X X X X XELT C406-2 HM (ARTEX) 3 frequency L2563-090-05 2,0 4,4 X X X X X X X XIFR pitch/roll SAS L2217-001-50 10,0 22,1 X X X X X X X XDigital AFCS (DAFCS) L2212-001-00 38,5 85,1 X X X X X X X XFirst aid kit L2562-001-00 1,3 2,6 X X X X X X X XEngine fire extinguishing L2621-001-00 3,8 8,4 X X X X X X X X(**) Select L2104-003-00 instead for EMS helicopters

Possible add-onsRadar Altimeter KRA 405B (HONEYWELL) L3441-090-04 3,2 7,1 X X X XRadar Altimeter AHV16 (THALES) L3441-090-06 4,0 8,8 X X or or X X or or or or or or or or or orExchange of 2 SMD45 screens to oneSMD68 on copilot side

ON REQUEST +1,1 +2,4 X X X X X X X X X X X X X X X X

Digital AFCS (DAFCS) L2212-001-00 38,5 85,1 instead of pitch/roll SAS(Rad. Alt. required)

Comm. Control Syst.,3rd stationAS 3100-XX (BECKER) (in cabin)

ON REQUEST 2,9 6,4 X X X X X X X X X X X X X X X

HF Communication system KHF 990/KFS594 (HONEYWELL)

L2313-008-00 12,5 27,6 X X X X X X X X X X X X X X X X

Tactical FM Radio Teledux 9 (AEG) 2m or4m BFE required

ON REQUEST 5,0 11,0 X X X X X X X X X X X X X X X X 14)

Tactical FM Radio GM 900 (MOTOROLA)BFE required


Tactical FM Radio MCS 2000 (MOTOROLA)BFE required


Tactical FM Radio Tac / Com II (NAT) VHF-low, VHF-high, UHF

ON REQUEST TBC TBC X X X X X X X X X X X X X X X 14)

VHF / UHF - AM / FM Transceiver ARC 210(Rockwell & Collins


Automatic Direction Finder DFS 43 L3452-092-05 7,0 15,5 X X X X X X X X X X X X X X X X 15)DF Chelton DF931(stand alone) ON REQUEST 7,7 17,0 X X X X X X X X X X X X X X X X 9) 14)Stand alone SAR DF517 (BECKER) L2313-010-03 2,8 6,2 X X X X X X X X X X X X X X X X 9) 14)GPS Nav System 2101 I/O Approach + L3442-092-12 2,3 5,1 X X X X X X X X X X X X X X X XStormscope WX 1000 429E (GOODRICH) L3443-090-07 6,2 13,7 X X X X X X X X X X X X X X X X 9)Colour weather radar RDR2000(HONEYWELL) (radome included)

L3443-090-02/L2571-001-00

10,0 22,1 X X X X X X X X X X X X X X X 10)

Colour weather search radar ON REQUEST TBC TBC X X X X X X X X X X X X X X X X 10)Moving Map DKG 3 (Dornier, basic version) L3168-090-01 3,2 7,1 X X X X X X X X X X X X X X X X 11) 14)Moving Map System DKG 4 (Dornier) Mapgenerator control unit + options

L2444-002-10 3,4 7,5 X X X X X X X X X X X X X X X X 10) 11)14)

Moving Map system Euro Nav III L3168-090-08 9,0 19,9 X X X X X X X X X X X X X X X X 10) 11) 14)ELT 100 HM (ARTEX) L2563-801-02 2,0 4,4 X or X or X or X or X or X or X or X orELT C406-2 HM (ARTEX) 3 frequencies L2563-090-05 2,1 4,6 X X X X X X X XELT C406-2 HM (ARTEX) 3 freq Nav. Option L2563-821-52 2,1 4,6 X or X or X or X or X or X or X or X or 13)ELT JE 290 (JOLLIET) L2563-808-01 2,1 4,6 X or X or X or X or X or X or X or X or or) can be selected instead of the corresponding equipmentinstalled within minimum PINAO package 9) Stand alone system; physical integration has to be checked 10) VRU (3ET) required 11) GPS required

13) ARINC 429 GPS required 14) Tactical mission equipment can not be certified by German CivilAviation Authorities. Eurocopter will ensure that the equipment iscompatible with the basic helicopter and will assist the customer inobtaining certification or acceptance approval in his country. 15) should be checked with customer airport landing requirements



PINAO code based on avionics solution 8

Minimum requirement equipment Wei

ght

(kg)

Wei

ght

(lbs)

2100

0

2100

1

2101

0

2101

1

2110

0

2110

1

2111

0

2111

1

3100

0

3100

1

3101

0

3101

1

3110

0

3110

1

3111

0

3111

1

Avionics solution 8 L2300-008-02 74,4 164,3 X X X X X X X X X X X X X X X XDual controls copilot L6701-001-00 7,1 15,7 X X X X X X X X X X X X X X X XCopilot I-Panel extension 7" L3111-001-03 2,7 6,0 X X X X X X X X X X X X X X X XAvionics compartment L2576-001-00 6,2 13,7 X X X X X X X X X X X X X X X XSlant panel L3113-001-00 0,7 1,5 X X X X X X X X X X X X X X X XCentre console L3113-004-00 2,1 1,5 X X X X X X X X X X X X X X X XCopilot static system L3411-001-00 1,3 2,9 X X X X X X X X X X X X X X X XBleed air heating (**) L2104-100-00 6,6 14,6 X X X X X X X X X X X X X X X XSearch & Landing light (450W) L3343-003-00 3,2 7,1 X X X X X X X X X X X X X X X XCopilot door sliding window L5211-001-00 0,1 0,2 X X X X X X X X X X X X X X X XWindshield wiper L3042-001-00 4,9 10,8 X X X X X X X X X X X X X X X X40 Ah battery L2433-005-00 19,4 42,8 X X X X X X X X X X X X X X X X200 A starter generators L2432-001-00 3,6 8,0 X X X X X X X X X X X X X X X XAC System L2420-002-00 3,2 7,1 X X X X X X X X X X X X X X X XMap case on I-Panel glare shield L3111-001-10 0,4 0,9 X X X X X X X X X X X X X X X XMap case in copilot door L2514-003-01 0,5 1,1 X X X X X X X X X X X X X X X XMEGHAS sensor kit L2212-300-00 15,9 35,1 X X X X X X X X X X X X X X X XRadar Altimeter KRA 405B (HONEYWELL) L3441-090-04 3,2 7,1 X X X X X X X X X X X XELT C406-2 HM (ARTEX) 3 frequencies L2563-090-05 2,0 4,4 X X X X X X X XIFR pitch/roll SAS L2217-001-50 10,0 22,1 X X X X X X X XDigital AFCS (DAFCS) L2212-001-00 38,5 85,1 X X X X X X X XFirst aid kit L2562-001-00 1,3 2,6 X X X X X X X XEngine fire extinguishing L2621-001-00 3,8 8,4 X X X X X X X X(**) Select L2104-003-00 instead for EMS helicopters

