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EC130 T2Technical Data2014

Technical Data

FENNEC(Military Version)

Ecureuil AS355 NP

Fennec AS550 C3e

Ecureuil AS350 B2

Ecureuil AS350 B3e

Ecureuil EC130 T2

130 T2

SINGLE ENGINE TWIN ENGINEECUREUIL

(Civil Version)

Technical Data

130 T2 14.101.01 E 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. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2014 – All rights reserved.

Contents 1 Foreword ................................................................................................................................ 3

2 General Characteristics ....................................................................................................... 5

2.1 Cockpit and Cabin Layouts ........................................................................................... 5

2.2 Weight ........................................................................................................................... 5

2.3 Power Ratings .............................................................................................................. 5

2.4 Fuel Capacities ............................................................................................................. 5

2.5 External Sound Level ................................................................................................... 5

2.6 External Dimensions ..................................................................................................... 6

2.7 Internal Dimensions ...................................................................................................... 7

2.8 Configurations............................................................................................................... 8

2.9 Other Characteristics .................................................................................................... 9

2.10 VFR Day and Night Package, included in Baseline Aircraft Definition ....................... 11

3 Baseline Aircraft Definition ................................................................................................ 12

4 Mission Configurations ...................................................................................................... 15

4.1 Passenger Transport Mission ..................................................................................... 17

4.2 Aerial Work Mission .................................................................................................... 21

4.3 Corporate Transport Mission (STYLENCE) ............................................................... 25

5 Further Equipment Information ......................................................................................... 29

5.1 List of Optional Equipment ......................................................................................... 29

6 Main Performance ............................................................................................................... 31

7 Service and Support Information ...................................................................................... 55

7.1 Assets ......................................................................................................................... 55

7.2 Inspection Programs ................................................................................................... 56

7.3 Main Components TBO/SLL ....................................................................................... 57

7.4 Technical Support ....................................................................................................... 58

7.5 Airbus Helicopters Maintenance Services .................................................................. 59

7.6 Engine Maintenance Program .................................................................................... 60

7.7 Training ....................................................................................................................... 61

7.8 Engine Training Courses ............................................................................................ 62

7.9 Technical Publication .................................................................................................. 62

7.10 T.I.P.I. (Technical Information Publication on Internet) .............................................. 63

7.11 Customer Flight Operations Support & Services ........................................................ 63

8 Abbreviations ...................................................................................................................... 65

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1 Foreword

The EC130 T2® is the upgraded version of the well known EC130 B4® and remains the leader on the tourism market thanks to its spacious cabin, its outstanding visibility and its very low external sound level that makes it the quietest helicopter in its class. This new comer in the ECUREUIL® range benefits from a massive redesign based on the successful EC130 B4. Comfort has been upgraded thanks to a brand new anti-vibration device, an air ventilation system that has been especially redesigned for this helicopter and air conditioning. In addition, the new STYLENCE® interior option offers a cabin layout with high level of finishing and comfort. The elegant interior design with stylish seats and high quality materials creates an exclusive ambiance. All these improvements make the flight smoother and more enjoyable for passengers and crew. The EC130 T2 responds to the most demanding safety requirements from the Certification Specifications (CS-27) of the European Aviation Safety Agency (EASA). Equipped with improved energy absorbing seats, it encompasses dual-hydraulics and is fitted with a crashworthy fuel tank to enhance safety. Man Machine Interface has been improved by introducing a new console panel’s concept, thus reducing pilot workload. It is equipped with the brand new Turbomeca ARRIEL 2D engine, controlled by a new generation FADEC including the latest technology, an Engine Data Recorder for a better monitoring of engine data along with a creep damage counter for a better surveillance of module 3 that enables to shift from classic maintenance to predictive one. Thus, anticipative actions drastically reduce unscheduled removals to enhance helicopter availability. The ARRIEL 2D engine offers 14% more power compared to the previous engine version and a 30 minute take-off power rating for occasional use. That makes the EC130 T2 much more versatile to answer to additional missions such as aerial work and hot and high operations. New optional equipment are available on the EC130 T2 such as the new cargo-sling with an external load capacity of 1,500 kg (3,307 lb) that increase the versatility of the helicopter. The design of the EC130 T2 has been driven by optimisation of the maintenance. The lower Direct Maintenance and Operating Costs thanks to higher engine TBO and a reduction of specific fuel consumption respond to Customers’ request in terms of economical improvements. More versatile, more comfortable, more modern and more powerful, the EC130 T2 is the answer for private owners as well as for operators performing passenger transport, utility, EMS and law enforcement missions. It is in addition perfectly adapted for operations in hot and high environments and mountainous areas.

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2 General Characteristics

2.1 Cockpit and Cabin Layouts

Passenger-transport 1 pilot + 6 passengers in standard version 1 1 pilot + 7 passengers in "8 seats layout" version

Cargo carrying 1 pilot + 3.7 m³ (130.7 ft³) load in cabin

2.2 Weight kg lb

Empty weight, Baseline Aircraft Definition 2 1,433 3 3,159 Useful load, Baseline Aircraft Definition 1,067 2,352 Maximum take-off weight (MTOW) 2,500 5,512 Maximum take-off weight with external load 3,050 6,724

Maximum cargo-sling load 1,500 3,307

Note: Empty weight accuracy: within 2 %

2.3 Power Ratings 1 Turbomeca ARRIEL 2D turboshaft engine EC130 T2 Thermodynamic Power, in standard atm., at SL. 4 kW shp

Take-off power 710 952 Maximum continuous power 638 856

2.4 Fuel Capacities liters US gal. kg lb

Crashworthy fuel tank 540 143 426 939 accuracy = ± 1 %

2.5 External Sound Level

In accordance with ICAO annex 16, chapter 11 and FAR Part 36 Appendix J Hover flight value at 2500 kg 81,1 dB SEL (- 5.9 dB / ICAO and FAR limits)

Margin with respect to the US Grand Canyon Nation Park For 6 passengers seats (- 0.7 dB SEL / GCNP 5 limit = 81.8 dB SEL) For 7 passengers seats (- 1.3 dB SEL / GCNP limit = 82.4 dB SEL)

1 If required by the local airworthiness authorities, the capacity can be limited to 1 pilot + 5 passengers. 2 Baseline aircraft empty weight includes oil and unusable fuel. 3 Empty weight according to baseline aircraft definition, as defined in pages 12 and 13, including the avionics suite. 4 These engine ratings are subject to other limitations. Please refer to the Flight Manual. 5 GCNP = Grand Canyon National Park.

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6 130 T2 14.101.01 E


2.6 External Dimensions

Technical Data

130 T2 14.101.01 E 7


2.7 Internal Dimensions

CABIN Surface

A 3,00 m²32.3 ft²

Volume 3.7 m³130.7 ft³

LH HOLD Surface 0.52 m²

5.60 ft²

Volume 0.285 m³10.06 ft³

RH HOLD Surface 0.47 m²

5.06 ft²

Volume 0.254 m³8.970 ft³

REAR HOLD

Surface 0.55 m²5.92 ft²

Volume 0.565 m³19.95 ft³

TOTAL HOLDS Surface 1.59 m²

17.12 ft²

Volume 1.135 m³ 40.07 ft³

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8 130 T2 14.101.01 E


2.8 Configurations Standard Layout

8 seats Layout

Note: 8 seats layout is an option to be contracted specifically.

