Technical Data

Contents
1 Foreword......................................................................................................................................... 3
2 General characteristics ................................................................................................................... 7
2.1 External dimensions ................................................................................................................... 7
2.2 Internal dimensions .................................................................................................................... 8
2.3 Possible cabin arrangement (seats & equipment as option)...................................................... 8
2.4 Weight ........................................................................................................................................ 9
2.5 Fuel Capacities........................................................................................................................... 9
2.6 Engines: 2 TURBOMECA turbine engines - ARRIEL 1E2 ......................................................... 9
2.7 Main transmission....................................................................................................................... 9
3 Standard aircraft definition............................................................................................................ 11
4 Basic configuration choice ............................................................................................................ 13
4.1 VFR packages, based on Avionics Solutions A1 and A2......................................................... 16
4.2 Dual pilot or Single/Dual Pilot IFR, based on Avionics Sol. B1 and B2 ................................... 22
4.3 Dual pilot or Single/Dual Pilot IFR with Dual FMS/NMS (Av. Sol. B3) ..................................... 28
4.4 Single Pilot IFR, based on Avionics Solution C........................................................................ 32
5 Cabin arrangement ....................................................................................................................... 37
5.1 Passenger transport ................................................................................................................. 37
5.2 EMS equipment ........................................................................................................................ 38
6 Optional equipment....................................................................................................................... 41
6.1 Shopping list ............................................................................................................................. 41
6.2 Shopping list avionics ............................................................................................................... 45
6.3 Offshore.................................................................................................................................... 47
7 Table of constraints ...................................................................................................................... 49
7.1 General Checklist for Incompatibilities: .................................................................................... 49
7.2 Legend of the following chart ................................................................................................... 50
8 Main performance ......................................................................................................................... 51

Manufacturer’s notes – Attention!

Eurocopter’s policy is one of on-going product enhancement which means

that alterations in definition, pictures, weights, dimensions or performance
may be made at any time without notice being included in those documents
that have already been issued.

This document cannot thus be taken as an offer or serve as an appendix to a

contract without a prior check as to its validity and prior written agreement of
EUROCOPTER.

The operational or certification regulations, as defined by the local

authorities, can make compulsory the installation of some of the equipment
or recommended solutions, listed in this document. This list does not claim to
cover the whole of the worldwide operational requirements nor the equipment
not specifically related to the helicopter (for example: life jacket) or necessary
for particular missions (for example: supplemental oxygen). The operator is
responsible for ascertaining with his local authorities that the planned
configuration of the helicopter complies with regulatory requirements for the
area(s) of operations and the type(s) of mission(s) considered.
®
EUROCOPTER, its logo, M’ARMS are trade marks of the Eurocopter group.

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

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

1 Foreword

The EC145 is a twin-engine, multi-purpose helicopter of the 3-4 ton class with up to 12 seats for pilot/s
and passengers. It combines Eurocopter’s latest developments, like advanced cockpit design, avionics
and sophisticated electrical system with the rugged and proven design elements of the BK117, as for
example the rotor system. The EC145’s hingeless rotor system with its monolithic titanium hub
(‘System Bölkow’) is proven all over the world. Furthermore, the rotor blades have been improved with
respect to higher performance and lower noise and vibrations levels. The use of the variable
rotorspeed and torque matching system (VARTOMS), known from the predecessor model BK117 C-1
has been extended. Besides ameliorating flying comfort, this makes the EC145 the quietest helicopter
in its class bringing it to 6.7 dBA below ICAO limits.
In addition to environmental and economical aspects, the rotor system together with high TBO
gearbox and airframe components grant for low maintenance costs, and on the other hand high in-
service-time of the helicopter due to low scheduled maintenance required.
The EC145 is equipped with two powerful and reliable Turbomeca Arriel 1E2 engines which, in
combination with its lifting system, provide outstanding performance and vital power reserves even in
one-engine-inoperative scenarios. Twin-engine reliability is complemented by a fully separated fuel
system, a tandem hydraulic system, dual electrical system and redundant lubrication for the main
transmission. Further positive safety aspects of the EC145 are design elements like energy absorbing
fuselage and seats, as well as crash resistant fuel cells. The EC145 allows Cat. A operation up to the
level of performance class 1 and performance class 2 according to JAR OPS 3 amendment 3.
A wide range of optional equipment, like emergency floats, rescue hoist, SX16 search light, load hook,
plus many more is available for the EC145 and can be fitted simultaneously in most cases. Together
with its most versatile cabin layout (utility, comfort, corporate, ...), the EC145 is ready to take up all
sorts of missions, for example survey, transport, EMS, public service, to name a few.

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

Compared to other helicopters in its class, the EC145 offers a significantly larger cabin, featuring:
„ excellent outside vision for pilot/s, crew or passengers
„ roomy cabin with no partitions or protrusions, no center post, no door post
„ unrivalled side loading (no door posts) and rear loading capability
„ flat floor all over the cabin area.

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

The EC145 offers a choice of modern state-of-the-art glass cockpit solutions comprising of primary
flight displays (PFD) and NAV displays (ND) as well as a central panel display system (CPDS). All
LCD screens are well arranged on the instrument panel, easy to read even if viewed from an angle
and feature perfect readability in any light conditions. An NVG layout is available as an option. The
unique color coding, warning and information concept helps the pilot/s to collect all relevant
parameters while suppressing presentation of non-relevant information. Additionally, Eurocopter’s
unique first limit indicator (FLI) dramatically simplifies engine and torque monitoring. Being relieved
from extensive instrument scan without missing vital information, pilots can dedicate more of their
attention to the mission.

Latest news / highlights:

„ High-density seating configuration for up to 10 passengers in the cabin
„ Search light SX5 will be available in the next months
„ Maintenance reduction package available (no 50 h inspection if fuzz burners for tail rotor and
intermediate gearbox are installed)
„ New Corporate Passenger Transport package is available

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

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

2 General characteristics

2.1 External dimensions

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

2.2 Internal dimensions

Floor area Volume

2 2
Cabin & baggage compartment 4.72 m 50.77 ft 6.04 m3 213.15 ft3
(Baggage compartment with 8 seats installed) 0.84 m2 9.07 ft2 1.32 m3 46.72 ft3
Copilot 0.72 m2 7.73 ft2 0.80 m3 28.25 ft3
Pilot (not shaded) 1.09 m2 11.80 ft2 1.24 m3 43.76 ft3

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

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

2.3 Possible cabin arrangement (seats & equipment as option)

1 or 2 pilots + up to 8 passengers in club seating configuration

Passenger transport
(energy absorbing individual seats) + 1.32 m3 baggage / freight
1 or 2 pilots + up to 10 passengers in high-density seating
High-density seating
configuration (energy absorbing individual troop seats)
EMS / Casualty evacuation 1 or 2 pilots + up to 2 stretcher patients + up to 3 HEMS crew

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

2.4 Weight

Note : margin ± 1.5 % kg lb

„ Empty weight, wet (in standard aircraft configuration) 1,792 3,951
„ Useful load (for standard aircraft configuration) 1,793 3,953
„ Pilot 80 176
„ Payload and / or fuel 1,713 3,777
„ Maximum take-off weight 3,585 7,903
„ Maximum take-off weight with external load 3,585 7,903
„ Sling load (single hook) 1,500 3,307

2.5 Fuel Capacities

Note: Tolerance of fuel figures: ±2% Usable Fuel Unusable Fuel

Fuel density used is 0.8 kg / liter.
lb kg l lb kg
„ Main Tank 1307.8 593.2 741.5 7.3 3.3
„ Supply Tank (left) 104.1 47.2 59.0 6.6 3.0
„ Supply Tank (right) 118.2 53.6 67.0 6.6 3.0
„ Total 1530.0 694.0 867.5 20.5 9.3

2.6 Engines: 2 TURBOMECA turbine engines - ARRIEL 1E2

Engine ratings

Thermodynamic limits per engine at SL, ISA kW ch shp

„ One Engine Inoperative (OEI), 2.5 min power 574 780 770
„ One Engine Inoperative (OEI), MCP 550 748 738
„ Take-Off Power (TOP) 550 748 738
„ Maximum Continuous Power (MCP) 516 701 692

2.7 Main transmission

Main transmission ratings

Single engine operation kW ch shp

„ 2.5 min OEI-power 1 x 551 1 x 750 1 x 739
„ Maximum continuous OEI-power 1 x 404 1 x 550 1 x 542

Twin engine operation

„ Take-Off Power (TOP) 2 x 388 2 x 528 2 x 520
„ Maximum Continuous Power (MCP) 2 x 316 2 x 430 2 x 424

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

BLANK

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

3 Standard aircraft definition

GENERAL

ƒ Energy absorbing fuselage ƒ Skid-type landing gear with skid protectors, capable of
ƒ Tail boom with fixed horizontal stabilizer and two end- taking ground-handling wheels
plates ƒ Long boarding steps, LH and RH
ƒ Upper deck with fittings for main gearbox, engines, ƒ Cold weather kit
hydraulic and cooling system ƒ Built-in maintenance steps and grips
ƒ Cowlings for main transmission and engines ƒ Exterior painting (single color)