Possible add-onsRadar Altimeter KRA 405B (HONEYWELL) L3441-090-04 3,2 7,1 X X X XRadar Altimeter AHV16 (THALES) L3441-090-06 4,0 8,8 X X or or X X or or or or or or or or or orDigital AFCS (DAFCS) L2212-001-00 38,5 85,1 instead of pitch/roll SAS

(Rad. Alt. required)Exchange of 2 SMD45 screens to one SMD68 oncopilot side

ON REQUEST +1,1 +2,4 X X X X X X X X X X X X X X X X

Comm. Control Syst.,3rd station AS 3100-XX(BECKER) (in passenger cabin)

ON REQUEST 2,9 6,4 X X X X X X X X X X X X X X X X

HF Communication system KHF 990/KFS 594 L2313-008-00 12,5 27,6 X X X X X X X X X X X X X X X XTactical FM Radio Teledux 9 (AEG) 2m or 4m ON REQUEST 5,0 11,0 X X X X X X X X X X X X X X X X 3) 14)Tactical FM Radio GM 900 (MOTOROLA) ON REQUEST 4,0 8,8 X X X X X X X X X X X X X X X X 3) 14)Tactical FM Radio MCS 2000 (MOTOROLA) ON REQUEST 3,5 7,7 X X X X X X X X X X X X X X X 3) 14)Tactical FM Radio Tac / Com II (NAT) VHF-low,VHF-high, UHF

ON REQUEST TBC TBC X X X X X X X X X X X X X X X X 14)



Automatic Direction Finder DFS 43 (incl. CD 432B) L3452-092-05 7,0 15,5 X X X X X X X X X X X X X X X X 15)Direction Finder Chelton DF931 stand alone ON REQUEST 7,7 17,0 X X X X X X X X X X X X X X X X 9) 14)Stand alone SAR DF (BECKER) L2313-010-03 2,8 6,2 X X X X X X X X X X X X X X X X 9) 14)

FMS/Radio management with GPS CanadianMarconi (CMA3000 + CMA 3012)

ONREQUEST 9,3 20,5

X X X X X X X X X X X X X X X X

GPS Nav System 2101 I/O Approach + (TRIMBLE) L3442-092-12 2,1 4,6 X X X X X X X X X X X X X X X XStormscope WX 1000 429E (GOODRICH) L3443-090-07 6,2 13,7 X X X X X X X X X X X X X X X 9)Colour weather radar RDR2000 (HONEYWELL)(radome included)

L3443-090-02/L2571-001-00

10,0 22,1 X X X X X X X X X X X X X X X X 10)

Colour weather search radar ON REQUEST TBC TBC X X X X X X X X X X X X X X X X 10)Moving Map DKG 3 (Dornier, basic version) L3168-090-01 3,2 7,1 X X X X X X X X X X X X X X X X 11) 14)

Moving Map System DKG 4 (Dornier) Mapgenerator control unit + options

L2444-002-10 3,4 7,5 X X X X X X X X X X X X X X X X 10) 11) 14)

Moving Map System Euro Nav III L3168-090-08 9,0 19,9 X X X X X X X X X X X X X X X X 10) 11) 14)ELT 100 HM (ARTEX) L2563-801-02 2,0 4,4 X or X or X or X or X or X or X or X or

ELT C406-2 HM (ARTEX) 3 frequencies L2563-090-05 2,1 4,6 X X X X X X X X

ELT C406-2 HM (ARTEX) 3 freque Nav. Option L2563-821-52 2,1 4,6 X or X or X or X or X or X or X or X or 13)

ELT JE 290 (JOLLIET) L2563-808-01 2,1 4,6 X or X or X or X or X or X or X or X or or) can be selected instead of the correspondingequipment installed within minimum PINAO package 3) BFE required 9) Stand alone system; physical integration has to bechecked 10) VRU (3ET) required 11) GPS required

13) ARINC 429 GPS required 14) Tactical mission equipment can not be certified by German Civil AviationAuthorities. Eurocopter will ensure that the equipment is compatible with thebasic helicopter and will assist the customer in obtaining certification oracceptance approval in his country. 15) should be checked with customer airport landing requirements



PINAO code based onavionics solution 9Minimum requirement equipment

Wei

ght (

kg)

Wei

ght (

lbs)

1100

011

001

1101

011

011

1110

011

101

1111

011

111

Avionics solution 9 L2300-009-02 63,4 140,1 X X X X X X X XAvionics compartment L2576-001-00 6,2 13,7 X X X X X X X XSlant panel L3113-001-00 0,7 1,5 X X X X X X X XCentre console L3113-004-00 2,1 1,5 X X X X X X X XCopilot static system L3411-001-00 1,3 2,9 X X X X X X X XBleed air heating (**) L2104-100-00 6,6 14,6 X X X X X X X XSearch & Landing light (450W) L3343-003-00 3,2 7,1 X X X X X X X XWindshield wiper L3042-001-00 4,9 10,8 X X X X X X X X40 Ah battery L2433-005-00 19,4 42,8 X X X X X X X X200 A starter generators L2432-001-00 3,6 8,0 X X X X X X X XAC System L2420-002-00 3,2 7,1 X X X X X X X XMap case on I-Panel glare shield L3111-001-10 0,4 0,9 X X X X X X X XMEGHAS sensor kit L2212-300-00 15,9 35,1 X X X X X X X XDigital AFCS (DAFCS) L2212-001-00 38,5 85,1 X X X X X X X XELT C406-2 HM (ARTEX) 3 frequencies L2563-090-05 2,0 4,4 X X X XFirst aid kit L2562-001-00 1,3 2,6 X X X XEngine fire extinguishing L2621-001-00 3,8 8,4 X X X X

(**) Select L2104-003-00 instead for EMS helicopters

Possible add-onsRadar Altimeter AHV16 (THALES) L3441-090-06 4,0 8,8 or or or or or or or orComm. Control Syst.,3rd station AS 3100-XX (BECKER)(in passenger cabin)