Technical Data

130 T2 14.101.01 E 9


2.9 Other Characteristics Turbomeca ARRIEL 2D turboshaft engine

952 shp (710 kW)Thermodynamic Power, in standard atmosphere, at Sea Level.

Triple engine control: one dual channel FADEC (Full Authority Digital Engine Control) unit plus and 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 One Engine Data Recorder, with a memory for

further download VEMD

Full color 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

Engine Creep Damage counter

Dual hydraulic system Safety and reliability of the EC130 T2 are highly improved with the dual hydraulic system installed in Baseline aircraft. Crashworthy fuel tank The fuel tank has been crashworthy certified by EASA and prevents from possible post crash fires. This protection is also valid with the aerial work configuration (cargo sling installed under the cabin).

Technical Data

10 130 T2 14.101.01 E


Sound level reduction

Automatic variable rotor speed control

Quiet FENESTRON® shrouded tail rotor

Anti vibration system The EC130 T2 is equipped with a dynamic anti vibration system aiming at reducing significantly vibrations of all the Cabin structure. This new system offers a significant comfort for the pilots and passengers. Air Conditioning system (option) The new air-conditioning system equipped with an automatic heating/cooling system and a new dynamic ventilation design offers higher performances and a very high comfort onboard.

Technical Data

130 T2 14.101.01 E 11


2.10 VFR Day and Night Package, included in Baseline Aircraft Definition The VFR day and night package is composed of the following equipment:

Emergency locator transmitter - Kannad (Orolia group) INTEGRA 406 AP-H

VHF/VOR/LOC/GS Honeywell KX165A

Intercom system (ICS) Garmin GMA340H

Transponder (mode S) Garmin GTX 330

VHF/VOR/LOC/GS/GPS Garmin GNS 430W

Gyro-horizon Thales H 321 EGM

Gyro Compass Honeywell KCS 55A with Horizontal Situation Indicator

Honeywell KI 525A

Altitude Encoder Shadin 8800T

Turn and Bank indicator UI 9560

Standard Instrument Panel Layout

Note: Instrument panel includes integrated lighting. The baseline aircraft definition includes an avionics package as defined here above. Brands and models are given for information. reserves the rights to modify the layout, any brand or model according to its policy in force.

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12 130 T2 14.100.01 E


3 Baseline Aircraft Definition

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130 T2 14.100.01 E 13


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14 130 T2 14.101.01 E


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4 Mission Configurations The following mission equipped configurations are proposed by Airbus Helicopters, benefitting from years of experience in designing & producing helicopters and from coordination with different operators of the ECUREUIL family around the world. All the configurations encompass several equipment as a basis for all missions, including avionics and the radio suite. On top of this Baseline Aircraft Definition, these pre-selected lists of optional equipment should be regarded as a recommended equipment list. In order to be further customized, these mission configurations can be complemented by additional optional equipment proposed in chapter 5 ‘Further equipment information’ of this Technical Data 1. For the EC130 T2, the reference mission configurations are:

Passenger Transport Mission

Aerial Work Mission

Corporate Transport Mission.

1 Please note that some constraints may exist between optional equipment. Any modification and/or complement of the

proposed mission configurations must be established with assistance of a AIRBUS HELICOPTERS sales representative.

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16 130 T2 14.101.01 E


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130 T2 14.101.01 E 17


4.1 Passenger Transport Mission The EC130 T2 with its FENESTRON shrouded fan tail rotor is one of the most silent helicopters flying nowadays. Its very low sound level is 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 raised to provide this excellent view.

Using the technologies of the well-known ECUREUIL family, the EC130 T2 has an exceptional high rate of availability. All these elements make the EC130 T2 therefore the benchmark for passenger transport and tourism helicopters. Weight

kg lb Empty weight, passenger transport mission configuration

(including engine oil and unusable fuel) 1,509 3,327

Useful load 991 2,184 Maximum all-up weight 2,500 5,511

Notes: Empty weight accuracy within 2 %

Including 7 headsets.

Technical Data

18 130 T2 14.101.01 E


4.1.1 Mission Configuration

Document reference

Commercial reference

Description kg lb

Basic Aircraft Components

00-10010-B 00-10010-03-CI EC130 T2 Baseline Aircraft (130 T2 14.100.01 E) 1433.0 3159.2

08-00025-C 08-00025-02-CI VFR day and night package, included in baseline definition 0.0 0.0

06-67076-A


2 frequencies: 121.5 MHz (VHF), 406 MHz (COSPAS-SARSAT). The Programming Data Sheet must be filled and communicated by the customer two months at the latest before the helicopter's delivery.

08-11010-A


08-16002-A


Includes the passenger interphone function.

ICS compatible with High level / High impedance headsets.

08-22016-B

Transponder (mode S) - Garmin GTX 330

The mode S identification must be communicated by the customer two months at the latest before the delivery.

08-43038-A


This equipment is delivered with the original EUROPE map. Subscription for updates to be made by the customer. Aircraft with capability WAAS (Wide Area Augmentation System). WAAS network only covers the United States and parts of Canada and Mexico.

08-51002-A


With slip indicator included when the Turn and Bank indicator is replaced by the stand-by gyro-horizon.

08-52011-A

Gyro Compass Honeywell KCS 55A with Horizontal Situation Indicator Honeywell KI 525A

With a selector switch for NAV1/NAV2 selection.

08-57002-A

Altitude encoder - Shadin 8800 T

08-63006-A


General Equipment

05-02068-A 05-02068-00-CI Enhanced exterior painting 4.0 8.8

Paint schemes with up to 3 colours. The paint scheme must be approved at the latest 6 months before the delivery of the helicopter.

05-03003-A 05-03003-00-CI First aid kit 1.9 4.2

Recommended for public transport mission. Its content is the buyer's responsibility as it may vary according to geographical region or applicable regulations.

05-23005-A 05-23005-00-CI Engine flushing device without removal of cowlings 0.8 1.8

05-25029-A 05-25029-00-CI Heavy duty blade pins 0.0 0.0

Recommended for operations in sandy and abrasive conditions.

05-31025-A 05-31025-00-CI Tinted windows for front windscreens 0.0 0.0

05-31033-A 05-31033-00-CI Sun protected upper windows 2.0 4.4

05-42025-B 05-42025-03-CI Enhanced Air conditioning system 39.6 87.3

Technical Data

130 T2 14.101.01 E 19


Mission Configuration (continued)

Document reference


Description kg lb

Specific Mission Equipment

06-42017-A 06-42017-00-CI Landing light adjustable in site and azimuth 4.3 9.5

May be a mandatory equipment, required by Local Airworthiness Authorities or operational regulations.

06-61006-A 06-61006-00-FP Emergency floatation gear - Fixed Parts 3.6 7.9

May be a mandatory equipment, required by Local Airworthiness Authorities or operational regulations. When the removable parts are not fitted on the aircraft, a part of fixed parts representing 2 kg - 4.4 lb can be easily dismounted.

06-93000-A 06-93000-00-CI Additional ballast plates in tail boom 8.0 17.6

In order to tune the weight and balance of the aircraft by the operator for customized configurations.

Avionics

08-18035-A 08-18035-00-CI Headset - David Clark H10-13H 0.5 1.1

High level / High impedance headset.

