Eurocopter EC130B4 Instruction manual

Eurocopter reserves the right to make configuration and data changes at any time without notice.
The facts and figures contained in this document and expressed in good faith do not constitute any offer or contract with Eurocopter
EC130 B4
130 B4 09.101.01 E
Technical
Data
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130 B4 09.101.01 E.pdf 1 15/01/2009 17:03:38

Technical Data
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.
130 B4 09.101.01 E 1
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-2009
Contents
1 - Foreword .................................................................................................... 3
2 - General characteristics ............................................................................ 4
3 - Baseline Aircraft Definition ..................................................................... 11
4 - Recommended mission configurations................................................... 13
5 - Optional equipment .................................................................................. 21
6 - Main performance ..................................................................................... 29
7 - Customer Service Overview ...................................................................... 49
Manufacturers notice
Attention !
EUROCOPTER, its logo, AS350, EC130, ALOUETTE,ECUREUIL,
FENESTRON, INDOC, STARFLEX, STYLENCE, VEMD, are trade marks of
the Eurocopter group.
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
and 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.

Technical Data
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.
130 B4 09.101.01 E 2
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Blank

Technical Data
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.
130 B4 09.101.01 E 3
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1- Foreword
The light single-engine EC130 B4 is the quietest, most spacious helicopter available on the market. It fulfils
the JAR 27 issue 1 regulation for VFR operation by day and night 1. With a Maximum Gross Weight of
2,427 kg /5,531 lb, the EC130 B4 is perfectly suited for the following missions:
Corporate use,
Passenger transport,
Tour operations,
Utility,
Emergency Medical Services (EMS / AMS),
The ultra-quiet EC130 B4 integrates the latest technological advances of EUROCOPTER's new generation
helicopters: a new 7/8 seats enlarged cabin with enhanced comfort, a new tail boom with quiet FENESTRON
shrouded tail rotor, a dual channel FADEC unit plus a third independent and automatic channel for engine
control, an automatic variable rotor speed control for noise reduction, a dual hydraulic system and energy
attenuating seats for each occupant. It has been designed to be environmental friendly, with an optimal
external noise pattern. It is one of the few aircraft meeting the very stringent noise level required in the
United States to fly over National Parks (GCNP). A high component community with EUROCOPTER light
helicopters' range results in a helicopter that is easy and affordable to maintain, increasing fleet versatility.
With its large cabin volume and high performance level, this "light truck" is the replacement of former
ALOUETTE III.
To optimise the Man-Machine Interface the helicopter is basically fitted with the VEMD (Vehicle and Engine
Multifunction Display) on the instrument panel. The EC130 B4 is powered with a TURBOMECA ARRIEL 2B1
engine of 847 shp (632 kW) and equipped with a dual channel FADEC system (Full Authority Digital Engine
Control), and third back-up control system. Therefore it offers the same world-beating performance
parameters, as the AS350 B3.
1by night, in VFR, when the equipment required by operational regulations are installed and serviceable.

Technical Data
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.
130 B4 09.101.01 E 4
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2- General Characteristics
Layout
Passenger-transport
z1 pilot + 6 passengers in standard version 1
z1 pilot + 7 passengers in "medium density" version
Casualty-evacuation
z1 pilot + 1 or 2 stretcher patients + 2 medical attendants
z2 pilots + 1 stretcher patient + 2 medical attendants
Cargo carrying
z1 pilot + 3.7 m³(130.7 ft³) load in cabin
Equipment
Complete 7 seats interior + trims + carpets included in standard
Ready to operate radio package included in standard :
z2 VHF
z2 VOR / LOC / GLIDE
z1 GPS
z1 ELT
z1 XPD mode A + C
z1 ICS capable of 8 outlets
z1 ADI
z1 HSI
Weights
Note : Empty weight accuracy : within
± 2 % kg lb
Empty weight, baseline aircraft 21,378 33,038
Useful load 41,049 2,313
Maximum all-up weight 2,427 5,351
Maximum cargo-swing load 1,160 2,557
Maximum all-up weight in external load configuration 2,800 6,172
1If required by the local airworthiness authorities, the capacity can be limited to 1 pilot + 5 passengers.
2Baseline aircraft empty weight includes oil and unusable fuel. Ballast plates can be added at the rear of the
FENESTRON, their mass is 12.8 kg (28.2 lb) maximum. The baseline helicopter is delivered as standard with
4.8 kg (10.6 lb) ballast weight that is not included in the basic empty weight.
3Empty weight according to baseline aircraft definition, as defined in pages 11 and 12, including the avionics suite.
4The useful load does not include the ballast plates. Depending on the configuration, the ballast’s weight will be
deducted from the useful load.