COCKPIT, CABIN AND CARGO COMPARTMENT

ƒ One-level cabin and cargo compartment floor with ƒ Instrument panel with extension on pilot's side and glare
integrated rails shield
ƒ Glazed canopy ƒ Ram-air for cockpit
ƒ Two hinged cockpit doors with sliding window ƒ Electrical ventilating system for cockpit
ƒ Map case in pilot's door ƒ Headset holder in the cockpit, rotatable
ƒ Two wide passenger sliding doors ƒ Portable fire extinguisher
ƒ Two rear hinged clam-shell doors ƒ Stowage net for first aid kit at the LH rear clam-shell door
ƒ Longitudinally adjustable energy absorbing pilot and copilot ƒ First aid kit
seats with head rest and 4-point safety belts with automatic ƒ Flash light (torch)
locking system ƒ 4 mobile tie-down rings
ƒ Cabin boarding grips (LH and RH) ƒ Slant panel
ƒ Interior panelling with integrated basic sound insulation ƒ Center console
ƒ Flight controls (pilot side) ƒ Windscreen wiper for pilot and copilot
ƒ Engine twist grip controls at pilot's collective pitch lever ƒ Door open warning

BASIC INSTRUMENTATION
Central Panel ƒ Warning unit:
ƒ Central Panel Display system (CPDS) consisting of two ƒ Engine fire warning with fuel emergency shut-off
LCD displays ƒ Warning lights
ƒ Caution Advisory Display (CAD) with digital indication of: ƒ Aural warning (for each warning, rotor RPM, fire
ƒ Caution and advisory information warning)
ƒ Fuel quantity indication ƒ Fire extinguishing system warning
ƒ Vehicle and Engine Management Display (VEMD) with ƒ Main switch panel:
digital indication of: ƒ DC power control
ƒ Engine parameters (engine oil pressure, engine oil ƒ VARTOMS control
temperature) ƒ Start switches
ƒ FLI (First Limit Indicator) for TQ, TOT, ΔN1 as ƒ Magnetic compass (mounted on the lateral nose spare of
analogue display the cockpit)
ƒ Main gear box parameters (oil pressure,
oil temperature) Air Data
ƒ Dual amperemeter for generator; amperemeter for ƒ Dual pitot static system (electrically heated pitot tube and
battery static port)
ƒ Dual voltmeter ƒ 2 ADC MEGHAS sensors
ƒ Outside air temperature (OAT)
ƒ Mast moment indication Standard Instruments (single pilot) 1)
ƒ Back-up conventional instruments (2“) ƒ Air speed indicator (3“)
ƒ Clock ƒ Vertical speed indicator (3“)
ƒ Stand-by-horizon ƒ Encoding altimeter (3“)
ƒ Triple (rotor and engines) RPM-indicator ƒ Artificial horizon (4“)
ƒ Gyro magnetic heading with horizontal situation ind. (3”)

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

The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
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 Technical Data
POWER PLANT
ƒ Two TURBOMECA ARRIEL 1E2 turbine engines, complete ƒ Fire detection and extinguishing system
with starting, fuel supply and control systems ƒ VARTOMS (VAriable Rotor speed and TOrque Matching
ƒ Crash resistant fuel system System)
ƒ Two independent oil cooling and lubrication systems of the ƒ Overspeed control
engines ƒ Cycle counter

TRANSMISSION SYSTEM

ƒ Main transmission including an independent redundant ƒ Tail rotor transmission system with splash lubrication,
lubrication system and monitoring sensors magnetic plug and oil level sight gauge
ƒ Rotor brake system

ROTOR AND FLIGHT CONTROLS

ƒ Hingeless main rotor (System Bölkow) with 4 glass and ƒ Dual hydraulic boost system for cyclic and collective blade
carbon fiber reinforced blades with erosion protection strip control of the main rotor
ƒ Semi-rigid tail rotor with 2 twisted glass fiber reinforced ƒ Single hydraulic boost system for yaw control
blades of new technology with erosion protection strip ƒ Stability augmentation system (SAS) for tail rotor
ƒ Basic provisions for an easy integration of a balancing ƒ Main and tail rotors tip painting (yellow)
system

ELECTRICAL INSTALLATION
ƒ Power generation system: ƒ Lighting:
ƒ Two starter/generators (2 x 200 A, 28 VDC) ƒ Anti-collision warning light (red flashing)
ƒ Nickel-Cadmium battery, (24 V, 27 Ah) ƒ Fixed landing light (250 W)
ƒ External power connector (STANAG 3302) ƒ Three position lights (red, green, white)
ƒ Power distribution system: ƒ Adjustable instrument lighting
ƒ Two primary busbars ƒ One utility light in the cockpit
ƒ Two essential busbars ƒ Lights in the cabin and cargo compartment
ƒ Two shedding busbars ƒ Boarding illumination
ƒ Two non-essential busbars (50 A) ƒ Emergency lights
for optional equipment only ƒ Radio:
ƒ Battery bus ƒ Two radio master switch
ƒ One utility receptacle in cargo compartment
(28VDC, 15A)

GROUND HANDLING KIT Weight not included in the standard helicopter empty weight
ƒ Two ground-handling wheels ƒ Battery key
ƒ Basic aircraft covers (short time) ƒ Lifting points
ƒ Oil drain hoses ƒ Compass compensation key
ƒ Keys for cockpit doors, cabin doors, baggage compartment ƒ Fuel drain device
doors and tank flap (one-key system)

DOCUMENTATION
STANDARD DOCUMENTATION: STANDARD DOCUMENTATION (contd.):
2) 1) 2)
ƒ Flight Manual ƒ Engine Documentation including:
2)
ƒ Pilots-Checklist ƒ Maintenance Manual
ƒ Logbook ƒ Illustrated Parts Catalogue (IPC)
ƒ Historical Record ƒ Service Bulletins
1) 2) 3)
ƒ CD-ROM including AMM, SDS, MSM, WDM, IPC
ƒ Master Servicing Manual (MSM)
1) 2) OPTIONAL DOCUMENTATION (hard copy format):
1) 2) 3)
ƒ Service Bulletin Catalogue (SB)
1) 2) ƒ Aircraft Maintenance Manual (AMM)
1) 2) 3)
ƒ List of Applicable Publications (LOAP)
1) 2) ƒ System Description Section (SDS)
1) 2) 3)
ƒ Avionics Manual (for avionics installed by Eurocopter)
1) 3) ƒ Wiring Diagram Manual (WMD)
1) 2)
ƒ Illustrated Parts Catalogue (IPC)
1) weight not included in the standard helicopter empty weight
2) documents revision service is available
3) customized documentation

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

4 Basic configuration choice

Selection of a PINAO package

Please select your PINAO code according to your operational needs by using the following table:

Single Dual Single/Dual

Pilot P 1 2 3
VFR IFR
VFR/IFR I 0 1
day night
Day/night N 0 1
no yes
Cat. A A 0 1
JAR-OPS 3 no yes
equipment * O 0 1

* This offered equipment package is derived from JAR-OPS 3 Amendment 3. It does not
cover oxygen equipment and equipment required for over water operations. As the
national operating rule may differ from the JAR-OPS 3 Amendment 3, the operator has
then to contact its national authority to assure that the planned equipment configuration
is acceptable for the intended kind of operation.

P I N A O
Î
Use this code to find your required “PINAO“ packages on the following pages.
„ As a general guidance, use the diagram on the next page
„ One PINAO code may lead to different PINAO packages

IMPORTANT NOTES:
„ For IFR, there is no difference between “day” and “night”. Therefore only IFR “night” PINAO
packages are listed.
„ All possible PINAO codes are listed in the following pages.
„ For all intercom systems, the following impedances are standard: LOW IMPEDANCE Î
Microphone: 5 Ω (dynamic) / Headset: 8 Ω (military - EUROCOPTER typical)

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

Use this diagram to find the appropriate Avionics Solution

based on your individual PINAO selection.

PINAO

Ó Ô
VFR IFR
packages packages
(PINAO codes x0xxx) (PINAO codes x1xxx)

Ð Ð
MEGHAS / FCDS MEGHAS / FCDS
Glass Cockpit Glass Cockpit

Ð Ó Ô
Single/Dual Pilot VFR Single/Dual Pilot IFR Single Pilot
(PINAO codes 10xxx or (PINAO codes 31xxx IFR (single sided)
20xxx are included in 30xxx) including 21xxx) (PINAO codes 11xxx)

Ð Ð Ð
Avionics Solution B1 or B2
(see page 22)
Avionics Solution A1 or A2 Avionics Solution C
or
(see page 16) (see page 32)
Avionics Solution B3
(see page 28)

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

BLANK

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

4.1 VFR packages, based on Avionics Solutions A1 and A2

4.1.1 Instrument panel overviews

Solution A1 OR Solution A2

1 SMD 45 (copilot) PFD: Primary Flight Display 2 SMD 45 (pilot) PFD: Primary Flight Display
3 SMD 45 (pilot) ND: Navigation Display 4 GPS / NAV / COM (pilot) GNS 430 (GARMIN)
5 GPS / NAV / COM (copilot) GNS 430 GARMIN 6 Transponder GTX 330 (GARMIN)
7 ICP´s: MEGHAS Instrument Control Panels 8 RCU: MEGHAS Reconfiguration Control Unit
9 Audio / Comm. control unit ACU6100 (copilot) 10 Audio / Comm. control unit ACU 6100 (pilot)
11 SMD 45 (copilot) ND: Navigation Display 12 NAV / COM system control units
13 Transponder control unit

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

4.1.2 Contents of Avionics Solution A1

Document Commercial
reference reference Title

- B2300-004-00 Avionics Solution A1, consisting of:

Intercom System
08-16054-D B2341-190-01 Audio/Comm. control system (pilot and copilot) 2x ACU 6100
and Remote Electronic Unit REU 6100 (BECKER)
08-16054-D B2341-293-01 IC amplifier IC 3100-4-01 (BECKER)
Transponder
08-22031-B B2325-092-00 Transponder (Mode S) GTX 330 (GARMIN)
GPS/NAV/COM
08-43026-B B3442-092-00 GPS / NAV / COM system GNS 430, pilot
(interfaced with MEGHAS / FCDS)
08-43026-B B3442-091-00 GPS / NAV / COM system GNS 430, copilot / 2nd system
(VOR/ILS interfaced to MEGHAS / FCDS, GPS stand alone)
Display system
08-65005-B B3161-090-09 MEGHAS - Flight Control Display System (FCDS) Dual (4xSMD45)
Miscellaneous
08-99000-A B0000-150-04 Avionics Solution A1 interconnection / wiring
- B2577-001-00 Battery relocation to the rear

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

4.1.3 Contents of Avionics Solution A2

Document Commercial
reference reference Title
- B2300-001-00 Avionics Solution A2, consisting of:
VHF/AM COM
08-11026-A B2313-092-01 VHF-AM / COM system, pilot VCS-40A (CHELTON/WULFSBERG)
B2313-092-34 Control unit CD-402B, pilot for VCS-40A (CHELTON/WULFSBERG)
Intercom System
08-16054-D B2341-190-01 Audio/Comm. control system (pilot and copilot) 2x ACU 6100
and Remote Electronic Unit REU 6100 (BECKER)
08-16054-D B2341-293-01 IC amplifier IC 3100-4-01 (BECKER)

Transponder
08-22014-A B2325-092-06 Transponder (Mode S) MST 67A (HONEYWELL)
B2325-092-36 Transponder control unit PS 578A (HONEYWELL)

VOR/ILS/MKR receivers
08-26012-A B3432-092-01 VOR/ILS/MKR Navigation system, pilot VNS-41A
(CHELTON / WULFSBERG)
B3432-092-34 Control unit CD 412 B, pilot for VNS-41A
(CHELTON / WULFSBERG)

Display system
08-65005-B B3161-090-09 MEGHAS - Flight Control Display System (FCDS) Dual (4xSMD45)

Miscellaneous
08-99000-A B0000-150-01 Avionics Solution A2 interconnection / wiring
- B2577-001-00 Battery relocation to the rear

ON REQUEST:
- NVG friendly version of
Avionics Solutions
A1 and A2

- Exchange of 2x SMD45 on
copilot side to one SMD68

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

4.1.4 Minimum required equipment for Avionics Solutions A1 and A2

Minimum required equipment for Avionics Solutions A1 and A2 PINAO

Weight

30000
30010
30100
30110
(margin ± 3 %)
Document Commercial
reference reference Title kg lb
05-37018-A B6701-001-00 Copilot flight controls 6.5 14.3 X X X X
05-38011-A B3111-001-03 7“ copilot instrument panel with glare shield 1.7 3.7 X X X X
1
05-41005-A B2104-100-00 Bleed air heating system 14.2 31.3 X X X X
05-43008-A B2576-003-00 Ventilation for avionics compartment 0.7 1.5 X X X X
05-61005-A B2433-002-00 Battery, type Saft, ULM, 40 Ah 3.4 7.0
X X X X
instead of standard battery 27 Ah
05-68002-A B3343-003-00 Additional electrical unit for Landing & search 1.5 3.1
X X
light, 400 / 200 W, SX16 or mirrors
06-45026-A B3343-006-00 Landing & search light, 400 / 200 W 4.5 9.9 X X
08-00011-A B2300-004-00 Avionics Solution A1 75.7 166.9
or X X X X
08-00008-A B2300-001-00 Avionics Solution A2 80.7 177.9
08-21016-A B3441-090-04 Radar altimeter KRA 405B (HONEYWELL) 3.0 6.6 X X X
08-53003-A B2212-300-00 MEGHAS sensor kit 20.8 45.9 X X X X

1
Only required for operation below 10° OAT
The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
145.06.101.02 E 19
This 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 - 01/2006
 Technical Data

4.1.5 Possible add-ons for Avionics Solution A1 and A2

Possible add-ons for Avionics Solutions A1 and A2 PINAO

Weight

30000
30010
30100
30110
(margin ± 3 %)
Document Commercial
reference reference Title kg lb
06-67045-A B2563-801-06 ELT C406-N HM (ARTEX) incl. NAV. Option 3.9 8.6
(if Avionics Solution A2 is selected, a GPS X X X X
system is required)
08-21016-A B3441-090-04 Radar altimeter KRA 405B (HONEYWELL) 3.0 6.6 X
08-24016-B B3452-002-00 ADF system DFS-43A (CHELTON/WULFSB.) 7.3 16.1
B3452-092-34 ADF control unit CD-432B 1.5 3.3 X X X X
(CHELTON / WULFSBERG)
08-43012-A B3442-092-13 GPS NAV system 2101 I/O Approach plus 3.8 8.4
X X X X
NVG (FREE FLIGHT) 2
08-72002-B B2212-001-00 Automatic Flight Control System - AFCS 31.4 69.2
X X X X
(Radar altimeter required)
08-81025-A B3132-001-10 M’ARMS® Cockpit Voice and Flight Data 8.8 19.4
Recorder (CVFDR), fixed provisions
B3132-001-20 M’ARMS® Cockpit Voice and Flight Data 7.2 15.9 X X X X
Recorder (CVFDR), detachable parts, ground
station not included

4.1.6 Further avionics add-ons see chapter 6 page 45

2
Only possible for Avionics Solution A2
The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
145.06.101.02 E 20
This 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 - 01/2006
 Technical Data

BLANK

The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
145.06.101.02 E 21
This 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 - 01/2006
 Technical Data

4.2 Dual pilot or Single/Dual Pilot IFR, based on Avionics Sol. B1 and B2
4.2.1 Instrument panel overviews

Solution B1 OR Solution B2

1 SMD 45 (copilot) PFD: Primary Flight Display 2 SMD 45 (pilot) PFD: Primary Flight Display
3 SMD 45 (pilot) ND: Navigation Display 4 GPS / NAV / COM (pilot) GNS 430 (GARMIN)
5 GPS / NAV / COM (copilot) GNS 430 GARMIN 6 Transponder GTX 330 (GARMIN)
7 ICP´s: MEGHAS Instrument Control Panels 8 RCU: MEGHAS Reconfiguration Control Unit
9 Audio / Comm. control unit ACU6100 (copilot) 10 Audio / Comm. control unit ACU 6100 (pilot)
11 Autopilot control unit 12 SMD 45 (copilot) ND: Navigation Display
13 Transponder control unit 14 NAV / COM system control units
15 Marker beacon receiver / lights

The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
145.06.101.02 E 22
This 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 - 01/2006
 Technical Data

4.2.2 Contents of Avionics Solution B1

Document Commercial
reference reference Title
- B2300-005-00 Avionics Solution B1, consisting of
Intercom System
08-16054-D B2341-190-01 Audio/Comm. control system (pilot and copilot) 2x ACU 6100
and Remote Electronic Unit REU 6100 (BECKER)
08-16054-D B2341-293-01 IC amplifier IC 3100-4-01 (BECKER)

Transponder
08-22031-B B2325-092-00 Transponder (Mode S) GTX 330 (GARMIN)
DME
08-25016-A B3455-002-00 Distance Measuring Equipment DMS-44A
(CHELTON / WULFSBERG)

VOR/ILS/MKR receivers
08-26027-B B3431-090-01 Marker Beacon receiver / lights KR 21 (HONEYWELL)
GPS/NAV/COM
08-43026-B B3442-092-00 GPS / NAV / COM system GNS 430, pilot
(interfaced with MEGHAS / FCDS)
08-43026-B B3442-091-00 GPS / NAV / COM system GNS 430, copilot / 2nd system
(VOR/ILS interfaced to MEGHAS / FCDS, GPS stand alone)

Display system
08-65005-B B3161-090-09 MEGHAS - Flight Control Display System (FCDS) Dual (4xSMD45)

Miscellaneous
08-99000-A B0000-150-05 Avionics Solution B1 interconnection / wiring
- B2577-001-00 Battery relocation to the rear

The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
145.06.101.02 E 23
This 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 - 01/2006
 Technical Data

4.2.3 Contents of Avionics Solution B2

Document Commercial
reference reference Title
- B2300-002-00 Avionics Solution B2, consisting of:
VHF/AM COM

08-11026-A B2313-092-01 VHF-AM / COM system, pilot VCS-40A (CHELTON/WULFSBERG)

B2313-092-34 Control unit CD-402B, pilot for VCS-40A (CHELTON/WULFSBERG)
08-11026-A B2313-091-01 VHF-AM / COM system,copilot VCS-40A CHELTON/WULFSBERG
B2313-091-34 Control unit CD-402B,copilot for VCS-40A CHELTON/WULFSBERG
Intercom System

08-16054-D B2341-190-01 Audio/Comm. control system (pilot and copilot) 2x ACU 6100
and Remote Electronic Unit REU 6100 (BECKER)
08-16054-D B2341-293-01 IC amplifier IC 3100-4-01 (BECKER)

Transponder

08-22014-A B2325-092-06 Transponder (Mode S) MST 67A (HONEYWELL)

B2325-092-36 Transponder control unit PS 578A (HONEYWELL)

DME

08-25016-A B3455-002-00 Distance Measuring Equipment DMS-44A (CHELTON / WULFSB.)