08-21008-A 08-21008-06-CI Radio altimeter Thales AHV16 5.6 12.3

May be a mandatory equipment, required by local airworthiness authorities or operational regulations.The Radio Altimeter includes a 100 ft warning signal. The volume of this signal can be tuned down.

08-51019-A 08-51019-01-CI Stand-by gyro-horizon Thales H321EGM, instead of Turn and Bank indicator UI 9560

3.1 6.8


Fitted with independant battery.

08-83017-A 08-83017-00-CI VEMD data download kit 0.0 0.0

Delivered in addition to the airborne kit, this kit includes two softwares and a connection wire. It allows compliance to EASA-OPS Part CAT (EU Regulation n° 965/2012) AMC2 CAT.POL.H.305(b) § (c) requirement concerning the ‘usage monitoring system’ function requested for ‘operations without an assured safe forced landing capability’. Requires absolute time data, given through a compatible connection with serviceable GPS equipment (Compliance achieved with the Baseline Aircraft definition).

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20 130 T2 14.101.01 E


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4.2 Aerial Work Mission The EC130 T2 has extended its versatility to Aerial work missions thanks to an increased external load capacity (1,500 kg – 3,307 lb) and a list of new optional equipment such as cargo-sling. This multi-mission helicopter is the right answer for operators that want to combine cargo-load operations and passenger transport mission. The new individual energy-absorbing rear seats can be easily and quickly removed for offering a large flat floor cabin for freight transportation. The ARRIEL 2D engine, more powerful and capable of 30 minutes take-off power rating for occasional use, offers high performance and allows operations in hot and high conditions even in mountainous environments.

The cockpit includes the dual LCD-screen VEMD, that gives the pilot the possibility to see all the vehicle parameters at one glance, reducing his workload and enhancing safety. It leaves the pilot the possibility to concentrate at its mission at hand. Weight

kg lb Empty weight, aerial work mission configuration

(including engine oil and unusable fuel) On request

Useful load On request Maximum all-up weight 2,500 5,511 Maximum cargo-sling load 1,500 3,307 Maximum all-up weight in external load configuration 3,050 6,724

Technical Data

22 130 T2 14.101.01 E



Document reference


Description kg lb




06-67076-A



08-11010-A


08-16002-A




08-22016-B



08-43038-A



08-51002-A



08-52011-A



08-57002-A


08-63006-A


General Equipment

05-02079-A 05-02079-00-CI Engine exhaust area black thermal painting 1.0 2.2

Recommended for aerial work mission. The paint scheme must be approved at the latest 6 months before the delivery of the helicopter.

05-03003-A 05-03003-00-CI First aid kit 1.9 4.2

Recommended for public transport mission. Its content is the buyer's responsibility as it may vary according to geographical region or applicable regulations.

05-21002-A 05-21002-00-CI Wire strike protection system 5.3 11.7

05-25027-B 05-25027-01-CI Enhanced Engine Air Particle Separator 7.1 15.7

The EAPS is recommended for flights in sandy environment and mandatory for flights in falling snow conditions.



05-32012-A 05-32012-00-CI Pilot's windshield wiper On request

Technical Data

130 T2 14.101.01 E 23



Document reference


Description kg lb


06-11006-A 06-11006-00-CI Short protective skid shoes 2.5 5.5

06-26026-A 06-26026-00-CI-ECL Dual external cargo sling mirrors On request

Recommended for sling work. May be a mandatory equipment, required by Local Airworthiness Authorities or operational regulations.

STC Eurocopter Canada installed on aircraft at delivery.

06-27048-A 06-27048-00-FP Cargo sling (1500kg) - Fixed Parts On request

06-27048-A 06-27048-00-RP Cargo sling (1500kg) - Removable Parts On request



Avionics





Technical Data

24 130 T2 14.101.01 E


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Technical Data

130 T2 14.101.01 E 25


4.3 Corporate Transport Mission (STYLENCE) In the corporate configuration, the EC130 T2 can transport up to seven passengers in roominess and comfort that is usually not found in a light helicopter. The elegant STYLENCE interior design with stylish seats and high quality materials creates an exclusive ambiance. 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 new STYLENCE Layout offers a high level of finishing to the interior of the helicopter and is available in 6 different colors.

Weight

kg lb Empty weight, corporate transport mission configuration

(including engine oil and unusable fuel) On request

Useful load On request Maximum all-up weight 2,500 5,511

Technical Data

26 130 T2 14.101.01 E



Document reference


Description kg lb




06-67076-A



08-11010-A


08-16002-A




08-22016-B



08-43038-A



08-51002-A



08-52011-A



08-57002-A


08-63006-A


General Equipment

05-02068-A 05-02068-01-CI Complex exterior painting 4.0 8.8

Complex paint schemes with up to 6 colors. The paint scheme must be approved at the latest 6 months before the delivery of the helicopter.

05-02068-A 05-02068-03-CI Exterior painting modifications 1.0 2.2

Modification of design (specific paint colors and/or paint scheme), consideration of color gradient, painted logo. The paint scheme must be approved at the latest 6 months before the delivery of the helicopter.







Technical Data

130 T2 14.101.01 E 27



Document reference


Description kg lb








Interior Layout

07-00021-C 07-00021-02-CI STYLENCE layout On request

The STYLENCE layout is available in 6 color schemes:

Silk Flame Terra Cobalt Titanium Shadow

Avionics

08-18037-A 08-18037-01-CI ICS installation compatible with Bose headset 1.0 2.2

Includes ICS stereo jacks : in addition to the standard jacks for pilot and copilot and in replacement of the standard jacks for passengers. Provides electrical supply for the use of Bose headset without battery pack.

08-18043-B 08-18043-01-CI Bose headset 0.5 1.1





3.1 6.8

May be a mandatory equipment, required by Local Airworthiness Authorities or operational regulations. Fitted with independant battery.


Delivered in addition to the airborne kit, this kit includes two softwares and a connection wire. It allows compliance to EASA-OPS Part CAT (EU Regulation n° 965/2012) AMC2 CAT.POL.H.305(b) § (c) requirement concerning the ‘usage monitoring system’ function requested for ‘operations without an assured safe forced landing capability’. Requires absolute time data, given through a compatible connection with serviceable GPS equipment (Compliance achieved with the Baseline Aircraft Definition).

Technical Data

28 130 T2 14.101.01 E


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5 Further Equipment Information

5.1 List of Optional Equipment This chapter includes all the optional equipment that can be selected to customize the EC130 T2 helicopter. Please note that some constraints may exist between optional equipment. Any configuration established from this list of optional equipment should be made with the assistance of an Airbus Helicopters sales representative. Note: value of the weight breakdown is based on actual weighting of aircraft or on robust estimation during design phase ; It is

given for information and shall not be considered as contractual.

Document reference


Description kg lb

General Equipment

05-01024-B 05-01024-01-CI Russian Certification Kit 4.0 8.8

05-02068-A 05-02068-00-CI Enhanced exterior painting 4.0 8.8

Paint schemes with up to 3 colours. The paint scheme must be approved at the latest 6 months before the delivery of the helicopter.

05-02068-A 05-02068-01-CI Complex exterior painting 4.0 8.8

Complex paint schemes with up to 6 colours. The paint scheme must be approved at the latest 6 months before the delivery of the helicopter.