Technical Data
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.
130 B4 09.101.01 E 5
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Power plant
1 TURBOMECA ARRIEL 2B1 turbine engine
Engine ratings
Thermodynamic Power, in standard atmosphere, at sea level : kW ch shp
Take-off power 632 860 847
Maximum continuous power 543 739 728
Usable Fuel capacities
litres US gal. kg lb
Standard fuel tank 540 143 426 939
External noise
In accordance with ICAO annex 16, chapter 8
Average value 86,8 EPNdB (- 7.0 dB / average ICAO limit)
Over flight 84,3 EPNdB (- 8.5 dB / ICAO limit)
(- 0.5 dB / GCNP 1noise rule 6 PAX)
(- 1.2 dB / GCNP noise rule 7 PAX)
Internal noise
The noise in the cabin is also improved in order to increase pilot and passengers comfort.
Measures have been realised on a standard aircraft and give the following mean levels :
81.3 dB SIL42in hover inside ground effect
86.1 dB SIL4 in cruise flight at 120 kts
1GCNP = Grand Canyon National Park.
2The method of sound level measurement used is Speech Interference Level (dB SIL4). This is the arithmetic
average of 4 octave (0.5, 1.0, 2.0 and 4.0 kHz) levels specified in dBlin (linear decibels). This particular set of
octaves corresponds to the human voice frequency range and thus allows to evaluate the interference with
passenger communication.

Technical Data
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.
130 B4 09.101.01 E 6
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Main dimensions

Technical Data
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.
130 B4 09.101.01 E 7
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Dimensions of compartments and accesses
Cabin main dimensions
CABIN
Surface
A 3,00 m²
32.3 ft²
Volume 3.7 m³
130.7 ft³
LH HOLD
Surface
0.52 m²
5.60 ft²
Volume 0.285 m³
10.06 ft³
RH HOLD
Surface
B 0.43 m²
4.63 ft²
Volume 0.245 m³
8.65 ft³
REAR HOLD
Surface
0.55 m²
5.92 ft²
Volume 0.565 m³
19.95 ft³
TOTAL HOLDS
Surface
1.50 m²
16.15 ft²
Volume
1.095 m³
38.66 ft³

Technical Data
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.
130 B4 09.101.01 E 8
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Configurations
Standard Layout
Club seating Layout
Medium density Layout 1
1Cabin lay-out if the option “8 Energy-absorbing seats lay-out” is fitted.

Technical Data
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.
130 B4 09.101.01 E 9
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Standard Cabin Lay-out and upholstery
The EC130 B4 offers an enlarged cabin floor, allowing comfortable accommodation for the pilot and
6 passengers on individual energy-absorbing seats. The rear seats are slightly elevated to offer a better
visibility to the passengers.
STYLENCE Cabin Lay-out and upholstery (optional)
Note: EC130 B4 in STYLENCE upholstery configuration.
Enlarged cargo holds

Technical Data
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.
130 B4 09.101.01 E 10
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Other characteristics
TURBOMECA ARRIEL 2B1 turbine engine
847 shp (632 kW) take-off power
Triple engine control : one dual channel FADEC
(Full Authority Digital Engine Control) unit plus a
third independent and automatic back up channel
Optimized engine ratings according to outside
operations conditions thanks to electronic
governing system (FADEC)
Optimized engine monitoring through the VEMD
Automatic starting sequence
VEMD (Vehicle and Engine Multifunction Display)
Full colour LCD display
Fully duplex equipment
Self monitoring at one glance
First Limitation Indication (FLI) with aural warning
Mission parameters calculation
Engine cycle counting
Engine health monitoring
Noise reduction
The outstanding noise reduction is given by :
Automatic variable rotor speed control
quiet FENESTRON shrouded tail rotor