VOR/ILS/MKR receivers

08-26012-A B3432-092-01 VOR/ILS/MKR Navigation system, pilot VNS-41A

(CHELTON / WULFSBERG)
B3432-092-34 Control unit CD 412 B, pilot for VNS-41A (CHELTON / WULFSB.)
08-26012-A B3432-091-01 VOR/ILS/MKR Navigation system, copilot VNS-41A
(CHELTON / WULFSBERG)
B3432-091-34 Control unit CD 412 B, copilot for VNS-41A (CHELTON / WULFSB.)

Display system

08-65005-B B3161-090-09 MEGHAS - Flight Control Display System (FCDS) Dual (4xSMD45)

Miscellaneous

08-99000-A B0000-150-02 Avionics Solution B2 interconnection / wiring

- B2577-001-00 Battery relocation to the rear

ON REQUEST:
- NVG friendly version of
Avionics Solutions
B1 and B2

- Exchange of 2x SMD45 on
copilot side to one SMD68

The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
145.06.101.02 E 24
This 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 - 01/2006
 Technical Data

4.2.4 Minimum required equipment for Avionics Solutions B1 and B2

Minimum required equipment for Avionics Solutions B1 and B2 PINAO

Weight

31100
31110
31111
(margin ± 3 %)
Document Commercial
reference reference Title kg lb

06-65005-A B2625-003-00 2nd portable fire extinguisher 2.6 5.7 X

05-37018-A B6701-001-00 Copilot flight controls 6.5 14.3 X X X

05-38011-A B3111-001-03 7“ copilot instrument panel with glare shield 1.7 3.7 X X X

05-39009-A B2514-003-01 Map case in copilot door 0.5 1.1 X X X

05-39011-A B3113-004-20 Illuminated chart holder, pilot side 1.1 2.4 X

05-41005-A B2104-100-00 Bleed air heating system 14.2 31.3 X X X

05-43008-A B2576-003-00 Ventilation for avionics compartment 0.7 1.6 X X X

05-61005-A B2433-002-00 Battery, type Saft, ULM, 40 Ah 3.4 7.5

X X X
instead of standard battery 27 Ah
05-68002-A B3343-003-00 Additional electrical unit for Landing & 1.5 3.3
X X X
search light, 400 / 200 W, SX16 or mirrors
06-45026-A B3343-006-00 Landing & search light, 400 / 200 W 4.5 9.9 X X X

06-67045-A B2563-801-06 ELT C406-N HM (ARTEX) incl. NAV. option 3.9 8.6
(if Avionics Solution B2 is selected, a GPS X
system is required)
08-00012-A B2300-005-00 Avionics Solution B1 83.3 183.6
or X X X

08-00009-A B2300-002-00 Avionics Solution B2 96.5 212.7

08-21016-A B3441-090-04 Radar altimeter KRA 405B (HONEYWELL) 3.0 6.6 X X X

08-53003-A B2212-300-00 MEGHAS sensor kit 20.8 45.9 X X X

08-72002-B B2212-001-00 Automatic Flight Control System - AFCS 31.4 69.2 X X X

08-81025-A B3132-001-10 M’ARMS® Cockpit Voice and Flight Data 8.8 19.4
Recorder (CVFDR), fixed provisions
B3132-001-20 M’ARMS® Cockpit Voice and Flight Data 7.2 15.9 X
Recorder (CVFDR), detachable parts, ground
station not included

The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
145.06.101.02 E 25
This 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 - 01/2006
 Technical Data

4.2.5 Possible add-ons for Avionics Solution B1 and B2

Possible add-ons for Avionics Solutions B1 and B2 PINAO

Weight

31100
31110
31111
(margin ± 3 %)
Document Commercial
reference reference Title kg lb
06-67045-A B2563-801-06 ELT C406-N HM (ARTEX) incl. NAV. Option 3.9 8.6
(if Avionics Solution B2 is selected, a GPS X X
system is required)
08-24016-A B3452-002-00 ADF system DFS-43A (CHELTON/WULFSB.) 7.3 16.1
B3452-092-34 ADF control unit CD-432B 1.5 3.3 X X X
(CHELTON / WULFSBERG)
08-43012-A B3442-092-13 GPS NAV system 2101 I/O Approach plus – 3.8 8.4
X X X
NVG (FREE FLIGHT) 3
08-81025-A B3132-001-10 M’ARMS® Cockpit Voice and Flight Data 8.8 19.4
Recorder (CVFDR), fixed provisions
B3132-001-20 M’ARMS® Cockpit Voice and Flight Data 7.2 15.9 X X
Recorder (CVFDR), detachable parts, ground
station not included

4.2.6 Further avionics add-ons see chapter 6 page 41

3
Only possible for Avionics Solution B2
The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
145.06.101.02 E 26
This 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 - 01/2006
 Technical Data

BLANK

The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
145.06.101.02 E 27
This 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 - 01/2006
 Technical Data

4.3 Dual pilot or Single/Dual Pilot IFR with Dual FMS/NMS (Av. Sol. B3)
4.3.1 Instrument panel overview

1 SMD 45 (copilot) PFD: Primary Flight Display

2 SMD 45 (pilot) PFD: Primary Flight Display
3 Autopilot (AFCS) control unit (minimum required equipment)
4 Audio / Comm. control unit ACU 6100 (pilot)
5 SMD 45 (pilot) ND: Navigation Display
6 Audio / Comm. control unit ACU 6100 (copilot)
7 RCU : MEGHAS Reconfiguration Control Unit
8 Navigation Management System CMA-9000 (pilot)
9/10 ICP´s: MEGHAS Instrument Control Panels
11 Navigation Management System CMA-9000 (copilot)
12 SMD 45 (copilot) ND: Navigation Display

The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
145.06.101.02 E 28
This 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 - 01/2006
 Technical Data

4.3.2 Contents of Avionics Solution B3

Document Commercial
reference reference Title
- B2300-006-00 Avionics Solution B3, consisting of:
VHF/AM COM

08-11026-A B2313-092-01 VHF-AM / COM system, pilot VCS-40A (CHELTON/WULFSBERG)

B2313-092-34 Control unit CD-402B, pilot for VCS-40A (CHELTON/WULFSBERG)
08-11026-A B2313-091-01 VHF-AM / COM system, copilot VCS-40A CHELTON/WULFSBERG
Intercom System

08-16054-D B2341-190-01 Audio/Comm. control system (pilot and copilot) 2x ACU 6100
and Remote Electronic Unit REU 6100 (BECKER)
08-16054-D B2341-293-01 IC amplifier IC 3100-4-01 (BECKER)

Transponder

08-22014-A B2325-092-06 Transponder (Mode S) MST 67A (HONEYWELL)

DME

08-25016-A B3455-002-00 Distance Measuring Equipment DMS-44A (CHELTON / WULFSB.)

VOR/ILS/MKR receivers

08-26012-A B3432-092-01 VOR/ILS/MKR Navigation system, pilot VNS-41A

(CHELTON / WULFSBERG)
B3432-092-34 Control unit CD 412 B, pilot for VNS-41A (CHELTON / WULFSB.)
08-26012-A B3432-091-01 VOR/ILS/MKR Navigation system, copilot VNS-41A
(CHELTON / WULFSBERG)
FMS

08-44026-A B2312-026-40 Flight-/ Navigation- / Radio management system (CMA 9000) - 4

Dual (CMC ELECTRONICS)
B3442-004-04 GPS sensor module CMA-3024 for CMA-9000 (CMC ELECTRONICS)

Display system

08-65005-B B3161-090-09 MEGHAS - Flight Control Display System (FCDS) Dual (4xSMD45)

Miscellaneous

08-99000-A B0000-150-06 Avionics Solution B3 interconnection / wiring

- B2577-001-00 Battery relocation to the rear

ON REQUEST:
- NVG friendly version of
Avionics Solution B3

- Exchange of 2x SMD45 on
copilot side to one SMD68

4
VHF-AM COM, VHF-NAV and ATC transponder are controlled via CMA-9000
The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
145.06.101.02 E 29
This 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 - 01/2006
 Technical Data

4.3.3 Minimum required equipment for Avionics Solution B3

Minimum required equipment for Avionics Solutions B3 PINAO

Weight

31100
31110
31111
(margin ± 3 %)
Document Commercial
reference reference Title kg lb
06-65005-A B2625-003-00 2nd portable fire extinguisher 2.6 5.7 X
05-37018-A B6701-001-00 Copilot flight controls 6.5 14.3 X X X
05-38011-A B3111-001-03 7“ copilot instrument panel with glare shield 1.7 3.7 X X X
05-39009-A B2514-003-01 Map case in copilot door 0.5 1.1 X X X
05-39011-A B3113-004-20 Illuminated chart holder, pilot side 1.1 2.4 X
05-41005-A B2104-100-00 Bleed air heating system 14.2 31.3 X X X
05-43008-A B2576-003-00 Ventilation for avionics compartment 0.7 1.6 X X X
05-61005-A B2433-002-00 Battery, type Saft, ULM, 40 Ah 3.4 7.5
X X X
instead of standard battery 27 Ah
05-68002-A B3343-003-00 Additional electrical unit for Landing & 1.5 3.3
X X X
Search light, 400 / 200 W, SX16 or mirrors
06-45026-A B3343-006-00 Landing & Search light, 400 / 200 W 4.5 9.9 X X X
06-67045-A B2563-801-06 ELT C406-N HM (ARTEX) incl. NAV. option 3.9 8.6 X
08-00013-A B2300-006-00 Avionics Solution B3 112.0 246.9 X X X
08-21016-A B3441-090-04 Radar altimeter KRA 405B (HONEYWELL) 3.0 6.6 X X X
08-53003-A B2212-300-00 MEGHAS sensor kit 20.8 45.9 X X X
08-72002-B B2212-001-00 Automatic Flight Control System - AFCS 31.4 69.2 X X X
08-81025-A B3132-001-10 M’ARMS® Cockpit Voice and Flight Data 8.8 19.4
Recorder (CVFDR), fixed provisions
B3132-001-20 M’ARMS® Cockpit Voice and Flight Data 7.2 15.9 X
Recorder (CVFDR), detachable parts, ground
station not included