05-02068-A 05-02068-02-CI Customized exterior painting On request

Unlimited number of colours and designs. To be defined with customer (upon request). The paint scheme must be approved at the latest 6 months before the delivery of the helicopter.

05-02068-A 05-02068-03-CI Exterior painting modifications 1.0 2.2

Modification of design (specific paint colors and/or paint scheme), consideration of color gradient, painted logo. The paint scheme must be approved at the latest 6 months before the delivery of the helicopter.

05-02077-A 05-02077-00-CI STYLENCE exterior painting On request

05-02079-A 05-02079-00-CI Engine exhaust area black thermal painting 1.0 2.2

Recommended for aerial work mission.

The paint scheme must be approved at the latest 6 months before the delivery of the helicopter.

05-03003-A 05-03003-00-CI First aid kit 1.9 4.0

Recommended for public transport mission. Its content is the buyer's responsibility as it may vary according to geographical region or applicable regulations

05-21002-A 05-21002-00-CI Wire strike protection system 5.3 11.7


05-24005-B 05-24005-00-CI High visibility paint scheme on main rotor blades (red or yellow strips) 0.1 0.2

05-25006-A 05-25006-00-CI Reinforced sand-erosion protection strip on main rotor blades 0.3 0.7

05-25027-B 05-25027-01-CI Enhanced Engine Air Particle Separator 7.1 15.7

The EAPS is recommended for flights in sandy environment and mandatory for flights in falling snow conditions.





05-32012-A 05-32012-00-CI Pilot's windshield wiper On request

05-37015-A 05-37015-00-CI Dual controls 2.6 5.7


05-63002-A 05-63002-02-CI 200 A starter-generator 1.1 2.4

05-92016-A 05-92016-00-FP Folding of main rotor blades - Fixed Parts 1.8 4.0

For rough weather conditions.

05-92016-A 05-92016-00-RP Folding of main rotor blades - Removable Parts 0.0 0.0

The Removable Parts are delivered as Ground Support Equipment.

Technical Data

30 130 T2 14.101.01 E


Document reference


Description kg lb


06-11006-A 06-11006-00-CI Short protective skid shoes 2.5 5.5

06-26026-A 06-26026-00-CI-ECL Dual external cargo sling mirrors On request

Recommended for sling work. May be a mandatory equipment, required by Local Airworthiness Authorities or operational regulations. STC EUROCOPTER Canada installed on aircraft at delivery.

06-27048-A 06-27048-00-FP Cargo sling (1500kg) - Fixed Parts On request

06-27048-00-RP Cargo sling (1500kg) - Removable Parts On request





06-61006-A 06-61006-00-RP Emergency floatation gear - Removable Parts 57.4 126.5




Interior Layout

07-00021-C 07-00021-02-CI STYLENCE Layout On request

07-24005-A 07-24005-00-CI 8 Energy-absorbing seats layout. 18.6 41.0

When the aircraft is delivered with 8 seats, the rails for installing 7 seats are provided as loose equipment. According to the aircraft configuration, ballast plates are included to tune the weight and balance of the aircraft.

The weight figure includes a ballast average value of 4.8 kg - 10.6 lb (maximum value 12.8 kg - 28.2 lb).

07-40006-A 07-40006-00-CI Cabin carpet for 7 seats layout 6.3 13.9

07-40006-B 07-40006-01-CI Cabin carpet for 8 seats layout 6.3 13.9

Avionics



08-18037-A 08-18037-01-CI ICS installation compatible with Bose headset 1.0 2.2

Includes ICS stereo jacks : in addition to the standard jacks for pilot and copilot and in replacement of the standard jacks for passengers. Provides electrical supply for the use of Bose headset without battery pack.

08-18043-B 08-18043-01-CI Bose headset 0.5 1.1




08-51015-B 08-51015-01-CI Stand-by gyro-horizon Thales H321EGM 3.8 8.4


3.1 6.8

May be a mandatory equipment, required by Local Airworthiness Authorities or operational regulations. Fitted with independant battery.



Technical Data

130 T2 14.101.01 E 31


6 Main Performance The following performance values and figures refer to an EC130 T2. Unless otherwise specified, the values and figures refer to a clean helicopter, equipped with a new engine, at Sea Level (SL), in International Standard Atmosphere (ISA) and zero wind condition. Note: The following data are extracted from the approved flight manual which is the reference for

performance computation.

Gross Weight kg 1,800 2,000 2,200 2,300 2,400 2,500 lb 3,968 4,409 4,850 5,071 5,291 5,512

Max. speed, VNE km/h 287 287 287 287 287 287 kts 155 155 155 155 155 155

Fast cruise speed (at MCP) km/h 247 244 242 240 238 236 kts 133 132 130 129 128 127

Recommended cruise speed km/h 222 222 222 222 222 222 kts 120 120 120 120 120 120

Fuel consumption kg/h 169 169 169 169 169 169 at fast cruise speed lb/h 372 373 373 373 373 373

Fuel consumption kg/h 148 150 153 154 156 157 at recommended cruise speed lb/h 326 331 337 339 343 346

Rate-of-climb m/s 12 11 10 9 9 8 ft/min 2,235 2,070 1,895 1,800 1,700 1,600

Hover ceiling I.G.E. at Take-Off Power ISA m 6,370 5,425 4,530 4,105 3,690 3,435*

ft 20,900 17,805 14,870 13,470 12,115 11,270* ISA + 20°C m 5,600 4,640 3,735 3,295 2,865 2,590*

ft 18,385 15,230 12,270 10,815 9,400 8,510* Hover ceiling O.G.E. at Take-Off Power

ISA m 5,940 4,975 4,060 3,625 3,210 2,950* ft 19,500 16,335 13,325 11,905 10,540 9,675*

ISA + 20°C m 5,155 4,165 3,225 2,770 2,325 2,040* ft 16,915 13,675 10,585 9,090 7,640 6,700*

Service ceiling (Vz = 0,5 m/sec. – 100 ft/min.)

ISA m >7,010 7,010 6,685 6,295 5,885 5,510 ft >23,000 23,000 21,945 20,660 19,320 18,085

ISA+ 20°C m 7,010 6,605 5,760 5,340 4,925 4,550 ft 23,000 21,678 18,903 17,531 16,168 14,942

Range (without fuel reserve, at fast cruise speed)

with standard tanks km 424 625 617 614 610 606 n.m 229 337 333 331 329 327

Range (without fuel reserve, at recommended cruise speed)

with standard tanks km 437 642 632 626 621 616 n.m 236 346 341 338 335 332

Endurance (without reserve) h / min 2:52 4:12 4:08 4:06 4:03 4:00

* Performance demonstrated for 2,465 kg (5,434 lb).

Technical Data

32 130 T2 14.101.01 E


Operating limitations The helicopter is cleared to be operated within the following altitude and temperature limitations (according to Flight Manual). For complementary information, refer to Flight Manual:

Maximum altitude Flight 7,010 m – 23,000 ft (PA)

Temperature

Maximum ISA + 35°C limited to 50°C Minimum - 40°C (basic)

Units nm nautical miles hr:min hours:minutes kts: Knots kg kilograms ft/min feet/minute lb pounds m/s meters per seconds km kilometers ° C degrees Celsius

Technical Data

130 T2 14.101.01 E 33


Performance charts The performance charts presented hereafter apply to an aircraft as per the standard definition.