Technical Data
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.
130 B4 09.100.01 E 11
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3- EC130 B4 ECUREUIL - Baseline Aircraft Definition
The helicopter in the definition, presented hereafter, meets the certification standards for day and night VFR operations, set by the following
airworthiness authorities : EASA, FAA, TC. This list is not restrictive and the status of approval by other airworthiness authorities must be
checked. Additional equipment item may be required by the relevant operational regulation (most of them are available in catalogue).
GENERAL
The EC130 B4®is certified with a pilot being on the left side
The baseline aircraft is delivered with left side controls and
fixed parts of the removable dual controls (the removable parts
of removable dual controls are optional)
Fuselage comprising the cabin and 3 luggage holds, with floor tie-
down nets and access doors
Tail boom with stabilizer, FENESTRON®type anti torque rotor,
and tail skid
Tubular skid landing gear, with replaceable skid shoes, with long
footsteps (on right and on left side), profiler on rear tube, capable
of taking handling wheels
Lifting points
Mooring fixtures
External paint : fuselage painted in 1 to 3 colours according to
standard paint schemes. Unless modified by optional item, the
main rotor head and tail rotor covers are painted in grey, the skid
landing gear in dark grey and the FENESTRON®duct in light
grey
Internal paint : light grey (prevailing colour)
Interior signs and markings : available in either French or English
CABIN
Cabin floor in light-alloy sheet-metal
2 pilot and copilot high-back energy-absorbing seats,
adjustable in reach, removable, complete with cushions, safety
belts and shoulder harnesses
1 passenger high-back energy-absorbing seat (front right),
removable, complete with cushions, safety belt and shoulder
harness
4 passenger high-back energy-absorbing seats (rear row),
removable, complete with cushions, safety belts and shoulder
harnesses fitted on a removable frame bolted on the cabin floor
2 pilot and copilot jettisonable doors
z1 LH front door fitted with a sliding window
z1 RH large front door
1 LH rear sliding door
1 RH rear fixed panel
Locks on every access to cabin and luggage compartments
Lock on fuel cap
Lateral and upper tinted windows (windscreen excluded)
1 ceiling housing the cabin lighting, 7 air ventilation outlets and
controls (ventilation controls, rotor brake and fuel cut-off)
Capabilities for mandatory optional item : air conditioning or
ventilation systems
Cabin heating
Demisting system for front windscreen
2 pilot map cases
Door map case in LH and RH front doors
Floor carpet
Rear bulkhead and lateral rear upholstery
1 fire-extinguisher
1 Flight Manuall: available in either French or English
Interior harmony according to definition in force
INSTRUMENTS
Instruments units : available in either metric or English units
1 airspeed indicator
1 altimeter
1 vertical speed indicator
1 LCD rotor and free turbine dual indicator
1 clock
1 warning panel
1 magnetic compass
1 heated pitot head
1 external side slip indicator
1 control box for light and electrical generation
1 ICS connection to audio warning issued from VEMD®
1 LCD dual screen Vehicle and Engine Multifunction display
(VEMD®) providing the following information :
zFirst limitation indicators (FLI)
torquemeter
exhaust gas temperature (T4)
gas generator tachometer (Ng, delta Ng)
zEngine oil temperature, pressure
zFuel quantity
zFuel flow and estimated remaining time to fly
zAmmeter and voltmeter and battery temperature
zOutside air temperature
zEnhanced usage monitoring functions
IGE/OGE performance calculations
engine cycle counting
engine power check
overlimits display
zVEMD®and peripheral maintenance information
zData downloading capability (software and connection wire
as option)