L2313-008-00 12,5 27,6 X X X X X X X X

Tactical FM Radio Teledux 9 (AEG) 2m or 4m ON REQUEST 5,0 11,0 X X X X X X X X 3) 14)Tactical FM Radio GM 900 (MOTOROLA) ON REQUEST 4,0 8,8 X X X X X X X X 3) 14)Tactical FM Radio MCS 2000 (MOTOROLA ON REQUEST 3,5 7,7 X X X X X X X X 3) 14)Tactical FM Radio Tac / Com II (NAT) VHF-low, VHF-high, UHF

ON REQUEST TBC TBC X X X X X X X X 14)

VHF / UHF - AM / FM Transceiver ARC 210 (Rockwell &Collins) Not civil certified

ON REQUEST 10,0 22,1 X X X X X X X X 14)

ADF DFS 43 (incl. CD 432B) L3452-092-05 7,0 15,5 X X X X X X X X 15)Direction Finder Chelton DF931(stand alone) ON REQUEST 7,7 17,0 X X X X X X X 9) 14)Stand alone SAR DF517 (BECKER) L2313-010-03 2,8 6,2 X X X X X X X X 9) 14)GPS Nav System 2101 I/O Approach + (TRIMBLE) L3442-092-12 2,1 4,6 X X X X X X X XStormscope WX 1000 429E (GOODRICH) L3443-090-07 6,2 13,7 X X X X X X X X 9)Colour weather radar RDR2000 (HONEYWELL) (radome included)

L3443-090-02L2571-001-00

10,0 22,1 X X X X X X X 10)

Colour weather search radar ON REQUEST TBC TBC X X X X X X X X 10)Moving Map Kneeboard DKG 3 (Dornier, basic version) L3168-090-01 3,2 7,1 X X X X X X X X 11) 14)Moving Map System DKG 4 (Dornier) Map generatorcontrol unit + options

L2444-002-10 3,4 7,5 X X X X X X X X 10) 11)14)

Moving Map System Euro Nav III (Euro Avionics) L3168-090-08 9,0 19,9 X X X X X X X X 10) 11) 14)ELT 100 HM (ARTEX) L2563-801-02 1,9 4,2 X or X or X or X orELT C406-2 HM (ARTEX) 3 frequencies L2563-090-05 2,1 4,6 X X X XELT C406-2 HM (ARTEX) 3 frequencies Nav. Option L2563-821-52 2,1 4,6 X or X or X or X or 13)ELT JE 290 (JOLLIET) L2563-808-01 2,1 4,6 X or X or X or X or or) can be selected instead of the corresponding equipmentinstalled within minimum PINAO package 3) BFE required 9) Stand alone system; physical integration has to be checked 10) VRU (3ET) required 11) GPS required

13) ARINC 429 GPS required 14) Tactical mission equipment can not be certified by German CivilAviation Authorities. Eurocopter will ensure that the equipment iscompatible with the basic helicopter and will assist the customer inobtaining certification or acceptance approval in his country. 15) should be checked with customer airport landing requirements



PINAO code based onavionics solution 10


Wei

ght (

kg)

Wei

ght (

lbs)

1100

011

001

1101

011

011

1110

011

101

1111

011

111

Avionics solution 10 L2300-010-02 70,9 156,7 X X X X X X X XAvionics compartment L2576-001-00 6,2 13,7 X X X X X X X XSlant panel L3113-001-00 0,7 1,5 X X X X X X X XCentre console L3113-004-00 2,1 1,5 X X X X X X X XCopilot static system L3411-001-00 1,3 2,9 X X X X X X X XBleed air heating (**) L2104-100-00 6,6 14,6 X X X X X X X XSearch & Landing light (450W) L3343-003-00 3,2 7,1 X X X X X X X XWindshield wiper L3042-001-00 4,9 10,8 X X X X X X X X40 Ah battery L2433-005-00 19,4 42,8 X X X X X X X X200 A starter generators L2432-001-00 3,6 8,0 X X X X X X X XAC System L2420-002-00 3,2 7,1 X X X X X X X XMap case on I-Panel glare shield L3111-001-10 0,4 0,9 X X X X X X X XMEGHAS sensor kit L2212-300-00 15,9 35,1 X X X X X X X XDigital AFCS (DAFCS) L2212-001-00 38,5 85,1 X X X X X X X XELT C406-2 HM (ARTEX) 3 frequencies L2563-090-05 2,0 4,4 X X X XFirst aid kit L2562-001-00 1,3 2,6 X X X XEngine fire extinguishing L2621-001-00 3,8 8,4 X X X X(**) Select L2104-003-00 instead for EMS helicopters

Possible add-onsRadar Altimeter AHV16 (THALES) L3441-090-06 3,6 12,0 or or or or or or or orComm. Control Syst.,3rd station AS 3100-XX(BECKER) (in passenger cabin)



L2313-008-00 12,5 27,6 X X X X X X X X

Tactical FM Radio Teledux 9 (AEG) 2m or 4m BFE required


Tactical FM Radio GM 900 (MOTOROLA) BFE required


Tactical FM Radio MCS 2000 (MOTOROLA) BFE required


Tactical FM Radio Tac / Com II (NAT) VHF-low, VHF-high, UHF

ON REQUEST TBC TBC X X X X X X X X 14)

VHF / UHF - AM / FM Transceiver ARC 210 (Rockwell& Collins) Not civil certified


Automatic Direction Finder DFS 43 (incl. CD 432B) L3452-092-05 7,0 15,5 X X X X X X X X 15)Direction Finder Chelton DF931 stand alone ON REQUEST 7,7 17,0 X X X X X X X X 9) 14)Stand alone SAR DF (BECKER) L2313-010-03 2,8 6,2 X X X X X X X X 9) 14)FMS/Radio management with GPS Canadian Marconi(CMA3000 + CMA 3012)


GPS Nav System 2101 I/O Approach plus (TRIMBLE) L3442-092-12 2,1 4,6 X X X X X X X XStormscope WX 1000 429E (GOODRICH) L3443-090-07 6,2 13,7 X X X X X X X X 9)Colour weather radar RDR2000 (HONEYWELL)(radome included)

L3443-090-02/L2571-001-00

10,0 22,1 X X X X X X X X 10)

Colour weather search radar ON REQUEST TBC TBC X X X X X X X 10)Moving Map Kneeboard DKG 3 Dornier, basic version L3168-090-01 3,2 7,1 X X X X X X X X 11) 14)Moving Map System DKG 4 (Dornier) Map generatorcontrol unit + options

L2444-002-10 3,4 7,5 X X X X X X X X 10) 11) 14)

Moving Map System Euro Nav III (Euro Avionics): L3168-090-08 9,0 19,9 X X X X X X X X 10) 11) 14)ELT 100 HM (ARTEX) L2563-801-02 2,0 4,4 X or X or X or X orELT C406-2 HM (ARTEX) 3 frequencies L2563-090-05 2,1 4,6 X X X XELT C406-2 HM (ARTEX) 3 frequencies Nav. Option L2563-821-52 2,1 4,6 X or X or X or X or 13)ELT JE 290 (JOLLIET) L2563-808-01 2,1 4,6 X or X or X or X or or) can be selected instead of the correspondingequipment installed within minimum PINAO package 9) Stand alone system; physical integration has to bechecked 10) VRU (3ET) required 11) GPS required

13) ARINC 429 GPS required 14) Tactical mission equipment can not be certified by GermanCivil Aviation Authorities. Eurocopter will ensure that theequipment is compatible with the basic helicopter and will assistthe customer in obtaining certification or acceptance approval inhis country. 15) should be checked with customer airport landing requirements


135.02.101.01.EThis document is the 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

37

3. Optional headsets and helmet

The equipment listed below apply to any package/solution

Manufacturer/Type LinearWire

SpiralWire

LowImp.