Page

Take-off weight in hover IGE, (height 5 ft, Maximum TOP, no wind)

34

Take-off weight in hover OGE, (Maximum TOP, no wind)

35

Fast cruise speed (ISA)

36

Fast cruise speed (ISA + 20°C)

37

Fast cruise speed (ISA + 35°C)

38

Recommended cruise speed (ISA)

39

Recommended cruise speed (ISA + 20°C)

40

Recommended cruise speed (ISA + 35°C)

41

Rate of climb in oblique flight (ISA)

42

Rate of climb in oblique flight (ISA + 20°C)

43

Rate of climb in oblique flight (ISA + 35°C)

44

Hourly fuel consumption at fast cruise speed (ISA, ISA + 20°C, ISA + 35°C)

45

Hourly fuel consumption at recommended cruise speed (ISA)

46

Hourly fuel consumption at recommended cruise speed (ISA + 20°C)

47

Hourly fuel consumption at recommended cruise speed (ISA + 35°C)

48

Payload / Range (ISA, fast cruise speed, without reserve)

49

Payload / Range (ISA + 20°C, fast cruise speed, without reserve)

50

Payload / Range (ISA + 35°C, fast cruise speed, without reserve)

51

Payload / Range (ISA, recommended cruise speed, without reserve)

52

Payload / Range (ISA + 20°C, recommended cruise speed, without reserve)

53

Payload / Range (ISA + 35°C, recommended cruise speed, without reserve)

54

Technical Data

34 130 T2 14.101.01 E


HOVER CEILING I.G.E. at maximum TOP (Height 5 ft)

0

5000

10000

15000

20000

0

1000

2000

3000

4000

5000

6000

7000

-40 -30 -20 -10 0 10 20 30 40 50

OAT (°C)

Zp (m) (ft)ISO-(kg)

ISA

ISA

+ 2

0

ISA

+ 3

5

1500

160017001800

1900200021002200230024002465

2500

Note: Approved performance, as long as the engine meets the power check criteria, as defined in the Flight Manual.

Technical Data

130 T2 14.101.01 E 35


HOVER CEILING O.G.E. at maximum TOP

0

5000

10000

15000

20000

0

1000

2000

3000

4000

5000

6000

7000

-40 -30 -20 -10 0 10 20 30 40 50

OAT (°C)

Zp (m) (ft)ISO-(kg)

ISA

ISA

+ 2

0

ISA

+ 3

5

150016001700

1800190020002100220023002400

2500260027002800

2900

30003050

2465

2500

Note: ISO weight curves in thin lines (from 2,500 to 3,050 kg) are curves with external load, for information. Approved performance, as long as the engine meets the power check criteria, as defined in the Flight Manual.

Technical Data

36 130 T2 14.101.01 E


FAST CRUISE SPEED ISA

80 90 100 110 120 130 140 150

0

5000

10000

15000

20000

0

1000

2000

3000

4000

5000

6000

7000

140 160 180 200 220 240 260 280

True Air Speed (km/h)

(kt)

Zp (m) (ft)ISO-Weight (kg) 1500

1600

1700

1800 1900

2000 210022002300

24002500

Note: Typical performance, with clean baseline aircraft and new engine.

Technical Data

130 T2 14.101.01 E 37


FAST CRUISE SPEED ISA+20°C

80 90 100 110 120 130 140 150

0

5000

10000

15000

20000

0

1000

2000

3000

4000

5000

6000

7000

140 160 180 200 220 240 260 280


(kt)

Zp (m) (ft)ISO-Weight (kg) 1500

1600

1700 1800

19002000 2100

22002300 2400

2500


Technical Data

38 130 T2 14.101.01 E


FAST CRUISE SPEED ISA+35°C

80 90 100 110 120 130 140 150

0

5000

10000

15000

20000

0

1000

2000

3000

4000

5000

6000

7000

140 160 180 200 220 240 260 280


(kt)

Zp (m) (ft)ISO-Weight (kg)

1500

1600 1700

1800

1900

20002100

22002300

2400

2500


Technical Data

130 T2 14.101.01 E 39


RECOMMENDED CRUISE SPEED ISA

80 90 100 110 120

0

5000

10000

15000

20000

0

1000

2000

3000

4000

5000

6000

7000

140 160 180 200 220

Vp (km/h)

(kt)

Zp (m) (ft)ISO-M (kg)

18001900200021002200

2300

24002500


Technical Data

40 130 T2 14.101.01 E


RECOMMENDED CRUISE SPEED ISA+20°C

80 90 100 110 120

0

5000

10000

15000

20000

0

1000

2000

3000

4000

5000

6000

7000

140 160 180 200 220

TAS (km/h)

(kt)

Zp (m) (ft)ISO-Weight (kg)1600

1700180019002000 2100

22002300 2400

2500


Technical Data

130 T2 14.101.01 E 41


RECOMMENDED CRUISE SPEED ISA+35°C

80 90 100 110 120

0

5000

10000

15000

20000

0

1000

2000

3000

4000

5000

6000

7000

140 160 180 200 220

TAS (km/h)

(kt)

Zp (m) (ft)ISO-Weight (kg)15001600

1700 1800

1900

20002100

22002300

2400

2500


Technical Data

42 130 T2 14.101.01 E


RATE OF CLIMB IN OBLIQUE FLIGHT ISA

00 10

0

5000

10000

15000

20000

0

1000

2000

3000

4000

5000

6000

7000

0 500 1000 1500 2000 2500 3000

Rate of Climb (ft/mn)

(m/s)


1500

1600

1700

1800

1900

2000

21002200230024002500


Technical Data

130 T2 14.101.01 E 43


RATE OF CLIMB IN OBLIQUE FLIGHT ISA + 20°C

00 10

0

5000

10000

15000

20000

0

1000

2000

3000

4000

5000

6000

7000

0 500 1000 1500 2000 2500 3000


(m/s)


1500

1600

1700

1800

1900200021002200230024002500


Technical Data

44 130 T2 14.101.01 E


RATE OF CLIMB IN OBLIQUE FLIGHT ISA + 35°C

00 10 15

0

5000

10000

15000

20000

0

1000

2000

3000

4000

5000

6000

7000

0 500 1000 1500 2000 2500 3000


(m/s)


1500

1600

17001800

1900

200021002200

230024002500


Technical Data

130 T2 14.101.01 E 45


HOURLY FUEL CONSUMPTION at fast cruise speed ISA, ISA + 20°C, ISA + 35°C

225 275 325 375

0

5000

10000

15000

20000

0

1000

2000

3000

4000

5000

6000

7000

80 100 120 140 160 180

Hourly Fuel Consumption (kg/h)

(lb/h)

Zp (m) (ft)ISO-ISA (kg)

ISA

ISA

+20

ISA

+35

Note: Typical consumption with clean baseline aircraft and new engine.

