EC130 T2
Technical Data 2014
130 T2
Technical Data
SINGLE ENGINE
ECUREUIL (Civil Version)
TWIN ENGINE
Ecureuil AS350 B2
Ecureuil AS355 NP
Ecureuil AS350 B3e
Ecureuil EC130 T2
FENNEC (Military Version)
Fennec AS550 C3e
Technical Data
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
5
4.1
Passenger Transport Mission ..................................................................................... 17
4.2
Aerial Work Mission .................................................................................................... 21
4.3
Corporate Transport Mission (STYLENCE) ............................................................... 25
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
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Abbreviations ...................................................................................................................... 65
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.
Technical Data
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130 T2 14.101.01 E
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.
Technical Data
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 dualhydraulics 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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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.
Technical Data
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130 T2 14.101.01 E
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.
Technical Data
2
General Characteristics
2.1
Cockpit and Cabin Layouts
2.2
Passenger-transport Cargo carrying
1 pilot + 6 passengers in standard version 1 1 pilot + 7 passengers in "8 seats layout" version
1 pilot + 3.7 m³ (130.7 ft³) load in cabin
Weight
Empty weight, Baseline Aircraft Definition 2 Useful load, Baseline Aircraft Definition Maximum take-off weight (MTOW) Maximum take-off weight with external load
Maximum cargo-sling load
kg
1,433 3 1,067 2,500 3,050
lb
3,159 2,352 5,512 6,724
1,500
3,307
Note: Empty weight accuracy: within r 2 %
2.3
Power Ratings 1 Turbomeca ARRIEL 2D turboshaft engine EC130 T2 Thermodynamic Power, in standard atm., at SL. 4 Take-off power Maximum continuous power
2.4
kW 710 638
shp 952 856
Fuel Capacities
liters 540
Crashworthy fuel tank
US gal. 143
kg 426
lb
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
Margin with respect to the US Grand Canyon Nation Park For 6 passengers seats
1
2 3 4 5
For 7 passengers seats
(- 5.9 dB / ICAO and FAR limits)
5
(- 0.7 dB SEL / GCNP limit = 81.8 dB SEL) (- 1.3 dB SEL / GCNP limit = 82.4 dB SEL)
If required by the local airworthiness authorities, the capacity can be limited to 1 pilot + 5 passengers. Baseline aircraft empty weight includes oil and unusable fuel. Empty weight according to baseline aircraft definition, as defined in pages 12 and 13, including the avionics suite. These engine ratings are subject to other limitations. Please refer to the Flight Manual. GCNP = Grand Canyon National Park.
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The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is 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.
Technical Data
2.6
6
External Dimensions
130 T2 14.101.01 E
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.
Technical Data
2.7
Internal Dimensions Surface A Volume
CABIN
3,00 m² 32.3 ft² 3.7 m³ 130.7 ft³
LH HOLD Surface Volume
0.52 m² 5.60 ft² 0.285 m³ 10.06 ft³
RH HOLD Surface Volume
0.47 m² 5.06 ft² 0.254 m³ 8.970 ft³
REAR HOLD Surface Volume
0.55 m² 5.92 ft² 0.565 m³ 19.95 ft³
TOTAL HOLDS Surface Volume
130 T2 14.101.01 E
1.59 m² 17.12 ft² 1.135 m³ 40.07 ft³
7
The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. 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.
Technical Data
2.8
Configurations Standard Layout
8 seats Layout
Note: 8 seats layout is an option to be contracted specifically.
8
130 T2 14.101.01 E
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.
Technical Data
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).
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The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is 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.
Technical Data
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.
10
130 T2 14.101.01 E
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.
Technical Data
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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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.
Technical Data
3
12
Baseline Aircraft Definition
130 T2 14.100.01 E
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.
Technical Data
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The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. 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.
Technical Data
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130 T2 14.101.01 E
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.
Technical Data
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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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.
Technical Data
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130 T2 14.101.01 E
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.
Technical Data
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
Empty weight, passenger transport mission configuration (including engine oil and unusable fuel) Useful load Maximum all-up weight
lb
1,509
3,327
991 2,500
2,184 5,511
Notes: Empty weight accuracy within r 2 % Including 7 headsets.
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The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is 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.
Technical Data
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)
08-00025-C 06-67076-A
08-00025-02-CI
VFR day and night package, included in baseline definition
Emergency locator transmitter - Kannad (Orolia group) INTEGRA 406 AP-H
1433.0
3159.2
0.0
0.0
4.0
8.8
1.9
4.2
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.
VHF/VOR/LOC/GS Honeywell KX165A
08-11010-A 08-16002-A
Intercom system (ICS) Garmin GMA340H Includes the passenger interphone function. ICS compatible with High level / High impedance headsets.
Transponder (mode S) - Garmin GTX 330
08-22016-B
The mode S identification must be communicated by the customer two months at the latest before the delivery.