HighImp.

ANR* Reference Weightkg

Weightlb.

HOLMBERG 90-04-08022-10 • • L2315-001-60 0.7 1.5

HOLMBERG 90-04-06025-10

• • L2315-001-61 0.7 1.5

DAVID CLARK H 10-76 • • L2315-001-10 0.5 1.1

DAVID CLARK H 10-56 • • L2315-001-11 0.5 1.1

SENNHEISER HMEC 222 III • • • L2315-001-52 0.4 0.9

* ANR: Active Noise Reduction Headsets

Manufacturer/Type LinearWire

SpiralWire

LowImp.

HighImp.

ANR* Reference Weightkg

Weightlb.

GENTEX Helmet SPH 5 • • L2315-002-10 1.3 2.4

* ANR: Active Noise Reduction Headsets



38




39

EQUIPMENT COMPATIBILITY

This chart concisely states the nature of the incompatibility:

��Impossibility of simultaneous fitment (hence impossible to sell the 2 items of equipment of the samehelicopter) – (“totally incompatible fitment”)

�� Impossibility of simultaneous fitment but possible to sell on the same aircraft (removable parts of one of theitems must be delivered, packed) – (“no simultaneous fitment”)

�� Possibility of simultaneous fitment on the same aircraft, but impossible to use simultaneously – (“nosimultaneous use”)

ReferenceOptional

Key-words ��"totally

incompatible fitment"

��"no

simultaneousfitment"

��"no

simultaneoususe"

Key-words

L1111-002-00 Two-colour external painting L1111-004-00 Multicolour external paintingL1111-004-00 Multicolour external painting L1111-002-00 Two-colour external paintingL2104-003-00 EMS Bleed air heating system L2104-200-00 Bleed air heating systemL2104-200-00 Bleed air heating system L2104-003-00 Bleed air heating system: EMS-versionL2105-001-00 Air conditioning system L2105-001-10 Air conditioning system for tropical environment

L8512-001-20 External hoist, detachable partsstd.Start./GenL8551-001-20 Light armour protection kit, detachable parts

L2105-001-10 Air conditioning for tropical environment L2105-001-00 Air conditioning systemL8512-001-20 External hoist, detachable parts

std.Start./GenL8551-001-20 Light armour protection kit, detachable parts

L2212-001-00 DAFCS. std.Start./GenL2217-001-10 VFR Pitch/Roll SASL2217-001-50 IFR Pitch/Roll SAS

L-2212-300-00 MEGHAS sensor kit L2300-001-02 Avionics solution 1L2300-003-02 Avionics solution 3L2300-004-02 Avionics solution 4

L2217-001-10 VFR Pitch/Roll SAS L2212-001-00 Digital Automatic Flight Control SystemL2217-001-50 IFR Pitch / Roll SAS

L2217-001-50 IFR Pitch/Roll SAS L2212-001-00 Digital Automatic Flight Control SystemL2217-001-10 VFR Pitch / Roll SAS

L2300-001-02 Avionics solution 1 L2212-300-00 MEGHAS sensors kitL3111-001-03 Copilot instrument panel extension 7"



L2300-007-02 Avionics solution 7 L3111-001-00 Copilot instrument panel extension 10"L3111-001-01 Copilot instrument panel extension 11"




L2420-002-00 AC system L2420-003-00 Dual AC systemL2420-003-00 Dual AC system L2420-002-00 AC systemL2433-001-00 Battery, "type Varta", (25Ah, 24V) L2433-002-00 Battery, type "Saft", 26Ah

L2433-005-00 Battery, "type Varta", 40 AhL2433-002-00 Battery, type "Saft", 26Ah L2433-001-00 Battery, type "Varta", 25Ah

L2433-005-00 Battery, "type Varta", 40 AhL2433-005-00 Battery, "type Varta", 40 Ah L2433-001-00 Battery, type "Varta", 25Ah

L2433-002-00 Battery, type "Saft", 26AhL2512-002-11 Pilot seat safety harness with manual lock L2512-003-10 Pilot seat with height setting capabilityL2512-002-02 Reversed copilot seat installation kit L2512-003-20 Copilot seat with height setting capability

(position change on ground) L2512-006-00 Winch operator seatL2525-101-76 VIP copilot's seat

std copil. seatEMS-Equip

L8551-001-20 Light armour protection kit, detachable partsL6701-001-00 Copilot flight controls

L2512-002-21 Manual lock for copilot seat L2512-003-20 Copilot seat with height setting capabilityL2512-006-00 Winch operator seat



40

ReferenceOptional



��"no


��"no

simultaneoususe"

Key-words

L2512-003-10 Pilot seat with height setting capability L2525-101-71 VIP pilot's seatstd. pilot seat

L2512-002-11 Pilot seat safety harness with manual lockL2512-003-20 Copilot seat height adjustable L2512-002-20 Reversed copilot seat installation kit

std. copil. seatL2512-002-21 Copilot seat safety harness with manual lock

L2512-006-00 Winch operator seatL2525-101-76 VIP copilot's seat

L2512-006-00 Winch operator seat turnable in flight L2512-002-20 Reversed copilot seat installation kitL2512-002-21 Copilot seat safety harness with manual lock

L2512-003-20 Copilot seat height adjustableL2513-004-40 Quick detachable VIP carpet for cabin

L2513-300-00 Floor covering, cockpit and cabin with carpetL2513-310-00 Floor covering with carpet complete