Technical Data

46 130 T2 14.101.01 E


HOURLY FUEL CONSUMPTION at recommended cruise speed ISA

225 275 325

0

5000

10000

15000

20000

0

1000

2000

3000

4000

5000

6000

7000

80 90 100 110 120 130 140 150 160


(lb/h)


1500

16

00

1700

1800

1900

2000

2100

2200

2300

2400

2500


Technical Data

130 T2 14.101.01 E 47


HOURLY FUEL CONSUMPTION at recommended cruise speed ISA + 20°C

225 275 325

0

5000

10000

15000

20000

0

1000

2000

3000

4000

5000

6000

7000

80 90 100 110 120 130 140 150 160


(lb/h)


1600

1700

1800

1900

2000

2100

2200

2300

2400

2500

1500


Technical Data

48 130 T2 14.101.01 E


HOURLY FUEL CONSUMPTION at recommended cruise speed ISA + 35°C

225 275 325

0

5000

10000

15000

20000

0

1000

2000

3000

4000

5000

6000

7000

80 90 100 110 120 130 140 150 160


(lb/h)


15001600

17001800

19002000

21002200

2300

2500

2400


Technical Data

130 T2 14.101.01 E 49


PAYLOAD RANGE ISA Fast cruise speed

0 100 200 300 400

0

500

1000

1500

2000

0

200

400

600

800

1000

0 200 400 600 800

Range (km)

(nm)

Payload (kg) (lb)

0ft - 0

m

5000f t - 1

524m

Notes:

Typical mission without reserve, with clean baseline aircraft and new engine. Empty Weight of the Baseline Aircraft definition equipped and approved for VFR day and night operations (avionics

included in empty weight) with 1 pilot.

Technical Data

50 130 T2 14.101.01 E


PAYLOAD RANGE ISA + 20°C Fast cruise speed

0 100 200 300 400

0

500

1000

1500

2000

0

200

400

600

800

1000

0 200 400 600 800

Range (km)

(nm)

Payload (kg) (lb)0ft - 0

m

50

00

ft - 152

4m

Notes: Typical mission without reserve, with clean baseline aircraft and new engine. Empty Weight of the Baseline Aircraft definition equipped and approved for VFR day and night operations (avionics


Technical Data

130 T2 14.101.01 E 51


PAYLOAD RANGE ISA + 35°C Fast cruise speed

0 100 200 300 400

0

500

1000

1500

2000

0

200

400

600

800

1000

0 200 400 600 800

Range (km)

(nm)

Payload (kg) (lb)

0ft - 0

m

50

00

ft - 15

24

m



Technical Data

52 130 T2 14.101.01 E


PAYLOAD RANGE ISA Recommended cruise speed

0 100 200 300 400

0

500

1000

1500

2000

0

200

400

600

800

1000

0 200 400 600 800

Range (km)

(nm)

Payload (kg) (lb)0

ft - 0m

50

00

ft - 15

24

m

Notes:



Technical Data

130 T2 14.101.01 E 53


PAYLOAD RANGE ISA + 20°C Recommended cruise speed

0 100 200 300 400

0

500

1000

1500

2000

0

200

400

600

800

1000

0 200 400 600 800

Range (km)

(nm)

Payload (kg) (lb)

0ft - 0

m

5000ft - 1

524m



Technical Data

54 130 T2 14.101.01 E


PAYLOD RANGE ISA + 35°C Recommended cruise speed

0 100 200 300 400

0

500

1000

1500

2000

0

200

400

600

800

1000

0 200 400 600 800

Range (km)

(nm)

Payload (kg) (lb)0

ft - 0m

5000ft - 1

524m

Notes:



Technical Data

130 T2 14.101.01 E 55


7 Service and Support Information

7.1 Assets At Airbus Helicopters, supporting Customer’s helicopter operations with the highest level of excellence is our priority. We have developed a strong reputation world-wide for being fully committed to providing Customers with mission-efficient aircraft combining both high aircraft availability rate and cost-effective support and services solutions. This high level of performance has been our main target throughout the years, and therefore Airbus Helicopters has stressed the importance of sharing operational feed-back with its Customers to better understand their operational needs, and closely follow-up in-service Reliability, Availability and Maintainability/Testability (RAMT). The final target is to reach the most optimized operational cost while ensuring the highest flight safety. Airbus Helicopters has built and delivered family the EC130 family since 2001. There are more than 470 helicopters in service world-wide. The total flight hours accumulated at this date exceeds 1,100,000 hours. The “fleet leader” aircraft has accumulated more than 17,000 flight hours. To ensure and the most efficient support of these helicopters whatever the location in the world, Airbus Helicopters offers:

A worldwide service network of 30 subsidiaries and participations, more than 100 distributors, representatives, training centers, repair and overhaul facilities, and maintenance

centers around the globe, as well as 5 logistics hubs in France , Germany, Hong Kong and the USA

Customer Service Centers in Europe, Asia and the USA offering around-the-clock Customer assistance, 7 days a week, 365 days a year

A wide array of services solutions to meet all operators needs in terms of technical support, component repair and overhaul, spare parts support, technical publications and training – at Airbus Helicopters facilities or at Customer’s location.

Technical Data

56 130 T2 14.101.01 E


7.2 Inspection Programs The Maintenance Program specifies the intervals between maintenance operations that are recommended by Airbus Helicopters, irrespective of whether they are mandatory or not. The program can: – either be used as is, – or be adapted by each operator to suit his own specific organization, provided he complies with

the maximum intervals. The following table provides an overview of all inspections. Scheduled inspections with shorter time intervals have to be added to those with longer time intervals.

Scheduled Airframe Inspection Estimated Man Hour

Pre-flight checks Pilot’s task

Flight related checks (10 flight hrs or 7 days periodicity tasks) Maintenance or other approved personnel

150 flight hrs or 12 months periodicity tasks 2,36 MMH

600 flight hrs or 24 months periodicity tasks 75 MMH

Airframe Major Inspection Estimated Man Hour

12 years periodicity tasks 200 MMH

Scheduled Engine Inspection ARRIEL 2D Estimated Man Hour

15 flight hrs or 7 days periodicity tasks

0,0348 MMH per FH

800 flight hrs periodicity tasks

MMH: Mean Man Hour FH:Flight Hour

Note: All the “hands-on” aircraft values mentioned here above are given on the basis of a 20 000 flight hours life cycle. They refer only to the scheduled inspections for the standard helicopter without optional equipment in accordance with the Master Servicing Manual (MSM). The announced Man Hours are without incoming flight, work preparation, reworking, servicing, Service Bulletin implementation and unscheduled maintenance.

Technical Data

130 T2 14.101.01 E 57


7.3 Main Components TBO/SLL Main component values are given for information purposes only. The reference document is the aircraft Master Servicing Manual

Main Components TBO (h) as per

MSM 002

SLL (h) as per

ASL 000 Main rotor blade 20000 Sleeve 4400 Main rotor shaft unit 58000 cycles Starflex hub 3000 Spherical thrust bearing 4600 Main gearbox bevel reduction gear 3000

Main gearbox epicyclic reduction gear 3000

Tail gearbox 4000 Blade,tail rotor 10000 Servo control, main rotor 3000 Tail rotor hub 6900 Servo control, main 20000

Engine TBO (h) TBO (h) Target Value

SLL (h)

ARRIEL 2D 4000 6000 Time Between Overhauls (TBO): The component in question must be removed at each interval that corresponds to the value indicated, in order to undergo the operations in a specialized workshop that will enable it to be put back into service for the next interval. A TBO is granted with a 10 % operational margin, limited at +300 hours. Some subcomponents may have a Service Life Limit, rated above the TBO limit. Service Life Limit (SLL): The Service Life Limit is an airworthiness limit. The component in question must be removed from service when it reaches the limit indicated.