Technical Data
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.
130 B4 09.100.01 E 12
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AVIONICS
1 avionics master switch
1 gyro-horizon
1 gyro-compass with
1 horizontal Situation Indicator
1 turn and bank indicator
1 VHF/VOR/LOC/GS
1 VHF/VOR/LOC/GS/GPS
1 transponder (mode A+C)
1 altitude encoder
1 Emergency Locator Transmitter
1 ICS + passenger interphone
POWER PLANT
1 Turboméca ARRIEL 2B1 632 kW (850 ch - 847 shp) turbine
engine complete with starting, fuel supply and dual channel
digital engine control system (FADEC) and 1 back-up fuel
control box that automatically controls the engine in case of a
total failure of the 2 digital channels of the FADEC
1 fuel system including 1 tank of 540 liters (143 US gal.) total
capacity
1 twist grip on pilot side (for engine reduction in case of tail
rotor failure and autorotation training)
1 magnetic plug and 1 chip detector
1 engine lubrication and oil cooling system
1 fire detection system
1 air-intake protection grids
1 torque-measurement pick-up
TRANSMISSION SYSTEM
1 main gearbox, anti-vibration mounted, with oil sight gauge,
chip detector, oil temperature and pressure switches, port for
endoscope and self sealing valve for oil sampling and draining
1 main gearbox oil cooling system
1 engine to main gearbox coupling shaft
1 rotor brake
1 main rotor high and low r.p.m. warning device
1 tail drive carried by five anti-friction bearings
1 tail gearbox with oil sight gauge, chip detector and port for
endoscopic inspection
ROTORS AND FLIGHT CONTROLS
1 main rotor with 3 composite-material blades around a
STARFLEX®head fitted with spherical thrust bearings
1 anti-torque rotor (FENESTRON®)with 10 asymmetrical
blades, integrated in vertical fin
3 main rotor hydraulic servo units (duplex servos)
2 independent hydraulic generation systems
ELECTRICAL INSTALLATION
One 150 A, 28 VDC starter-generator
One 15 A.h cadmium-nickel battery
1 ground power receptacle
3 position lights (LED)
1 flashing anti-collision light (LED)
2 fixed landing lights
2 cabin light sets, each with 2 reading lights for 2 rear
passengers and 1 dome light
1 instrument panel lighting system
Integrated lighting in central console
1 reading map light on upper canopy strut for pilot
1 cockpit breaker panel
One 28 V DC cabin power outlet
AIRBORNE KIT (*)
1 pitot head cover
2 static port stoppers
1 engine air-intake blanking cover
1 tail-pipe plug
2 ground handling bogies c/w hydraulic jacking system
1 lifting ring
2 upper mooring rings
3 main-blade socks
1 document holder
1 airborne kit stowage bag
Manuals (CD ROM)
(*) (weight not included in standard aircraft empty weight)

Technical Data
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.
130 B4 09.101.01 E 13
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4- Recommended mission configurations
EUROCOPTER proposes different mission configurations for its helicopters. This pre-selected list
of optional equipment should be regarded as a recommended minimum equipment list and can be
complemented by additional equipment from the optional equipment list in chapter 5.Please take
note that there can be incompatibilities between optional equipments. Any modification and/or
complement of the proposed mission configuration must be done in with assistance of a
EUROCOPTER sales representative.
The proposed mission configurations are done by EUROCOPTER using its years of experience in
making helicopters and in coordination with different operators of the EC130 B4 around the world.
For the EC130 B4 the recommended mission configurations are:
Passenger transport mission
Corporate transport mission (STYLENCE).

Technical Data
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.
130 B4 09.101.01 E 14
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4-1 Passenger transport mission
The EC130 B4 with its FENESTRON shrouded fan tail rotor is one of the most silent helicopters flying
nowadays. Its very low noise level is 7 dB under the limits defined by the Grand Canyon National Park rule.
The helicopter has been designed with the occupants in mind. Each passenger is comfortably seated on
individual and comfortable seats. The wide and unobstructed cabin with very high visibility offers the
passengers an excellent view for both the front and the rear passengers. The rear passengers' seats are
placed on a raised platform to provide this excellent view.
Using the technologies of the well-known ECUREUIL family, the EC130 B4 has an exceptional high rate of
availability. All these elements make the EC130 B4 therefore the benchmark for passenger transport and
tourism helicopters.
Weights
Note : Empty weight accuracy : within
± 2 % kg lb
Empty weight, Passenger transport mission configuration
(including engine oil and unusable fuel) 1,460 3,219
Useful load 967 2,132
Maximum all-up weight 2,427 5,351
Maximum cargo-swing load 1,160 2,557
Maximum all-up weight in external load configuration 2,800 6,172