VHF/VOR/LOC/GS/GPS Garmin GNS 430W
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.
Gyro-horizon Thales H 321 EGM
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
08-57002-A 08-63006-A
Altitude encoder - Shadin 8800 T
With a selector switch for NAV1/NAV2 selection.
Turn and Bank indicator UI 9560
General Equipment 05-02068-A
05-02068-00-CI
Enhanced exterior painting 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 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
18
130 T2 14.101.01 E
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.
Technical Data
Mission Configuration (continued) Document reference
Commercial 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
3.6
7.9
8.0
17.6
0.5
1.1
5.6
12.3
3.1
6.8
0.0
0.0
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 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 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 High level / High impedance headset.
08-21008-A
08-21008-06-CI
Radio altimeter Thales AHV16 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 May be a mandatory equipment, required by Local Airworthiness Authorities or operational regulations. Fitted with independant battery.
08-83017-A
08-83017-00-CI
VEMD data download kit 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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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.
Technical Data
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130 T2 14.101.01 E
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.
Technical Data
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
Empty weight, aerial work mission configuration (including engine oil and unusable fuel) Useful load Maximum all-up weight Maximum cargo-sling load Maximum all-up weight in external load configuration
130 T2 14.101.01 E
lb On request
On request 2,500 5,511 1,500 3,307 3,050 6,724
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The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is 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.
Technical Data
4.2.1
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)
08-00025-C 06-67076-A
08-00025-02-CI
VFR day and night package, included in baseline definition
Emergency locator transmitter - Kannad (Orolia group) INTEGRA 406 AP-H
1433.0
3159.2
0.0
0.0
1.0
2.2
1.9
4.2
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
VHF/VOR/LOC/GS Honeywell KX165A
08-22016-B
Transponder (mode S) - Garmin GTX 330
Intercom system (ICS) Garmin GMA340H Includes the passenger interphone function. ICS compatible with High level / High impedance headsets. The mode S identification must be communicated by the customer two months at the latest before the delivery.
VHF/VOR/LOC/GS/GPS Garmin GNS 430W
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.
Gyro-horizon Thales H 321 EGM
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
08-57002-A 08-63006-A
Altitude encoder - Shadin 8800 T
With a selector switch for NAV1/NAV2 selection.
Turn and Bank indicator UI 9560
General Equipment 05-02079-A
05-02079-00-CI
Engine exhaust area black thermal painting 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 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
0.0
0.0
The EAPS is recommended for flights in sandy environment and mandatory for flights in falling snow conditions.
05-25029-A
05-25029-00-CI
Heavy duty blade pins Recommended for operations in sandy and abrasive conditions.
05-32012-A
05-32012-00-CI
Pilot's windshield wiper
On request
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130 T2 14.101.01 E
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.
Technical Data
Mission Configuration (continued) Document reference
Commercial reference
Description
kg
lb
Specific Mission Equipment 06-11006-A 06-26026-A
06-11006-00-CI 06-26026-00-CI-ECL
Short protective skid shoes Dual external cargo sling mirrors
2.5
5.5
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
06-42017-A
06-42017-00-CI
Landing light adjustable in site and azimuth
4.3
9.5
0.5
1.1
0.0
0.0
May be a mandatory equipment, required by Local Airworthiness Authorities or operational regulations.
Avionics 08-18035-A
08-18035-00-CI
Headset - David Clark H10-13H High level / High impedance headset.
08-83017-A
08-83017-00-CI
VEMD data download kit 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).
130 T2 14.101.01 E
23
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.
Technical Data
Blank
24
130 T2 14.101.01 E
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.
Technical Data
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
Empty weight, corporate transport mission configuration (including engine oil and unusable fuel) Useful load Maximum all-up weight
130 T2 14.101.01 E
lb
On request On request 2,500 5,511
25
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.
Technical Data
4.3.1
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)
08-00025-C 06-67076-A
08-00025-02-CI
VFR day and night package, included in baseline definition
Emergency locator transmitter - Kannad (Orolia group) INTEGRA 406 AP-H
1433.0
3159.2
0.0
0.0
4.0
8.8
1.0
2.2
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.
VHF/VOR/LOC/GS Honeywell KX165A
08-11010-A 08-16002-A
Intercom system (ICS) Garmin GMA340H Includes the passenger interphone function. ICS compatible with High level / High impedance headsets.
Transponder (mode S) - Garmin GTX 330
08-22016-B
The mode S identification must be communicated by the customer two months at the latest before the delivery.
VHF/VOR/LOC/GS/GPS Garmin GNS 430W
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.
Gyro-horizon Thales H 321 EGM
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
08-57002-A 08-63006-A
Altitude encoder - Shadin 8800 T
With a selector switch for NAV1/NAV2 selection.
Turn and Bank indicator UI 9560
General Equipment 05-02068-A
05-02068-01-CI
Complex exterior painting 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 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.