The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
145.06.101.02 E 30
This 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 - 01/2006
 Technical Data

4.3.4 Possible add-ons for Avionics Solution B3

Possible add-ons for Avionics Solutions B3 PINAO

Weight

31100
31110
31111
(margin ± 3 %)
Document Commercial
reference reference Title kg lb
06-67045-A B2563-801-06 ELT C406-N HM (ARTEX) incl. NAV. Option 3.9 8.6 X X
08-24016-A B3452-002-00 ADF system DFS-43A 7.3 16.1
(CHELTON / WULFSBERG) X X X
controlled via CMA-9000
08-81025-A B3132-001-10 M’ARMS® Cockpit Voice and Flight Data 8.8 19.4
Recorder (CVFDR), fixed provisions
B3132-001-20 M’ARMS® Cockpit Voice and Flight Data 7.2 15.9 X X
Recorder (CVFDR), detachable parts, ground
station not included

4.3.5 Further avionics add-ons see chapter 6 page 45

The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
145.06.101.02 E 31
This 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 - 01/2006
 Technical Data

4.4 Single Pilot IFR, based on Avionics Solution C

4.4.1 Instrument panel overview

1 SMD 45 (pilot) PFD: Primary Flight Display

2 Back-up DME indicator SD 442 B
3 Autopilot control unit (minimum required equipment)
4 Audio / Comm. control unit ACU 6100 (1st system)
5 Audio / Comm. control unit ACU 6100 (2nd system)
6 RCU: MEGHAS Reconfiguration Control Unit
7 Back-up indicator (CDI) KI 204
8 SMD 45 (pilot) ND: Navigation Display
9 ICP´s: MEGHAS Instrument Control Panels

The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
145.06.101.02 E 32
This 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 - 01/2006
 Technical Data

4.4.2 Contents of Avionics Solution C

Document Commercial
reference reference Title
- B2300-003-00 Avionics Solution C, consisting of:
VHF/AM COM

08-11026-A B2313-092-01 VHF-AM / COM system, pilot VCS-40A (CHELTON/WULFSBERG)

B2313-092-34 Control unit CD-402B, pilot for VCS-40A (CHELTON/WULFSBERG)
08-11026-A B2313-091-01 VHF-AM / COM system, copilot VCS-40A CHELTON/WULFSBERG
B2313-091-34 Control unit CD-402B,copilot for VCS-40A CHELTON/WULFSBERG
Intercom System

08-16054-D B2341-190-01 Audio/Comm. control system (pilot and copilot) 2x ACU 6100
and Remote Electronic Unit REU 6100 (BECKER)
08-16054-D B2341-293-01 IC amplifier IC 3100-4-01 (BECKER)

Transponder

08-22014-A B2325-092-06 Transponder (Mode S) MST 67A (HONEYWELL)

B2325-092-36 Transponder control unit PS 578A (HONEYWELL)

DME

08-25016-A B3455-002-00 Distance Measuring Equipment DMS-44A (CHELTON / WULFSB.)

VOR/ILS/MKR receivers

08-26012-A B3432-092-01 VOR/ILS/MKR Navigation system, pilot VNS-41A

(CHELTON / WULFSBERG)
B3432-092-34 Control unit CD 412 B, pilot for VNS-41A (CHELTON / WULFSB.)
08-26012-A B3432-091-01 VOR/ILS/MKR Navigation system, copilot VNS-41A
(CHELTON / WULFSBERG)
B3432-091-34 Control unit CD 412 B, copilot for VNS-41A (CHELTON / WULFSB.)
08-26012-A B0000-200-12 Back-up CDI KI 204 (HONEYWELL) and
Back-up DME indicator SD 442 B (CHELTON / WULFSBERG)

Display system

08-65005-B B3161-092-02 MEGHAS - Flight Control Display System (FCDS) Single

(2xSMD45)

Miscellaneous

08-99000-A B0000-150-03 Avionics Solution C interconnection / wiring

- B2577-001-00 Battery relocation to the rear

ON REQUEST:
- NVG friendly version of Avionics Solution C
- SP IFR with Single sided GARMIN GNS430 version

The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
145.06.101.02 E 33
This 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 - 01/2006
 Technical Data

4.4.3 Minimum required equipment for Avionics Solution C

Minimum required equipment for Avionics Solutions C PINAO

Weight

11100
11110
11111
(margin ± 3 %)
Document Commercial
reference reference Title kg lb
06-65005-A B2625-003-00 2nd portable fire extinguisher 2.6 5.7 X
05-39011-A B3113-004-20 Illuminated chart holder, pilot side 1.1 2.4 X
05-41005-A B2104-100-00 Bleed air heating system 14.2 31.3 X X X
05-43008-A B2576-003-00 Ventilation for avionics compartment 0.7 1.6 X X X
05-61005-A B2433-002-00 Battery, type Saft, ULM, 40 Ah 3.4 7.5
X X X
instead of standard battery 27 Ah
05-68002-A B3343-003-00 Additional electrical unit for Landing & 1.5 3.3
X X X
Search light, 400 / 200 W, SX16 or mirrors
06-45026-A B3343-006-00 Landing & Search light, 400 / 200 W 4.5 9.9 X X X
06-67045-A B2563-801-06 ELT C406-N HM (ARTEX) incl. NAV. option 3.9 8.6
X
(GPS system required)
08-00010-A B2300-003-00 Avionics Solution C 93.2 205.5 X X X
08-21016-A B3441-090-04 Radar altimeter KRA 405B (HONEYWELL) 3.0 6.6 X X X
08-53003-A B2212-300-00 MEGHAS sensor kit 20.8 45.9 X X X
08-72002-B B2212-001-00 Automatic Flight Control System - AFCS 31.4 69.2 X X X
08-81025-A B3132-001-10 M’ARMS® Cockpit Voice and Flight Data 8.8 19.4
Recorder (CVFDR), fixed provisions
B3132-001-20 M’ARMS® Cockpit Voice and Flight Data 7.2 15.9 X
Recorder (CVFDR), detachable parts, ground
station not included

The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
145.06.101.02 E 34
This 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 - 01/2006
 Technical Data

4.4.4 Possible add-ons for Avionics Solution C

Possible add-ons for Avionics Solutions C PINAO

Weight

11100
11110
11111
(margin ± 3 %)
Document Commercial
reference reference Title kg lb
06-67045-A B2563-801-06 ELT C406-N HM (ARTEX) incl. NAV. Option 3.9 8.6
X X
(GPS system required)
08-24016-A B3452-002-00 ADF system DFS-43A 7.3 16.1
(CHELTON / WULFSBERG)
X X X
B3452-092-34 ADF control unit CD-432B 1.5 3.3
(CHELTON / WULFSBERG)
08-43012-A B3442-092-13 GPS NAV system 2101 I/O Approach plus – 3.8 8.4
X X X
NVG (FREE FLIGHT)
08-81025-A B3132-001-10 M’ARMS® Cockpit Voice and Flight Data 8.8 19.4
Recorder (CVFDR), fixed provisions
B3132-001-20 M’ARMS® Cockpit Voice and Flight Data 7.2 15.9 X X
Recorder (CVFDR), detachable parts, ground
station not included

4.4.5 Further avionics add-ons see chapter 6 page 45

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

BLANK

The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
145.06.101.02 E 36
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 Technical Data

5 Cabin arrangement

5.1 Passenger transport

5.1.1 Eight (8) corporate passenger cabin configuration

Weight
(margin ± 3 %)

Document Commercial
reference reference Title kg lb
06-65005-A B2625-003-00 2nd portable fire extinguisher (cabin floor mounted) 2.6 5.7

07-27003-A B2523-002-00 Club seating (8 pax), energy absorbing individual seats 90.4 199.3

07-81021-A B2512-100-00 Modification of pilot and copilot seat with leather, 0.0 0.0
restraint system in matching color
07-81021-A B2523-100-00 Modification of passenger seats (8 club seats) with leather, 0.0 0.0
restraint system in matching color
07-83008-A B2525-001-00 Carpet for cockpit, cabin and cargo compartment 14.5 31.9

5.1.2 Variations of the corporate passenger cabin configuration

In order to adapt to individual needs, above corporate package can be modified on customer’s
request. Possible variations would include cabinets, leather covered interior and swiveling seats.