L6701-001-00 Dual controls, copilotEMS-equip

std. copil. seatL2525-101-76 VIP copilot's seat

L8551-001-20 Light armour protection kit, detachable partsL2513-004-40 Floor covering, cabin with quick L2512-006-00 Winch operator seat turnable in flight

detachable VIP carpet L2513-300-00 Floor covering, cockpit and cabin with carpetL2513-310-00 Floor covering with carpet completeL2522-004-20 Utility seats det. parts model Eurocopter

EMS-equip.L8522-320-00 Stretcher (16G), type BucherL8522-350-00 Installation device for one Bucher stretcherL8525-002-20 Inst. device for 1 FERNO/aerolite litterL8525-003-00 FERNO/Aerolite litter, SRFW 12-2/16G modifiedL8551-001-20 Light armour protection kit, detachable parts

L2513-200-00 Floor covering, cockpit, washable L2513-220-00 Floor washable completeL2513-300-00 Floor covering, cockpit and cabin with carpetL2513-310-00 Floor covering with carpet complete

L2513-210-00 Floor covering, cargo compartment, L2513-220-00 Floor washable completewashable L2513-300-00 Floor covering, cockpit and cabin with carpet

L2513-310-00 Floor covering with carpet completeL2513-220-00 Floor covering, cockpit, cabin and L2513-200-00 Floor covering, cockpit, washable

cargo compartment, washable L2513-210-00 Floor covering, cargo compartment, washableL2513-300-00 Floor covering, cockpit and cabin with carpetL2513-310-00 Floor covering with carpet complete

L2513-300-00 Floor covering, cockpit and cabin with L2512-006-00 Winch operator seat turnable in flightcarpet L2513-004-40 Quick detachable VIP carpet for cabin

L2513-200-00 Floor covering, cockpit, washableL2513-210-00 Floor covering, cargo compartment, washableL2513-220-00 Floor covering washable, completeL8522-320-00 Stretcher (16G), type BucherL8522-350-00 Installation device for one Bucher stretcherL8525-002-20 Inst. device for 1 FERNO/aerolite litterL8525-003-00 FERNO/Aerolite litter, SRFW 12-2/16G modifiedL2513-310-00 Floor covering with carpet completeL8551-001-20 Light armour protection kit, detachable partsEMS-Equip.

L2513-310-00 Floor covering, cockpit, cabin and L2512-006-00 Winch operator seatcargo compartment with carpet L2513-004-40 Quick detachable VIP carpet for cabin

L2513-200-00 Floor covering, cockpit, washableL2513-210-00 Floor covering, cargo compartment, washableL2513-220-00 Floor covering washable, completeL8522-320-00 Stretcher (16G), type BucherL8522-350-00 Installation device for one Bucher stretcherL8525-002-20 Inst. device for 1 FERNO/aerolite litterL8525-003-00 FERNO/Aerolite litter, SRFW 12-2/16G modifiedL2513-300-00 Floor covering, cockpit and cabin with carpetL8551-001-20 Light armour protection kit, detachable partsEMS-Equip.

L2514-003-01 Map case, integrated in copilot door L2525-102-81 Executive kitL2522-004-10 Utility seat arrangement for 3 rear L2524-001-00 cabin / cargo compartment separation wall

passengers, fixed provisions L8551-001-20 Light armour protection kit, detachable partsL2522-004-20 Utility seats for 3 rear pax, detachable parts L2513-004-40 Quick detachable VIP carpet for cabin

(in addition to the standard seats) L2524-001-00 Cabin / cargo compartment separation wallrear seats

L2524-021-00 Cabin/cargo compartment separation curtainL8522-320-00 Stretcher (16 G), type BucherL8522-350-00 Installation device for one Bucher stretcherL8525-002-20 Inst. device for 1 FERNO/aerolite litter

EMS & VIPEqui

L8525-003-00 FERNO/Aerolite litter, SRFW 12-2/16G modifiedL8551-001-20 Light armour protection kit, detachable parts



41

ReferenceOptional



��"no


��"no

simultaneoususe"

Key-words

L2524-001-00 Cabin / cargo compartment separation wall L2522-004-20 Utility seat arrangement for 3 rear passengersL2522-004-30 Utility seat arrangement for 3 rear passengersL2524-021-00 Cabin/cargo compartment curtain

EMS-EquipL8522-320-00 Stretcher (16 G), type BucherL8522-350-00 Installation device for one Bucher stretcherL8525-002-20 Inst. device for 1 FERNO/aerolite litterL8525-003-00 FERNO/Aerolite litter, SRFW 12-2/16G modifiedL8551-001-20 Light armour protection kit, detachable parts

L2524-002-00 Cockpit/cabin separating curtain L2524-003-00 NVG compatible cockpit/cabin separation curtainL3312-003-00 NVG-compatible std cockpit layout

L2524-003-00 NVG cockpit/ cabin separation curtain, L2524-002-00 Cockpit/cabin separation curtainL2524-021-00 Cabin/cargo separation curtain, L2522-004-20 Utility seat arrangement for 3 rear passengers

compatible with avionics rack (including L2522-004-30 Utility seat arrangement for 3 rear passengerssmoke detector) L2524-001-00 . Cabin/cargo compartment separation wall

EMS-EquipL8522-320-00 Stretcher (16 G), type BucherL8522-350-00 Installation device for one Bucher stretcherL8525-002-20 Inst. device for 1 FERNO/aerolite litterL8525-003-00 FERNO/Aerolite litter, SRFW 12-2/16G modifiedL8551-001-20 Light armour protection kit, detachable parts

L2525-101-71 VIP pilot’s seat L2512-003-10std pilot’s seat

Height adjustable pilot’s seat

L2525-101-76 VIP copilot’s seat L2512-002-02 Reversed copilot’s seat installation kitL2512-003-20 Height adjustable copilot’s seat

std copil. seatL2512-006-00 Winch operator seat turnable in flight

L2525-102-81 Executive kit L2514-003-01 Map case integrated in copilot doorL3111-001-10 Map case on instrument panel glare shield

L2562-001-00 First aid kit L2562-001-10 First aid kit for DGAC certificationL2562-001-10 First aid kit for DGAC certification L2562-001-00 First aid kitL2818-100-20 Internal long range fuel system, det. parts EMS & VIP

Equip.L2513-310-00 Carpet for cockpit, cabin & cargo compartment

L3042-001-00 Windshield wiper system L3043-001-00 Windshield wiper with washing deviceL3043-001-00 Windshield wiper system with washing sys L3042-001-00 Windshield wiper systemL3111-001-00 Copilot instrument panel extension 10" L3111-001-01 Copilot instrument panel extension 11"

L3111-001-03 Copilot instrument panel extension 7"L2300-007-02 Avionics solution 7L2300-008-02 Avionics solution 8L2300-009-02 Avionics solution 9L2300-010-02 Avionics solution 10