Technical Data
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.
130 B4 09.101.01 E 15
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Mission configuration
Document
reference Commercial
reference Name kg lb
EC130 B4 Baseline aircraft as per 130 B4 09.100.01 E 1,378.0 3,038.0
General Equipment
05-02049-A 05-02049-00-CI Customized external paint scheme 1 - 25.0 11.0
05-03003-A 05-03003-00-CI First aid kit 31.8 4.0
05-23005-A 05-23005-00-CI Engine wash 0.8 1.8
05-27001-A 05-27001-00-CI Cabin fire-extinguisher 41.7 3.7
05-31033-A 05-31033-00-CI Sun protected upper windows 2.0 4.4
05-37015-A 05-37015-00-CI Dual controls 2.6 5.7
05-42025-A 05-42025-01-CI Air conditioning system with reinforced front air distribution 43.0 94.8
Specific Mission Equipment
06-27003-A 06-27003-00-FP Cargo swing 1,160 kg – 2,557 lb - Fixed Parts 5.1 11.2
06-42017-A 06-42017-00-CI Landing light adjustable in site and azimuth 54.3 9.5
06-61006-A 06-61006-00-FP Emergency floatation gear - Fixed Parts 5- 63.6 7.9
Avionics
Standard VFR day and night package (included in Baseline Aircraft)
Thales H321EGM - Gyro-horizon 7
Honeywell KCS55A - Gyro Compass with
Honeywell KI525A - Horizontal Situation Indicator 8
UI 9560 - Turn and Bank indicator
Honeywell KX165A - VHF/VOR/LOC/GS
Garmin GNS430W - VHF/VOR/LOC/GS/GPS 9- 10
Garmin GTX327 - Transponder (mode A+C)
Shadin 8800T - Altitude Encoder
Kannad 406AF-H - Emergency Locator Transmitter 11
Garmin GMA340 - ICS 12 -13
Configuration continued on next page…
1The paint scheme must be approved at the latest 6 months before the delivery of the helicopter.
2The option customized external paint scheme includes between 4-6 different colors.
3Recommended for public transport mission. Its content is the buyer’s responsibility as it may vary according to
geographical region or applicable regulations.
4If type is accepted by local regulations.
5May be a mandatory equipment, required by local airworthiness authorities or operational regulations.
6When the removable parts are not fitted on the aircraft, a part of the fixed parts representing 2 kg - 4.4 lb can be
easily dismounted (less than one working day).
7With slip indicator included when the Turn and Bank indicator is replaced by the stand-by gyro-horizon.
8With a selector switch for NAV1/NAV2 selection.
9This equipment is delivered with the original EUROPE map which can be not up to date. Subscription to be made
by the customer.
10 Aircraft with capability WAAS (Wide Area Augmentation System). WAAS network only covers the entire United
States and some of Canada and Mexico.
11 3 frequencies : 121.5 MHz, 243 MHz, 406 MHz. Compliant with ED 62 and TSO C91A.
The Programming Data Sheet must be filled and communicated by the customer two months at the latest before
the helicopter's delivery.
12 Includes the passenger interphone function.
13 I.C.S. compatible only with High level / High impedance headsets.
The headsets of the passengers should be of the same mark and the same model.

Technical Data
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.
130 B4 09.101.01 E 16
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Document
reference Commercial
reference Name kg lb
Avionics
08-22019-A 08-22019-01-CI Garmin GTX330 - Transponder (mode S) 1- 2
instead of Garmin GTX327 - Transponder (mode A+C) 0.7 1.5
08-51019-A 08-51019-01-CI Thales H321EGM - Stand-by gyro-horizon 1-3
instead of UI 9560 - Turn and Bank indicator 3.1 6.8
08-18035-A 08-18035-00-CI David Clark H10-13H – Headset (Qty. 7) 43.5 7.7
08-21008-A 08-21008-06-CI Thales AHV16 - Radio altimeter 1 - 5 -6 4.6 10.1
08-83017-A 08-83017-00-CI VEMD data download kit 7- 8— —
1May be a mandatory equipment, required by local airworthiness authorities or operational regulations.
2The mode S identification must be communicated by the customer two months at the latest before the delivery.
3Fitted with independent battery.
4High level / High impedance headset.
5The Radio Altimeter includes a 100 ft warning signal. The volume of this signal can be tuned down.
6Option available for deliveries end 2009.
7Allows compliance to JAR OPS 3 Amendment 3 requirement, as defined in Appendix 1
to JAR OPS 3.517 (a) and (b)(5)(i). Requires absolute time data, given through a compatible connection with
serviceable GPS equipment (Compliance achieved with the standard aircraft as defined on pages 11 and 12).
8Delivered in addition to the airborne kit, the kit includes two software and a connection wire.