The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
145.06.101.02 E 37
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 Technical Data

5.2 EMS equipment

5.2.1 Basic EMS kit - Aerolite (STC)

5.2.1.1 Content
Weight
(margin ± 3 %)

Document Commercial
reference reference Title kg lb
07-70010-A AG-X982-4c Basic EMS kit - Aerolite (STC) 140.5 309.1
consisting of:
„ Cabin Floor Lining Kit
„ Stationary Med Seat RH
„ Stationary Med Seat LH
„ Primary Stretcher Kit
„ Center Stowage Cabinet
„ Med Supply Unit
„ Med Oxygen System 3x3L
„ Med Vacuum System (ATMOPORT N)
„ IV Hook
„ Strap Down Web
„ Medical Retainer Set
„ Cover for 1 (one) passenger seat

5.2.1.2 Minimum requirement equipment

Weight
(margin ± 3 %)

Document Commercial
reference reference Title kg lb
05-67015-A B8522-001-00 Additional electrical interface for mission equipment 0.8 1.6
05-68001-A B3113-011-00 Additional circuit breaker panel 5.2 11.5
07-27003-A B2523-002-22 1 passenger club seat, middle row, RH 11.7 25.7
07-75020-A B2514-300-00 Airline style attachment rails (LH and RH cabin ceiling) 3.4 7.5
07-90016-A B2524-008-11 Multi-purpose fittings in cabin, LH 3.0 6.6
07-90016-A B2524-008-12 Multi-purpose fittings in cabin, RH 3.0 6.6

The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
145.06.101.02 E 38
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 Technical Data

5.2.2 Mid range EMS kit - Aerolite (STC)

5.2.2.1 Content
Weight
(margin ± 3 %)

Document Commercial
reference reference Title kg lb
07-70011-A AG-X982-5c Mid range EMS kit - Aerolite (STC) 182.0 400.4
consisting of:
„ Cabin Floor Lining Kit
„ Slide&Swivel Med Seat RH
„ Slide&Swivel Med Seat LH
„ Primary Stretcher Kit
„ Secondary Stretcher Kit
„ Center Stowage Cabinet
„ Rear Door Stowage Box
„ Med Supply Unit
„ Overhead Compartment
„ Med Oxygen System 3x3L
„ Lighting System
„ Med Vacuum System (ATMOPORT N)
„ IV Hook
„ Strap Down Web
„ Medical Retainer Set
„ Cover for 1 (one) passenger Seat

5.2.2.2 Minimum requirement equipment

Weight
(margin ± 3 %)

Document Commercial
reference reference Title kg lb
05-67015-A B8522-001-00 Additional electrical interface for mission equipment 0.8 1.6
05-68001-A B3113-011-00 Additional circuit breaker panel 5.2 11.5
07-27003-A B2523-002-22 1 passenger club seat, middle row, RH 11.7 25.7
07-75020-A B2514-300-00 Airline style attachment rails (LH and RH cabin ceiling) 3.4 7.5
07-90016-A B2524-008-11 Multi-purpose fittings in cabin, LH 3.0 6.6
07-90016-A B2524-008-12 Multi-purpose fittings in cabin, RH 3.0 6.6
The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
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 Technical Data

5.2.3 High sophisticated EMS kit - Aerolite (STC)

5.2.3.1 Content
Weight
(margin ± 3 %)

Document Commercial
reference reference Title kg lb
07-70014-A AG-X982-6c High sophisticated EMS kit - Aerolite (STC) 222.6 489.7
consisting of:
„ Integral Floor Kit
„ Slide&Swivel Med Comfort Seat RH
„ Slide&Swivel Med Comfort Seat LH
„ Intensive Care Stretcher
„ Center Stowage Cabinet
„ Rear Door Stowage Box
„ Med Supply Unit
„ Overhead Compartment
„ Med Oxygen System 3x3L
„ Med Air System 1x3L
„ Lighting System
„ Lighting Battery Kit
„ Med Vacuum System (ATMOPORT N)
„ IV Hook
„ Strap Down Web
„ Medical Retainer Set
„ Cover for 1 (one) passenger Seat

5.2.3.2 Minimum requirement equipment

Weight
(margin ± 3 %)

Document Commercial
reference reference Title kg lb
05-67015-A B8522-001-00 Additional electrical interface for mission equipment 0.8 1.6
05-68001-A B3113-011-00 Additional circuit breaker panel 5.2 11.5
07-27003-A B2523-002-22 1 passenger club seat, middle row, RH 11.7 25.7
07-75020-A B2514-300-00 Airline style attachment rails (LH and RH cabin ceiling) 3.4 7.5
07-90016-A B2524-008-11 Multi-purpose fittings in cabin, LH 3.0 6.6
07-90016-A B2524-008-12 Multi-purpose fittings in cabin, RH 3.0 6.6
The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
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 Technical Data

6 Optional equipment

6.1 Shopping list

Weight
General Equipment
(margin ± 3 %)

Document Commercial
reference reference Title kg lb
05-02020-A B1111-002-00 Two-color external painting instead of single color painting 2.0 4.4

05-02020-A B1111-003-00 Multicolor external painting instead of single color painting 3.0 6.6

05-02029-A B1112-001-00 High visibility paint scheme for main rotor blades 0.0 0.0
(3 concentric rings on top of blades)
05-21016-A B8541-001-10 Wire strike protection system, fixed provisions 3.8 8.4

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

05-22004-A B7924-001-00 Fuzz burner for engines 1.1 2.4

05-22005-A B7924-002-00 Fuzz burner for tail rotor and intermediate gearbox 1.1 2.4
(chip detectors included)
05-22006-A B7924-003-00 Chip detectors tail rotor and intermediate gearbox 0.9 2.0

05-22015-A B6343-001-00 Fuzz burner for main transmission 1.1 2.4

05-22016-A B7922-001-00 Scavenge oil filter 1.8 4.0

05-23007-A B7165-002-00 Engine compressor washing device 1.7 3.7

05-25017-A B7161-001-10 Sand filter system, fixed provisions 5.2 11.5

05-25017-A B7161-001-20 Sand filter system, detachable parts 32.7 72.1

05-31029-A B2514-002-00 Tinted sun shades for cockpit windshield roof section 2.1 4.6

05-31030-A B2524-030-10 IFR - training screen, fixed provisions 0.1 0.2

05-31030-A B2524-030-20 IFR - training screen, detachable parts 2.1 4.6

05-31032-A B5213-001-11 Sliding door fastener, intermediate and max. position, LH 0.4 0.9
(required for flight with open doors)
05-31032-A B5213-001-21 Sliding door fastener, intermediate and max. position, RH 0.4 0.9
(required for flight with open doors)
05-31034-A B5633-001-10 Window in clam-shell door, LH 0.3 0.7

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

05-31046-A B5632-002-00 Push-out cabin windows 3.0 6.6

05-36008-A B8532-002-30 Multifunction step LH for standard landing gear (instead of 3.4 7.5
standard boarding step)
05-36008-A B8532-002-40 Multifunction step RH for standard landing gear (instead of 3.4 7.5
standard boarding step)
05-37018-A B6701-001-00 Copilot flight controls 6.5 14.3

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

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

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

Weight
General Equipment (contd.)
(margin ± 3 %)

Document Commercial
reference reference Title kg lb
05-39010-A B3111-001-10 Map case on instrument panel glare shield 0.6 1.3

05-39011-A B3113-004-10 Illuminated chart holder, copilot side 1.1 2.4

05-39011-A B3113-004-20 Illuminated chart holder, pilot side 1.1 2.4

05-41005-A B2104-100-00 Bleed air heating system 14.2 31.3

05-42022-A B2105-001-00 Air conditioning/cooling system – Metro (STC) 51.2 112.9

05-61005-A B2433-002-00 Battery, type “Saft”, ULM, 40 Ah, 24 V instead of standard battery 3.4 7.5

05-61005-A B2433-003-00 Battery, type “Saft”, ULM, 44 Ah, 24 V instead of standard battery 6.9 15.2

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

05-68002-A B3343-003-00 Additional electrical unit for Landing & search light, 400 / 200 W, 1.5 3.3
SX16 or mirrors
05-81034-A B2818-100-10 Internal long range fuel tank system, fixed provisions 2.3 5.1

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

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

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

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

05-92015-A B6611-001-30 Main rotor blade folding, ground handling kit 15.0 33.1

05-93009-A B8544-001-10 Lashing points (wind speeds up to 60 kts) 1.3 2.8

05-93010-A B8544-002-00 Lashing points (wind speeds up to 100 kts), incl. 0.9 kg of GSE 4.4 9.7

Weight
Specific Mission Equipment
(margin ± 3 %)

Document Commercial
reference reference Title kg lb
06-11023-A B3272-001-20 Snow skids 22.8 50.3

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

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

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

(in combination with emergency floats 12.4 kg / 27.3 lb,
if fixed prov. on both LH and RH side, weight has to be checked)
06-21019-A B8512-001-11 External hoist, RH, fixed provisions 10.5 23.2
(in combination with emergency floats 12.8 kg / 28.2 lb,
if fixed prov. on both LH and RH side, weight has to be checked)
06-21019-A B8512-001-20 External hoist (without hook), detachable parts 65.2 143.7
(incl. 1 week winch operator training)
06-21019-A B8512-001-21 External hoist hook 3.6 7.9

The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
145.06.101.02 E 42
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 Technical Data

Weight
Specific Mission Equipment (contd.)
(margin ± 3 %)

Document Commercial
reference reference Title kg lb
06-21020-A B8512-002-11 External hoist observation light, LH, fixed provisions 0.7 1.5

06-21020-A B8512-002-12 External hoist observation light, RH, fixed provisions 0.7 1.5