L3111-001-01 Copilot instrument panel extension 11" L3111-001-00 Copilot instrument panel extension 10"L3111-001-03 Copilot instrument panel extension 7"L2300-007-02 Avionics solution 7L2300-008-02 Avionics solution 8L2300-009-02 Avionics solution 9L2300-010-02 Avionics solution 10

L3111-001-03 Copilot instrument panel extension 7" L3111-001-00 Copilot instrument panel extension 10"L3111-001-01 Copilot instrument panel extension 11"L2300-001-02 Avionics solution 1L2300-003-02 Avionics solution 3L2300-004-02 Avionics solution 4

L3111-001-10 Map cases on instrument panel L2525-102-81 Executive kitL3215-001-21 Emergency floats, detachable parts, L3273-001-00 Lengthened skids

L3216-001-10 High skid landing gearL3272-001-20 Snow skids, detachable parts

L3216-001-10 High skid landing gear L3215-001-21 Emergency floats, detachable partsL3272-001-20 Snow skids, detachable parts L3215-001-21 Emergency floats, detachable parts

L3216-001-10 High skid landing gearL3274-001-20 Settling protectors, detachable parts

L3273-001-00 Lengthened skids L3215-001-21 Emergency floats, detachable partsL3216-001-10 High skid landing gear

L3274-001-20 Settling protectors, detachable parts L3272-001-20 Snow skids, detachable partsL3312-003-00 NVG compatible standard cockpit layout L2524-002-00 Cockpit/cabin separating curtainL3322-001-00 Boarding step illumination L3353-005-00 Emergency lightsL3343-003-00 Landing & searchlight 450 W L3343-006-00 Landing & searchlight 400/200W NVG

L8511-002-20 Cargo hook mirrors detachable partsL3343-006-00 Landing & searchlight 400 W/200W L3343-003-00 Landing & searchlight 450 W

NVG compatible L8511-002-20 Cargo hook mirrors detachable partsL3346-100-10 SX16, front installation fixed provisions L2571-001-00 Radar radom

L3346-300-10 SX16, LH, MFS mounted, fixed provisionsL3346-400-20 SX16, LH, MFS mounted, detachable parts



42

ReferenceOptional



��"no


��"no

simultaneoususe"

Key-words

L3346-100-20 SX16, front installation, L2571-001-00 Radar radomdetachable parts, (without vendor parts) L3346-300-10 SX16, LH, MFS mounted, fixed provisions

L3346-400-20 SX16, LH, MFS mounted, detachable partsL3346-300-10 Search light SX 16 fixed provisions L3346-100-10 SX16, front installation, fixed provisions

LH MFS mounted L3346-100-20 SX16, front installation, detachable parts,L3346-400-20 SX16 MFS mounted L3346-100-10 SX16, front installation, fixed provisions

detachable parts, without vendor parts L3346-100-20 SX16, front installation, detachable parts,L3353-005-00 Emergency lights L3322-001-00 Boarding step illuminationL5213-001-11 Int. and max. posi. sliding door fastener LH L5213-001-12 Sliding door fastener, max. position, LHL5213-001-12 Sliding door fastener, max. position, LH L5213-001-11 Interme&max. position sliding. door fastener, LHL5213-001-21 Inter&max. position sliding door fastener RH L5213-001-22 Sliding door fastener, max. position, RHL5213-001-22 Sliding door fastener, max. position, RH L5213-001-21 Interme&max. position sliding. door fastener, LHL6701-001-00 Dual controls L2512-006-00 Winch operator seat instead of copilot seat,

L6721-001-00 Copilot controls coverL6721-001-00 Copilot flight controls cover L6701-001-00 Copilot flight controlsL7161-001-00 Sand filter system

std.Start./GenL8512-001-20 External hoist, detachable parts

L8511-002-20 Cargo hook mirrors detachable parts L3343-003-00 Landing & searchlight 450 WL3343-006-00 Landing & searchlight 400/200 W NVG

L8512-001-10 External hoist, fixed provisions L8534-000-11 Rope-down device, LH, fixed provisionsL8512-001-20 External hoist, detachable part L2105-001-00 Air conditioning/cooling system (Vapour cycle)

L2105-001-10 Air conditioning for tropical environmentstd.Start./Gen

L8544-002-00 Lashing points for high wind speedsL7161-001-00 Sand filter system

L8534-000-12 Rope down device for 2 persons, det. parts, LHL8514-001-00 Multipurpose attachment hardpoints L8512-001-10 External hoist, fixed provisions

L8534-00-11 Rope-down device, fixed provisions LHL8534-00-21 Rope-down device, fixed provisions RH

L8522-320-00 Folding stretcher (16 G), type Bucher L2513-004-40 quick detachable VIP carpet for cabinL2513-300-00 Floor covering, cockpit and cabin with carpetL2513-310-00 Carpet for cockpit, cabin and cargo compartment

L2522-004-20 Utility seats for 3 rear passengers, det.partsL2522-004-30 Utility seats for 3 rear passengers, det. partsL2524-001-00 Cabin / cargo compartment separation wallL2524-020-00 Cabin/cargo compartment separation curtain

L8525-002-201 std rear seat

Installation device for one FERNO/Aerolite-type

L8525-003-00 FERNO/Aerolite-type litter, 12-2/16G modifiedL8551-001-20 Armour protection kit, detachable parts

L8522-350-00 Stretcher retainer system for one L2513-004-40 Quick detachable VIP carpet for cabinBucher-type folding stretcher (16G) L2513-300-00 Floor covering, cockpit and cabin with carpet

L2513-310-00 Carpet for cockpit, cabin and cargo compartmentL2522-004-20 Utility seats for 3 rear passengers, det. partsL2522-004-30 Utility seats for 3 rear passengers, det. partL2524-001-00 Cabin / cargo compartment separation wallL2524-020-00 Cabin/cargo compartment separation curtain


Installation device for one FERNO/Aerolite-type

L8525-003-00 FERNO/Aerolite-type litter, 12-2/16G modifiedL8551-001-20 Armour protection kit, detachable parts

L8525-002-20 Litter installation device for one L2513-004-40 Quick detachable VIP carpet for cabinFerno/Aerolite-type litter, L2513-300-00 Floor covering, cockpit and cabin with carpetmodel SRFW 12-2/16 G modified L2513-310-00 Carpet for cockpit, cabin and cargo compartment

L2522-004-20 Utility seat for 3 rear passengers, det. partsL2522-004-30 Utility seat for 3 rear passengers, det. partL2524-001-00 Cabin / cargo compartment separation wallL2524-020-00 Cabin/cargo compartment separation curtain