Technical Data

58 130 T2 14.101.01 E


7.4 Technical Support Airbus Helicopters proposes a comprehensive range of Technical Assistance services such as: Front Office support On-site Technical Representative The on-site Technical Representative is responsible for the following activities:

Interface between the customer and Airbus Helicopters in-house technical and engineering support

Aircraft setting-up assistance (explanation for usage of special maintenance tools and equipment)

Troubleshooting assistance, diagnostic and solution recommendation Demonstration of standard maintenance practices to customer

Aircraft Technical Assistance Airbus Helicopters team of skilled field service technicians provides the customer with world-class support and enhanced services for aircraft maintenance, repairs and retrofits at customer’s premises. As part of this service Airbus Helicopters technicians will bring the required tooling such as a mobile jig to carry out the required maintenance tasks. Back Office support Technical Product Support Airbus Helicopters will provide technical knowledge dedicated to your helicopters, aimed at supporting the safe and reliable operation of the aircraft. A team of highly skilled engineers in close and daily relation with Design Office, is committed to answer any technical question. This group is also in charge to establish technical improvements, recommendations for use, Customer information (Service Bulletins, Information Notices…), and is the focal point of contact for technical relation with .

Technical Data

130 T2 14.101.01 E 59


7.5 Airbus Helicopters Maintenance Services Airbus Helicopters offers its Customers a wide array of services in favour of an increased availability and a better cost control. These services are tailored to the various operators’ profiles such as High Flyers, Low Flyers, operators looking for immediate parts availability or wishing maximum budget control. They range from basic OEM repair and overhaul service up to comprehensive By-the-Hour maintenance programs. Customers, according to their operational requirement, have the possibility to select one of below flexible and modular main solutions. By-Event services:

Classical Support Standard exchange service Guaranteed Turn-Around-Time (TAT) program

By-the-Hour services:

Unscheduled Maintenance Insurance Program (UMIP) Parts-By-the-Hour program (PBH)

Classical Support The classical support consists in an Initial Provisioning package to support aircraft operation. This package includes Tools, Test Equipment, but also spare parts necessary to carry-out aircraft inspections and reparable parts to cover immediate replacement when necessary. For reparable parts, the required level of operational availability determines the part numbers and the quantity of parts needed, and therefore the investment to be put in place. In addition to this Initial Provisioning package, a classical Repair & Overhaul service mode is proposed and consists in parts return to Airbus Helicopters for repair or overhaul when needed. Airbus Helicopters will perform an appraisal and quote the work to be done. Work shall be performed upon acceptance of the estimate. With this type of classical support package, Customer keeps the responsibility to monitor the component R&O activity, manage obsolescence, and maintain the right inventory level on site. Standard Exchange The Standard Exchange consists in replacing a defective part with a serviceable and interchangeable part within 48 hours. This service is available for dynamic components, and equipment. Guaranteed Turn-Around-Time (TAT) program Airbus Helicopters offers contracts covering a list of specific components and for which repair or overhaul price and Turn-Around-Times are committed. In exceptional cases, should the contractual date of delivery be impossible to reach, Airbus Helicopters will provide the Customer with a standard exchange for the agreed repair or overhaul price.

Technical Data

60 130 T2 14.101.01 E


Unscheduled Maintenance Insurance Plan (UMIP) With the UMIP, Airbus Helicopters gives the customer the option to secure unscheduled maintenance costs while remaining responsible for the scheduled events (overhaul, life limited part replacement). Price for this service is calculated per flight hour. The UMIP service includes unscheduled component repair within 24H through Standard Exchange based on a dedicated inventory. This service is available for dynamic components, blades and equipment. Parts By the Hour (PBH) The Parts By the Hour (PBH) service is a comprehensive program that offers and balances at the same time guaranteed maintenance costs, reduced inventory and minimized helicopter downtime. This service is intended for Customers looking for total cost control and high level of aircraft availability. Price for this service is calculated per flight hour. The PBH service includes component unscheduled repairs component overhauls as well as Life Limited part replacement. Parts replacement is guaranteed within 24H through Standard Exchange based on a dedicated inventory. This service is available for dynamic components, blades and equipment.

7.6 Engine Maintenance Program Always careful to maximize the efficiency of your operations and reduce your costs, Turbomeca, the engine manufacturer has developed an improved service offering. Turbomeca puts at Customers’ disposal 32 Repair Centers across the globe, supplemented by several new factory-authorized service facilities strategically located near Customer’s operations. Turbomeca range of services covers:

Classical Repair and Overhaul Standard Exchange AOG services Support By the Hour (SBH) services

Within the Support By the Hour coverage, Turbomeca developed specific maintenance packages, as summarized hereafter. Standard Coverage: “Classical” SBH The “classical” Support by the Hour (SBH) is a global support service offered to operators to enable them to maintain the best availability of their engines fleet through a contract arrangement paid by running hours. The Support by the Hour (SBH) is operated mainly through Standard Exchange supported by Turbomeca dedicated Corporate Pool.

Technical Data

130 T2 14.101.01 E 61


Customized Coverage: “Mission” SBH The new service, Support By the Hour Mission, offers a modular series of comprehensive service and engine management packages whereby Turbomeca undertakes to guarantee its operator's engine availability and care. From basic engine support requirement to fully comprehensive range of additional services, three different types of packages are offered to operators:Pro, Prime and Privilege. Turbomeca Internet Web Site - TOOLS Turbomeca's Operator On-Line Support (TOOLS site) is entirely dedicated to helping customers. With 24/7 availability, operators can access important information when they want to from where they want to, winning precious time and staying head. TOOLS at www.turbomeca-support.com

7.7 Training With more than 50 years of experience, the Airbus Helicopters training centers provide the most comprehensive, coherent and highest standard helicopter training in the world for pilots and technicians, whether civilian or military. Qualification training, allowing operators to comply with regulatory requirements, and services training, more mission oriented and tailored to the customers’ operational needs, are addressed. All training courses are established according to the relevant civil aviation authorities’ requirements. The centers are approved by the relevant airworthiness authorities (EASA, FAA, DGAC, LBA, CAA…). We are certified ISO 9001: V2000 and regularly audited by independent organisms such as Véritas, AFAQ… Airbus Helicopters training centers provide a wide range of courses and services, from basic training up to preparation for the most sophisticated civil and military missions. As part of the full range of services on offer, Airbus Helicopters also plays an active role in helicopter pilot development through its Ab Initio programs. Centers are equipped with multimedia classrooms. This includes computers overhead projectors and state-of-the-art means such as Computer Aided Instruction (CAI), Computer Based Training (CBT). Some centers also have self-learning laboratories. Airbus Helicopters has set up a network of 25training centers. For detailed information refer to Airbus Helicopters specific publication.

Technical Data

62 130 T2 14.101.01 E


EC130 - Example of basic training course

COURSE TYPE COURSE REFERENCE THEORETICAL

INSTRUCTION FSTD FLIGHT INSTRUCTION

Pilots Initial Type Rating - VFR 1 week 6 hours 6 hours Type Rating Instruction 6 days - 7 hours

COURSE TYPE COURSE REFERENCE THEORETICAL INSTRUCTION

Technicians Airframe Type Rating

(+ Engine) 5 weeks

Avionic Type Rating 3 week Blades Maintenance and repair up To 2 weeks

Note: Training duration and content are given as information and depend on pilot or technician qualification

or experience and the configuration of the aircraft. Complementary courses may be required. FSTD: Flight Simulation Training Device.