06-21020-A B8512-002-20 External hoist observation light, detachable parts 0.8 1.7

06-21026-A B8512-001-22 External hoist hook damper floating device 0.4 0.9

06-24011-A B8534-003-11 Rope-down device for 2 persons, LH, fixed provisions 2.2 4.8
(in combination with emergency floats 4.9 kg / 10.8 lb)
06-24011-A B8534-003-12 Rope-down device for 2 persons, RH, fixed provisions 2.2 4.8
(in combination with emergency floats 4.9 kg / 10.8 lb)
06-24011-A B8534-003-21 Rope-down device for 2 persons, LH, detachable parts 15.2 33.5
(operation cannot be civil certified)
06-24011-A B8534-003-22 Rope-down device for 2 persons, RH, detachable parts 15.2 33.5
(operation cannot be civil certified)
06-26012-A B8511-002-10 Cargo hook mirrors, fixed provisions 0.5 1.1
(additional electrical unit required)
06-26012-A B8511-002-20 Cargo hook mirrors, detachable parts 3,8 8,4

06-26012-A B8511-002-21 Cover for cargo hook mirrors (required for operation at night with 0.4 0.9
search or landing lights in use)
06-27028-A B8511-005-10 Cargo hook system (sling type), fixed provisions 9.3 20.5

06-27028-A B8511-005-20 Cargo hook system (sling type), detachable parts 8.9 19.6

06-27029-A B8511-003-10 Cargo hook weighing system (sling type), fixed provisions 0.4 0.9

06-27029-A B8511-003-20 Cargo hook weighing system (sling type), detachable parts 1.8 4.0

06-27030-A B8511-008-10 Double cargo hook (fixed beam), fixed provisions 6.9 15.2
(additional circuit breaker panel required)
06-27030-A B8511-008-20 Double cargo hook system (fixed beam), detachable parts 21.4 47.2

06-27031-A B8511-091-10 Double cargo hook weighing system, fixed provisions 0.4 0.9

06-27031-A B8511-091-20 Double cargo hook weighing system, detachable parts 1.8 4.0

06-31014-A B8531-001-00 External loudspeaker system with siren 10.1 22.3

06-40001-A B3349-001-00 Tail flood lights for tail rotor and clam-shell doors 1.3 2.9
(additional circuit breaker panel required)
06-41015-A B3342-001-00 LED Anti-Collision Light (ACL) instead of standard version 0.0 0.0

06-42018-A B3343-001-50 Additional landing light, cross tube mounted LH, 250 W 1.2 2.6
(additional circuit breaker panel required)
06-45026-A B3343-006-00 Landing & search light 400/200 W, NVG compatible 4.5 9.9
(additional electrical unit required)
06-45027-A B3346-004-10 Search light SX16, LH multi function step mounted, fixed 5.3 11.7
provisions (additional electrical unit required)
06-45027-A B3346-004-20 Search light SX16, LH multi function step mounted, detachable 10.2 22.5
parts (w/o vendor parts)
06-45027-A B3346-500-20 Search light SX16, with infrared filter, vendor parts 29.8 65.7

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

Weight
Specific Mission Equipment (contd.)
(margin ± 3 %)

Document Commercial
reference reference Title kg lb
06-46004-A B3344-001-10 Strobe lights, white 2.0 4.4

06-61017-A B3215-001-10 Emergency floats, fixed provisions 1.8 4.0

06-61017-A B3215-001-20 Emergency floats, detachable parts 64.3 141.8

06-65003-A B2566-001-00 Emergency hammer 0.2 0.5

06-65005-A B2625-003-00 2nd portable fire extinguisher (cabin floor mounted) 2.6 5.7

06-66002-A B3353-015-00 Helicopter Emergency Egress Lighting (HEEL) 4.4 9.7

06-66011-A B3353-006-00 Illuminated signs "NO SMOKING/FASTEN SEAT BELT" 0.2 0.4

06-67048-A B2563-031-00 Underwater Locator Beacon (ULB) 0.3 0.7

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

06-69006-A B2341-006-61 Voice alert generator (611-014) 0.5 1.1

06-71007-A B2524-003-10 Separation curtain for cockpit / cabin (NVG compatible), fixed 0.1 0.2
provisions
06-71007-A B2524-003-20 Separation curtain for cockpit / cabin (NVG compatible), 1.1 2.4
detachable parts
06-81010-A B8503-001-10 Fire extinguishing bucket attachment (Bambi Bucket), fixed prov. 0.8 1.8
(cargo hook system and add. circuit breaker panel required)

Weight
Interior Layout
(margin ± 3 %)

Document Commercial
reference reference Title kg lb
07-00017-A B2581-002-20 Comfort improvement kit 23.9 52.7

07-15014-A B2512-003-10 Height adjustable pilot seat instead of standard pilot seat 3.7 8.2

07-15014-A B2512-003-20 Height adjustable copilot seat instead of standard copilot seat 3.7 8.2

07-27003-A B2523-002-00 Club seating, 8 pax configuration - other seating arrangements 90.4 199.3
on request
(depending on the number of pax seats installed, a second
portable fire extinguisher in the cabin may be required)
07-27009-A B2522-009-20 High-density seating, 9 pax configuration - SIMULA (STC) 111.3 245.4

07-27009-A B2522-010-20 High-density seating, 10 pax configuration - SIMULA (STC) 122.0 269.0
Other seating arrangement on request
(depending on the number of pax seats installed, a second
portable fire extinguisher in the cabin may be required)
07-30019-B B2581-001-00 Basic soundproofing kit 6.0 13.2

07-30019-B B2581-003-00 Enhanced soundproofing kit tbd tbd

07-40010-A B2513-220-00 Washable floor covering for cockpit, cabin and cargo 14.1 31.1
compartment

The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
145.06.101.02 E 44
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 Technical Data

Weight
Interior Layout (contd.)
(margin ± 3 %)

Document Commercial
reference reference Title kg lb
07-50032-A B5212-001-30 Jettisonable sliding doors 0.0 0.0

07-50033-A B5212-001-00 Jettisonable cockpit doors 0.6 1.3

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

07-60019-A B2552-001-00 Cargo tie-down net for cabin 4.2 9.3

07-75020-A B2514-300-00 Airline-style attachment rails (LH and RH cabin ceiling) 3.4 7.5

07-90016-A B2524-008-11 Multi-purpose fittings in cabin, LH 4.0 8.8

07-90016-A B2524-008-12 Multi-purpose fittings in cabin, RH 4.0 8.8

6.2 Shopping list avionics

Weight
Avionics
(margin ± 3 %)

Document Commercial
reference reference Title kg lb
5
08-12028-A B4321-092-01 Tactical radio NPX 138N (NAT) 2.3 5.1

08-15031-A B2319-001-10 Fixed provisions for GSM phone 2.4 5.3

(antenna, 28VDC, interfacing to ICS for panel mount radio)
08-15511-A B2315-092-00 IRIDIUM satellite phone AEROPHONE (AERODATA) 4.0 8.8

08-16054-D B2341-193-01 Audio/Comm. control system (PAX/3rd station) ACU 6100 2.0 4.4
6
(BECKER) standard version
(installed in RH passenger cabin ceiling)
08-16054-D B2341-845-00 Audio/Comm. control system (PAX/3rd station) ACU 6100 1.4 3.1
6
(BECKER) EMS version
(delivered as loose item, incl. connector interface in LH
passenger cabin ceiling)
08-17041-A B2331-001-00 Cabin loudspeaker 2.3 5.1
(enhanced soundproofing kit required)
08-17043-A B2332-001-00 Passenger address system (DP4100 BECKER) 1.6 3.5
(cabin loudspeaker with enhanced soundproofing kit required)
08-18023-A B2315-001-10 Headset H 10-76 (David Clark), low impedance, spiral wire 0.5 1.1

08-18023-A B2315-001-14 Headset H 10-76 ANR/ENC (David Clark), low impedance, 0.9 2.0
spiral wire

5
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 will assist the customer in
obtaining certification or acceptance approval in his country.
6
Only available for EMS packages Aerolite Middle range and high sophisticated
The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
145.06.101.02 E 45
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 Technical Data

Weight
Avionics (contd.)
(margin ± 3 %)

Document Commercial
reference reference Title kg lb
08-31037-A B3443-004-10 Search And Rescue weather radar RDR1600 (Telephonics), f.p. 1.7 3.8
B3443-004-20 Search And Rescue weather radar RDR1600 (Telephonics), d.p. 14.2 31.3
B2571-001-00 + Radar radome for RDR 1600 4.7 10.4
05-62011-A B2420-004-00 + AC system 1.5 3.3
(Video Radar Unit (VRU) required → see below)
08-35020-A B2327-001-01 Traffic Advisory System TAS 9900BX with 3" indicator (RYAN) 11.0 24.3
7
08-46013-A B3168-090-01 Digital moving Map DKG 3 (DORNIER), basic version 2.9 6.4
(GPS required)
enhanced options and maps on request
08-46021-B B3168-092-04 Digital moving Map EURONAV IV - RN6 (EURO AVIONICS) 6.6 14.6
7
interfaced with FCDS / MEGHAS, basic version
(VRU and GPS required → see below)
enhanced options and maps on request
08-53005-A B3424-000-00 AHRS Free Steering Mode 0.5 1.1

08-65006-A B3443-010-00 Video Radar Unit (VRU) for weather radar or digital moving map 4.9 10.8
indication on FCDS
08-83008-A B3171-001-10 M’ARMS® Usage Monitoring System (UMS), incl. SSQAR 4.5 9.9
option, fixed provisions
B3171-001-20 M’ARMS® Usage Monitoring System (UMS), incl. SSQAR 3.1 6.8
option, detachable parts ground station not included
AFCS required
(in combination with CVFDR: 1.7 kg / 3.8 lb)

Tactical radios

Fixed provisions can be offered on request

NVG Equipment

Different solutions can be offered on request:

All avionics solutions can be NVG modified

NVG compatible cabin and cargo compartment lighting
NVG friendly external lighting kit, comprising position and anti-collision lights
Landing & search light 400/200 W, NVG compatible

Broadcast, Thermal Imaging and Video Surveillance Equipment

“Ultraforce II” (FLIR Systems) on request

7
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 will assist the customer in
obtaining certification or acceptance approval in his country.