Folding stretcher (16 G), type Bucher

L8522-350-00 Stretcher retainer for one Bucher- stretcherL8551-001-20 Armour protection kit, detachable parts

L8525-003-00 FERNO/Aerolite-type foldable litter, L2513-004-40 Quick detachable VIP carpet for cabinmodel SRFW 12-2 / 16G modified L2513-300-00 Floor covering, cockpit and cabin with carpet

L2513-310-00 Carpet for cockpit, cabin and cargo compartmentL2522-004-20 Utility seats for 3 rear passengers, det. partsL2522-004-30 Utility seats for 3 rear passengers, det. partL2524-001-00 Pax/cargo compartment separation wallL2524-020-00 Cabin/cargo compartment separation curtainL8522-320-00 Folding stretcher (16 G), type Bucher


Stretcher retainer for one Bucher- stretcher

L8551-001-20 Armour protection kit, detachable parts



43

ReferenceOptional



��"no


��"no

simultaneoususe"

Key-words

L8534-000-11 Rope-down device fixed provisions, LH L8512-001-10 External hoist, fixed provisionsL8534-000-12 Rope-down device for two persons, L8512-001-20 External hoist, detachable parts

detachable parts, LH L8544-002-00 Lashing points for high wind speedsL8544-002-00 Lashing points for high wind speeds L8512-001-20 External hoist, detachable part

L8534-000-12 Rope-down device, detachable parts, LHL8551-001-20 Light armour protection kit, cockpit and L2105-001-00 Air conditioning system

cabin, detachable parts L2105-001-10 Air conditioning system for tropical environmentL2512-002-20 Reversed copilot seat, installation kitL2512-006-00 Winch operator seat

L2513-004-40 Quick detachable VIP carpet for cabinL2513-300-00 Floor covering, cockpit and cabin with carpetL2513-310-00 Carpet for cockpit, cabin and cargo compartmentL2522-004-20 Utility seat for 3 passengers, det. parts

L2524-001-00 Cabin/cargo compartment separation wallL8522-320-00 Folding stretcher (16 G), type BucherL8522-350-00 Stretcher retainer for one Bucher-type stretcherL8525-002-20 Installation device for one FERNO/Aerolite-type



44




45

MAIN PERFORMANCE

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

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

The EC135 P2 will be certified over the complete envelope and for the increased OEI power levels for the end ofmarch 2002, and therefore some performance data have to be considered as preliminary (OEI hover/climb) orare not available yet (Cat. A)

PERFORMANCE ON 2 ENGINESPratt & Whitney PW206B2

Gross Weight kg

lb

2,200

4,850

2,400

5,290

2,630

5,800

2,720

6,000

2,835

6,250

� Maximum speed VNE km/hkts

287155

278150

278150

278150

259140

� Maximum cruising speed km/hkts

262141

261141

259140

257139

256138

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

232.5512.5

232.5512.5

232.5512.5

232.5512.5

232.5512.5

� Economical cruising speed km/hkts

220119

224121

226122

228123

229124

� Fuel consumptionat economical cruising speed

kg/hlb/h

187.5413.5

193425.5

198436.5

201443

205452

� Fuel consumption at 65 KIAS kg/hlb/h

143.5316.5

148.5327.5

155342

157.5347.2

161355

� Rate of climb (TOP) m/sft/min

11.72300

10.42050

8.91750

8.41,650

7.61,500

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

mft

4,5701)

15,0001) 4,5701)

15,0001) 4,45014,600

4,14013,600

3,0452)

10,0002)

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

mft

3,8801)

12,7501) 3,8801)

12,7501)3,230

10,6002,8309,300

2,3157,600

� Hover ceiling OGE (TOP), ISA mft

4,5701)

15,0001)4,420

14,5003,580

11,750 3,26010,700

2,1907,200

� Hover ceiling OGE (TOP), ISA + 20°C mft

3,8801)

12,7501)3,155

10,3502,0756,800

1,6405,400

1,1003,600

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

mft

4,5723)

15,0003) 4,5723)

15,0003) 4,5723)

15,0003) 4,5723)

15,0003) 3,0452)

10,0002)

1) 15,000 ft density altitude certification limit2) 10,000 ft pressure altitude certification limit3) this limitation may be suppressed during the year 2002.



46

PERFORMANCE ON 2 ENGINESPratt & Whitney PW206B2

Gross Weight kg

lb

2,200

4,850

2,400

5,290

2,630

5,800

2,720

6,000

2,835

6,250

� Maximum range (without fuel reserve ateconomical cruise speed)

• standard tank configuration (536 kg)

• long rang tank configuration

• standard tank configuration (560 kg*)


kmnmkmnm

kmnmkmnm

640345835451

670362863466

635343825445

660356853460

625337815440

655353843455

620335810437

651351838452

615332805434

646349833450

� Maximum endurance (without fuel reserve at65 KIAS

• standard tank configuration (536 kg)• long rang tank configuration

• standard tank configuration (560 kg*)• long rang tank configuration

h:minh:min

h:minh:min

3:545:06

4:055:17

3:454:57

4:565:08

3:364:48

3:484:56

3:334:42

3:454:53

3:304:36

3:394:47

*only available from the helicopter with the S/N (Serial Number) 250 onwards.

PERFORMANCE ON 1 ENGINEPratt & Whitney PW206B2

Gross Weight kg

lb

2,200

4,850

2,400

5,290

2,630

5,800

2,720

6,000

2,835

6,250

� Service ceiling w. 100 ft/min climb reserve(MCP OEI-power) at ISA

mft

4,89016,050

4,26514,000

3,55011,650

3,27510,750

2,9259,600

� Service ceiling w. 100 ft/min climb reserve(MCP OEI-power) at ISA + 20°C

mft

4,21013,800

3,50511,500

2,6958,850

2,3757,800

1,9656,450

� Rate of climb (MCP OEI-power at SL) m/sft/min

4.0785

3.0585

1.9380

1.5300

1.1215

� Max. temperature for CAT A take-off fromclear heliport at SL

°C + 50 + 50 + 50 + 50 + 45

� Max. gross weight hover ceiling OGE, SL,ISA, OEI, no wind (30-sec-power)

kglb

2,6655,875

� Max. gross weight hover ceiling OGE, SL,ISA + 20°C, OEI, no wind (30-sec-power)

kglb

2,5505,622

� Max. gross weight hover ceiling IGE, SL, 4ftISA, OEI, no wind (2-min-power)

kglb

2,8356,250

� Max. gross weight hover ceiling IGE, SL, 4ftISA + 20°C, OEI, no wind (2-min-power)

kglb

2,6305,798

� Max. gross weight CAT A, VTOL, SL,(ISA / ISA + 10°C)

kglb

2,8356,250



47

The EC135T2 will be certified over the complete flight envelope for mid. 2002, and therefore performance datahave to be considered as preliminary (OEI hover/climb, Cat A)