7.8 Engine Training Courses Training courses dedicated to Engine Maintenance is also organized by Turbomeca training schools and approved centers the world over. Up-to-date course calendars, on-line tests and e-learning modules are also available on the Turbomeca Operator On-Line Support (TOOLS site).

7.9 Technical Publication Airbus Helicopters provides all the technical publications necessary for safely operating and maintaining its aircraft cost effectively. Airbus Helicopters technical publications are available on an interactive electronic medium as a standard or in hard copies as an option. The INDOC DVD-ROM includes the Aircraft Maintenance Manual (AMM), System Description Section (SDS), Master Servicing Manual (MSM), Illustrated Parts Catalogue (IPC) and the Wiring Diagram Manual (WDM). The component maintenance manual (CMM) is available on DVD-ROM or hard copy, depending on the Vendor. Along with the INDOC DVD-ROM, provides a hard copy of the Airworthiness Technical Publication (Flight Manual, Master Servicing Manual …) as well as the Service Bulletin Catalog. The DVD ROM is available in English or French language; it includes the latest technical information available and is updated on a regular basis.

Technical Data

130 T2 14.101.01 E 63


7.10 T.I.P.I. (Technical Information Publication on Internet) Description T.I.P.I. website is entirely dedicated to provide a real-time issuing service for the following publications:

Emergency Alert Service Bulletin (formerly Telex Alert), Alert Service Bulletin , Safety Information Notice (formerly Telex Information), Service Bulletin, Information Notice (formerly Service Letter,), Technical Information Letter.

Airworthiness Limitations Section (ALS). FLM revisions. List of Applicable Publications (LOAP). List of Master Minimum Equipment List (MMEL). T.I.P. (Technical Improvement Proposal). Flight Ops Briefing Notes (please refer to § Customer Flight Operations Support & Services).

Main features

Each time a publication is issued, the customer is automatically informed by an e-mail. The download of the publication in pdf format is possible either directly from the e-mail or after

logging on the T.I.P.I. website. A keywords search tool is provided (aircraft family, type of publication, date of edition...).

Address: https://www.airbushelicopters/techpub/ The publications are available in English, French or German depending on the case.

A small summary, already included in the e-mail, helps the customer to understand quickly the subject.

Small icons allow the customer to identify immediately the type of information received.

7.11 Customer Flight Operations Support & Services This new set of support & services activities aims at answering all operational related constraints and issues met by Pilots and Operations Departments. On line Support (Crew Help Desk) The Crew Help Desk is dedicated to Customers’ aircrew & Flight Operations managers and is aimed at reinforcing Flight Safety and operational efficiency. It provides answers to queries relative to best knowledge and operation of the helicopter The Crew Help Desk support is ensured through the worldwide Airbus Helicopters Group network in order to rely on the community relationship. The Crew Help Desk support is free of charge. On site Support (Pilot Assistance) Through the on-site pilot assistance package, Airbus Helicopters provide Customers’ pilots complementary knowledge on the new helicopter and also on how to master the associated mission systems and equipment in Customer’s specific operational environments. Available for civil and military operations, it is built according to Customer’s specific needs and is held at Customer’s desired location. This pilot assistance can be provided at helicopter delivery, and also upon request at any time.

Technical Data

64 130 T2 14.101.01 E


Operational Documentation (Pilots Check-list) These abbreviated check-lists present standard operating procedures based on Customer’s flight manual. Even if they do not supersede the information of the Flight Manual, the check-lists hey will be updated by Normal Revision (RN) according to the Flight Manual revisions, each time these revisions impact the normal or the emergency procedures. The check lists are provided in PDF format, in English language. Operational Documentation (Flight Ops Briefing Note: FOBN) Customers Flight Ops Department publishes on Customer or Internal request briefing note to address Fleet Safety and Ops Procedures needs. The FOBN are distributed free of charge on T.I.P.I. Safety Management System Services A Safety Management System (SMS) is a structured approach to safety management, which encompasses the organizational structures, responsibilities, policies and procedures necessary in order to ensure safe operations of a company. Eurocopter International Services (EIS) consulting division can support the introduction of SMS in Customer’s organization. EIS consulting experts have extensive operational and technical knowledge and can provide practical solutions tailored to Customer’s needs.

Technical Data

130 T2 14.101.01 E 65


8 Abbreviations Abbreviation Meaning AEO All Engines Operative AFAQ Association Francaise d'Assurance Qualité AGL Above Ground Level ALS Airworthiness Limitations Section AMM Aircraft Maintenance Manual AOG Aircraft On Ground CAA Civil Aviation Authority CAI Computer Aided Instruction CBT Computer Based Training CMM Component Maintenance Manual DA Density Altitude DGAC Direction Générale de l´Aviation Civile DMC Direct Maintenance Cost EASA European Aviation Safety Agency FAA Federal Aviation Administration FH Flight Hour FLM Flight Manual GCNP Grand Canyon National Park GPS Global Positioning System ICAO International Civil Aviation Organisation IFR Instrument Flight Rules IGE In Ground Effect IPC Illustrated Parts Catalogue ISA International Standard Atmosphere JAA Joint Aviation Authorities JAR Joint Aviation Requirements LBA Luftfahrt-Bundesamt LOAP List of Applicable Publications MCP Maximum Continuous Power MMEL List of Master Minimum Equipment List MMH Mean Man Hour MSM Master Servicing Manual OEI One Engine Inoperative OEM Original Equipment Manufacturer OGE Out of Ground Effect PA Pressure Altitude PBH Parts By the Hour RAM Reliability, Availability and Maintainability SBH Support By the Hour SDS System Description Section SL Sea Level SLL Service Life Limit TAS True Air Speed TAT Turn Around Time TBO Time Between Overhauls TIPI Technical Information Publication on Internet TOOLS Turbomeca Operator On-Line Support TOP Take-Off Power UMIP Unscheduled Maintenance Insurance Plan

Technical Data

66 130 T2 14.101.01 E


Abbreviation Meaning VEMD Vehicle and Engine Multifunction Display VFR Visual Flight Rules VNE Never Exceed Speed VTOL Vertical Take-Off and Landing Vtoss Take-off safety speed Vy Optimum climbing speed Vz Rate-of-climb WDM Wiring Diagram Manual

Technical Data

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Manufacturer's notes

Airbus Helicopters 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 Airbus Helicopters.

Image(s) (i.e. photos, general drawings, pictures, diagrams) is (are) an example only.

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.

Airbus Helicopters, its logo, EC130 T2, COLIBRI, FENESTRON, SPHERIFLEX, VEMD, STYLENCE are trade marks of the Airbus Helicopters group.

Technical Data

68 130 T2 14.101.01 E


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Designed by AIRBUS HELICOPTERS

Photos: © AIRBUS HELICOPTERS

Cover photo: © Anthony Pecchi - 2013

Printed by I & D (France)

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© AIRBUS HELICOPTERS, Aeroport International

Marseille Provence - 13725 Marignane Cedex -

France

2014 - All rights reserved

Airbus Helicopters’ logo and the names of its

products and services are registered trademarks.

Airbus Helicopters 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 Airbus Helicopters.