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

6.3 Offshore

Various equipment can be offered on request:

• Automatic Deployable ELT

• Emergency floats
• Life raft installation
• Jettisonable cockpit door
• AHRS Free Steering Mode
• Helicopter Emergency Egress Lighting (HEEL)
• Underwater Locator Beacon
• Search and weather radar
• Traffic Advisory System TAS 9900BX
• Cabin loudspeaker / Passenger address system
• Corrosion prevention treatment for offshore operation
• Push-out cabin windows

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

BLANK

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

7 Table of constraints

7.1 General Checklist for Incompatibilities:

„ Detachable parts require the related fixed provisions

„ Only one to be selected:

- External painting
- Battery
- Cargo hook system

„ All recommended configurations in Chapter 4 exclude each other. Mixed Configurations are
possible but have to be individually checked.

„ For B2327-001-01 Traffic Advisory System TAS 9900BX, the incompatibilities have to be checked.

Commercial Commercial
reference
Title MSG reference
Title

The protective Cargo hook mirrors,

B8511-002-20
capability is detachable parts
Wire Strike Protection
significantly B2571-001-00 Radar radome
B8541-001-20 System, (WSPS)
degraded in
detachable parts
combination Traffic Advisory
B2327-001-01
with System TAS 9900BX

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

7.2 Legend of the following chart

EXL Impossibility of simultaneous fitment of the fixed parts of 2 items of equipment
NSF Total or partial incompatibility of simultaneous fitment of the removal parts of two items of equipment

Nature of
the
Document Commercial Constraint Commercial Document
Installation Installation
Reference Reference Reference Reference

NSF
EXL
B3168-092-04 Digital moving Map EURONAV IV - 08-46021-B
- - Recommended EMS configurations X RN6 (EURO AVIONICS) interfaced
with FCDS / MEGHAS, basic version
05-42022-A B2105-001-00 Air conditioning/cooling system – X B2315-092-00 IRIDIUM satellite phone AEROPHONE 08-15551-A
Metro (STC) (AERODATA)
05-42022-A B2105-001-00 Air conditioning/cooling system – x B2563-812-00 Automatic Deployable ELT (ADELT) 06-67049-A
Metro (STC)
05-42022-A B2105-001-00 Air conditioning/cooling system – x B2300-006-00 Avionics Solution B3 -
Metro (STC)
06-11023-A B3272-001-20 Snow skids X B3274-001-20 Settling protectors, det. parts 06-11024-A

06-11024-A B3274-001-20 Settling protectors, det. parts x B3272-001-20 Snow skids 06-11023-A

06-21019-A B8512-001-1? External hoist, fixed prov. (on X B8534-003-1? Rope-down device for 2 persons, fixed 06-24011-A
respective side) prov. (on respective side)
06-21019-A B8512-001-2? External hoist, det. parts (on X B8534-003-2? Rope-down device for 2 persons, det. 06-24011-A
respective side) parts (on respective side)
07-27003-A B2523-002-00 Club seating, 8 pax configuration X B2522-009-20 High-density seating, 9 pax 07-27009-A
configuration
07-27003-A B2523-002-00 Club seating, 8 pax configuration X B2522-010-20 High-density seating, 10 pax 07-27009-A
configuration
07-27009-A B2522-009-20 High-density seating, 9 pax X B2523-002-00 Club seating, 8 pax configuration 07-27003-A
configuration
07-27009-A B2522-010-20 High-density seating, 10 pax X B2523-002-00 Club seating, 8 pax configuration 07-27003-A
configuration
08-35020-A B2327-001-01 Traffic Advisory System TAS x B7161-001-10 Sand filter system, fixed provisions 05-25017-A
9900BX

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

8 Main performance
The following performance values and figures refer to an EC145, equipped with average production
engines.
Unless otherwise specified, the values and figures refer to a clean helicopter at Sea Level (SL), in
International Standard Atmosphere (ISA) and zero wind condition.

Performance on 2 engines (AEO)

kg 2,400 2,700 3,000 3,300 3,585
8.1.1 Gross Weight lb 5,290 5,950 6,615 7,275 7,905
km/h 278 278 268 268 268
„ Maximum speed (VNE)
kts 150 150 145 145 145
km/h 256 254 252 250 246
„ Maximum cruising speed (VH)
kts 138 137 136 135 133
km/h 237 239 241 243 243
„ Recommended cruising speed
kts 128 129 130 131 131
„ Fuel consumption at recommended cruising kg/h 234 238 244 251 254
speed lb/h 516 525 538 554 560
m/s 14.9 13.0 11.2 9.3 8.1
„ Maximum rate of climb, TOP
ft/min 2940 2560 2210 1840 1600
m 5,485 5,485 4,695 3,840 2,925
„ Hover ceiling IGE (3 ft AGL), TOP
ft 18,000 18,000 15,400 12,600 9,600
m 5,485 5,120 4,345 3,445 770
„ Hover ceiling OGE, TOP, ISA
ft 18,000 16,800 14,260 11,300 2,530
„ Service ceiling, MCP, m 5,485 5,485 5,485 5,485 5,240
(climb reserve 200 ft/min), ISA ft 18,000 18,000 18,000 18,000 17,200
„ Range (SL, ISA) with max. fuel capacity at
recommended cruise speed (no reserve)
z Std fuel tank configuration (694 kg) km --- 705 700 685 680
nm --- 380 377 370 370
z Long range fuel tank inst. (869 kg) km --- --- 875 865 855
nm --- --- 472 467 461

„ Endurance (SL, ISA) with maximum fuel

capacity at 65 KIAS (no reserve)
z Std fuel tank configuration (694 kg) h:min --- 3:55 3:50 3:40 3:35
z Long range fuel tank inst. (869 kg) h:min --- --- 4:50 4:40 4:30

The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
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 Technical Data
Performance on 1 engine (OEI)
kg 2,400 2,700 3,000 3,300 3,585
Gross Weight lb 5,290 5,950 6,615 7,275 7,905
„ Single engine service ceiling, OEI, MCP, m 5,456 4,590 3,755 2,966 1,996
100 ft/min climb reserve, ISA ft 17,900 15,060 12,320 9,730 6,550
„ Single engine service ceiling, OEI, MCP, m 4,968 4,029 3,097 2,185 1,338
100 ft/min climb reserve, ISA + 20°C ft 16,300 13,220 10,160 7,170 4,390
m/s 5.7 4.4 3.2 2.1 1.2
„ Maximum rate of climb, OEI, MCP, SL, ISA
ft/min 1,120 860 630 420 230
„ Max. temperature for CAT A, take-off from
°C + 50 + 50 + 50 + 49 + 42
clear heliport at SL
„ Max. weight, HOGE, SL, ISA, kg 2,785
(OEI 2.5 min-power) lb 6,140
„ Max. weight, HOGE, SL, ISA + 20°C, kg 2,520
(OEI 2.5 min-power) lb 5,555
kg 3,415
„ Max. weight, CAT A, VTOL, SL, ISA
lb 7,530
kg 3,320
„ Max. weight, CAT A, VTOL, SL, ISA + 10°C
lb 7,320

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

5,485 m PA
„ Maximum operating altitude
18,000 ft PA
5,485 m PA or DA
„ Maximum operating altitude for hover in ground effect,
18,000 ft PA or DA
takeoff and landing
whichever is less
„ Minimum temperature - 45 °C
ISA + 35 °C
„ Maximum temperature
(max. + 50°C)

Abbreviations

AGL Above Ground Level OGE Out Of Ground Effect

DA Density Altitude PA Pressure Altitude
IGE In Ground Effect SL Sea Level
ISA International Standard Atmosphere TOP Take-Off Power
MCP Maximum Continuous Power VNE Never-Exceed Speed
OEI One Engine Inoperative VTOL Vertical Take-Off and Landing

The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
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 Technical Data
Hover In Ground Effect (HIGE, TOP)

The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
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 Technical Data
Hover Out Of Ground Effect (HOGE, TOP)

The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
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 Technical Data
Take-Off Weight, Cat. A, Clear Heliport

The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
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 Technical Data
Take-Off Weight, Cat. A, VTOL

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

The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
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 Technical Data
Maximum Rate Of Climb, TOP, 3585 kg (MTOW)

The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
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 Technical Data
Maximum Rate of Climb, MCP, 3585 kg (MTOW)

The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
145.06.101.02 E 59
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 Technical Data
Fuel consumption (AEO)

see page 62

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

see page 62

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

see pages 60
and 61

The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
145.06.101.02 E 62
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 Technical Data
Payload vs. Range (AEO)

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

BLANK

The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
145.06.101.02 E 64
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