PERFORMANCE ON 2 ENGINESTurbomeca Arrius 2B2

Gross Weight kg

lb

2,200

4,850

2,400

5,290

2,630

5,800

2,720

6,000

2,835

6,250

� Maximum speed VNE km/hkts

287155

278150

278150

278150

259140

� Maximum cruising speed km/hkts

262141

261141

259140

257139

256138

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

237522

237522

237522

237522

237522

� Economical cruising speed km/hkts

231125

233126

235127

237128

239129

� Fuel consumptionat economical cruising speed

kg/hlb/h

204450

208.5460.0

213470

215.5475.0

219483

� Fuel consumption at 65 KIAS kg/hlb/h

155.5343.0

160353

166366

168.5371.5

171.5378.0

� Rate of climb (TOP) m/sft/min

11.72,300

10.42,050

8.91,650

8.41,650

7.61,500

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

mft

4,5701)

15,0001) 4,5701)

15,0001) 4,32014,150

4,04013,250

3,0452)

10,0002)

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

mft

3,8801)

12,7501) 3,8801)

12,7501) 3,10010,150

2,7409,000

2,2557,400

� Hover ceiling OGE (TOP), ISA mft

4,5701)

15,0001) 4,29014,050

3,48011,400

3,10010,200

2,1907,200

� Hover ceiling OGE (TOP), ISA + 20°C mft

3,8801)

12,7501) 3,05010,000

1,9556,400

1,5255,000

1,0053,300

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

mft

6,09520,000

6,09520,000

5,48018,000

5,22517,150

3,0452)

10,0002)

1) 15,000 ft density altitude certification limit2) 10,000 ft pressure altitude certification limit



48

PERFORMANCE ON 2 ENGINESTurbomeca Arrius 2B2

Gross Weight kg

lb

2,200

4,850

2,400

5,290

2,630

5,800

2,720

6,000

2,835

6,250

� Maximum range (without fuel reserve ateconomical cruise speed)

• standard tank configuration (536 kg)


• standard tank configuration (560 kg*)


kmnmkmnm

kmnmkmnm

610329795429

641346823444

605326790426

636343818441

600324785424

626338808436

598322780421

625337804434

595321775418

621335799431

� Maximum endurance (without fuel reserve at65 KIAS

• standard tank configuration (536 kg)• long rang tank configuration

• standard tank configuration (560 kg*)• long rang tank configuration

h:minh:min

h:minh:min

3:334:39

3:454:50

3:274:33

3:394:42

3:214:24

3:304:32

3:184:21

3:274:29

3:154:15

3:244:26

*only available from the helicopter with the S/N (Serial Number) 250 onwards.

PERFORMANCE ON 1 ENGINETurbomeca Arrius 2B2

Gross Weight kg

lb

2,200

4,850

2,400

5,290

2,630

5,800

2,720

6,000

2,835

6,250

� Service ceiling w. 100 ft/min climb reserve(MCP OEI-power) at ISA

mft

5,15016,900

4,51014,800

3,79012,450

3,52011,500

3,045 10,0002)

� Service ceiling w. 100 ft/min climb reserve(MCP OEI-power) at ISA + 20°C

mft

4,51014,800

3,73012,250

2,8309,300

2,5008,200

2,0706,800

� Rate of climb (MCP OEI-power at SL) m/sft/min

4.0785

3.0585

1.9380

1.5300

1.1215

� Max. temperature for CAT A take-off fromclear heliport at SL

°C + 50 + 50 + 50 + 50 + 46

� Max. gross weight hover ceiling OGE, SL,ISA, OEI, no wind (30-sec-power)

kglb

2,6655,875

� Max. gross weight hover ceiling OGE, SL,ISA + 20°C, OEI, no wind (30-sec-power)

kglb

2,6155,765

� Max. gross weight hover ceiling IGE, SL, 4ftISA, OEI, no wind (2-min-power)

kglb

2,8356,250

� Max. gross weight hover ceiling IGE, SL, 4ftISA + 20°C, OEI, no wind (2-min-power)

kglb

2,6905,930

� Max. gross weight CAT A, VTOL, SL,(ISA / ISA + 10°C)

kglb

2,8356,250

2) 10,000 ft pressure altitude certification limit



49

OPERATING LIMITATIONS

The helicopter can be operated within the following altitude limitations (according to the Flight Manual):

Gross Weight 2,720 kg6,000 lb

2,835 kg6,250 lb

� Maximum operating altitude 6,100 m PA20,000 ft PA

3,048 m PA10,000 ft PA

� Maximum operating altitude for hover in ground effect,takeoff and landing

4,570 m DA15,000 ft DA

3,048 m PA10,000 ft PA

� Minimum temperature - 35°C (- 31°F)

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

ABBREVIATIONS

AGL : Above Ground Level OGE : Out Of Ground EffectDA : Density Altitude PA : Pressure AltitudeIGE : In Ground Effect SL : Sea LevelISA : International Standard Atmosphere TOP : Take-Off PowerMCP : Maximum Continuous Power VNE : Never-Exceed SpeedOEI : One Engine Inoperative VTOL: Vertical Take-Off and Landing



50

Hover In Ground Effect (HIGE, TOP, no wind)

with two PW206B2 engines



51

Hover In Ground Effect (HIGE, TOP, no wind)

with two ARRIUS 2B2 engines



52

Hover Out Of Ground effect (HOGE, TOP)




53

Hover Out Of Ground Effect (HOGE, TOP)




54

Hover Out Of Ground effect (HOGE, OEI, 30 sec-power)

with one PW206B2 engine



55

Hover Out Of Ground effect (HOGE, OEI, 2.0 min-power)

with one PW206B2 engine



56

Hover Out Of Ground Effect (HOGE, OEI, 30 sec-power)

with one ARRIUS 2B2 engine



57

Hover Out Of Ground effect (HOGE, OEI, 2.0 min-power)

with one ARRIUS 2B2 engine



58

Maximum Cruising Speed




59

Maximum Cruising Speed




60

Maximum Rate Of Climb, TOP

with two PW206B2 engines, MTOW: 2835 kg



61

Maximum Rate Of Climb, TOP

with two ARRIUS 2B2 engines, MTOW: 2835 kg



62

Payload/Range




63

Payload/Range




64


EC 135 Technical data

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Transcript of EC 135 Technical data