Technical Data
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.
130 B4 09.101.01 E 17
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Technical Data
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.
130 B4 09.101.01 E 18
This document is the property of EUROCOPTER©; no part of it shall be reproduced or transmitted without the express prior written authorization ο f EUROCOPTER©and its contents shall not be disclosed. © EUROCOPTER-2009
4-2 Corporate transport mission (STYLENCE)
In the corporate configuration, the EC130 B4 can transport up to seven passengers in roominess and
comfort that is usually not found in a light helicopter. A large sliding door and the long boarding steps along
both sides of the helicopter allow easy access to the cabin. The passengers are seated on forward facing
energy absorbing seats
The additional STYLENCE package offers a high level of finishing to the interior of the helicopter. It is
available in six different colours (brick, aubergine, camel, graphite, silver and marine).
Weights
Note : Empty weight accuracy : within
± 2 % kg lb
Empty weight, Corporate transport mission configuration
(including engine oil and unusable fuel) 1,508 3,324
Useful load 919 2,027
Maximum all-up weight 2,427 5,351
Maximum cargo-swing load 1,160 2,557
Maximum all-up weight in external load configuration 2,800 6,172

Technical Data
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.
130 B4 09.101.01 E 19
This document is the property of EUROCOPTER©; no part of it shall be reproduced or transmitted without the express prior written authorization ο f EUROCOPTER©and its contents shall not be disclosed. © EUROCOPTER-2009
Mission configuration
Document
reference Commercial
reference Name kg lb
EC130 B4 Baseline aircraft as per 130 B4 09.100.01 E 1,378.0 3,038.0
Mission Package
00-50015-B 00-50015-02-CI STYLENCE package 1102.0 225.0
General Equipment
05-23005-A 05-23005-00-CI Engine wash 0.8 1.8
05-25027-A 05-25027-00-CI Enhanced Engine Air Particle Separators 27.1 15.7
05-37015-A 05-37015-00-CI Dual controls 2.6 5.7
Specific Mission Equipment
06-27003-A 06-27003-00-FP Cargo swing 1,160 kg – 2,557 lb - Fixed Parts 5.1 11.2
06-42017-A 06-42017-00-CI Landing light adjustable in site and azimuth 34.3 9.5
06-61006-A 06-61006-00-FP Emergency floatation gear - Fixed Parts 3- 43.6 7.9
Avionics
Standard VFR day and night package (included in Baseline Aircraft)
Thales H321EGM - Gyro-horizon 5
Honeywell KCS55A - Gyro Compass with
Honeywell KI525A - Horizontal Situation Indicator 6
UI 9560 - Turn and Bank indicator
Honeywell KX165A - VHF/VOR/LOC/GS
Garmin GNS430W - VHF/VOR/LOC/GS/GPS 7- 8
Garmin GTX327 - Transponder (mode A+C)
Shadin 8800T - Altitude Encoder
Kannad 406AF-H - Emergency Locator Transmitter 9
Garmin GMA340 - ICS 10 -11
Configuration continued on next page…
1For the content of the STYLENCE package, please refer to page 21 of this Technical Data.
2Capabilities included in standard aircraft. The sand filter authorises the flight under falling snow.
3May be a mandatory equipment, required by local airworthiness authorities or operational regulations.
4When the removable parts are not fitted on the aircraft, a part of the fixed parts representing 2 kg - 4.4 lb can be
easily dismounted (less than one working day).
5With slip indicator included when the Turn and Bank indicator is replaced by the stand-by gyro-horizon.
6With a selector switch for NAV1/NAV2 selection.
7This equipment is delivered with the original EUROPE map which can be not up to date.
Subscription to be made by the customer.
8Aircraft with capability WAAS (Wide Area Augmentation System). WAAS network only covers the entire United
States and some of Canada and Mexico.
93 frequencies : 121.5 MHz, 243 MHz, 406 MHz. Compliant with ED 62 and TSO C91A.
The Programming Data Sheet must be filled and communicated by the customer two months at the latest before
the helicopter's delivery.
10 Includes the passenger interphone function.
11 I.C.S. compatible only with High level / High impedance headsets.
The headsets of the passengers should be of the same mark and the same model.