05-23005-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
26
130 T2 14.101.01 E
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.
Technical Data
Mission Configuration (continued) Document reference
Commercial 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
3.6
7.9
8.0
17.6
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 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 In order to tune the weight and balance of the aircraft by the operator for customized configurations.
Interior Layout 07-00021-C
07-00021-02-CI
On request
STYLENCE layout
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
0.5
1.1
5.6
12.3
3.1
6.8
0.0
0.0
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 High level / High impedance headset.
08-21008-A
08-21008-06-CI
Radio altimeter Thales AHV16 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 May be a mandatory equipment, required by Local Airworthiness Authorities or operational regulations. Fitted with independant battery.
08-83017-A
08-83017-00-CI
VEMD data download kit 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).
130 T2 14.101.01 E
27
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.
Technical Data
Blank
28
130 T2 14.101.01 E
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.
Technical Data
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
Commercial 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
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 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
05-02079-A
05-02079-00-CI
Engine exhaust area black thermal painting
On request 1.0
2.2
1.9
4.0
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 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
05-23005-A
05-23005-00-CI
Engine flushing device without removal of cowlings
0.8
1.8
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
0.0
0.0
The EAPS is recommended for flights in sandy environment and mandatory for flights in falling snow conditions.
05-25029-A
05-25029-00-CI
Heavy duty blade pins 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
05-32012-A
05-32012-00-CI
Pilot's windshield wiper
On request
05-37015-A
05-37015-00-CI
Dual controls
2.6
5.7
05-42025-B
05-42025-03-CI
Enhanced Air conditioning system
33.5
73.9
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
0.0
0.0
For rough weather conditions.
05-92016-A
05-92016-00-RP
Folding of main rotor blades - Removable Parts The Removable Parts are delivered as Ground Support Equipment.
130 T2 14.101.01 E
29
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.
Technical Data
Document reference
Commercial reference
Description
kg
lb
Short protective skid shoes
2.5
5.5
Dual external cargo sling mirrors
On request
Specific Mission Equipment 06-11006-A 06-26026-A
06-11006-00-CI 06-26026-00-CI-ECL
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
06-42017-A
06-27048-00-FP
Cargo sling (1500kg) - Fixed Parts
On request
06-27048-00-RP
Cargo sling (1500kg) - Removable Parts
On request
06-42017-00-CI
Landing light adjustable in site and azimuth
4.3
9.5
3.6
7.9
57.4
126.5
8.0
17.6
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 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.
06-61006-A
06-61006-00-RP
Emergency floatation gear - Removable Parts May be a mandatory equipment, required by Local Airworthiness Authorities or operational regulations.
06-93000-A
06-93000-00-CI
Additional ballast plates in tail boom In order to tune the weight and balance of the aircraft by the operator for customized configurations.
Interior Layout 07-00021-C
07-00021-02-CI
STYLENCE Layout
07-24005-A
07-24005-00-CI
8 Energy-absorbing seats layout.
On request 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
08-18035-00-CI
Headset - David Clark H10-13H
0.5
1.1
1.0
2.2
0.5
1.1
5.6
12.3
Avionics 08-18035-A
High level / High impedance headset.
08-18037-A
08-18037-01-CI
ICS installation compatible with Bose headset 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 High level / High impedance headset.
08-21008-A
08-21008-06-CI
Radio altimeter Thales AHV16 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.
08-51015-B
08-51015-01-CI
Stand-by gyro-horizon Thales H321EGM
3.8
8.4
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
0.0
0.0
May be a mandatory equipment, required by Local Airworthiness Authorities or operational regulations. Fitted with independant battery.
08-83017-A
08-83017-00-CI
VEMD data download kit 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).
30
130 T2 14.101.01 E
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.
Technical Data
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 lb
1,800 3,968
2,000 4,409
2,200 4,850
2,300 5,071
2,400 5,291
2,500 5,512
Max. speed, VNE
km/h kts
Fast cruise speed (at MCP)
km/h kts
247 133
244 132
242 130
240 129
238 128
236 127
Recommended cruise speed
km/h kts
222 120
222 120
222 120
222 120
222 120
222 120
Fuel consumption at fast cruise speed
kg/h lb/h
169 372
169 373
169 373
169 373
169 373
169 373
Fuel consumption at recommended cruise speed
kg/h lb/h
148 326
150 331
153 337
154 339
156 343
157 346
Rate-of-climb
m/s ft/min
12 2,235
11 2,070
10 1,895
9 1,800
9 1,700
8 1,600
Hover ceiling I.G.E. at Take-Off Power z ISA
m ft m ft
6,370 20,900 5,600 18,385
5,425 17,805 4,640 15,230
4,530 14,870 3,735 12,270
4,105 13,470 3,295 10,815
3,690 12,115 2,865 9,400
3,435* 11,270* 2,590* 8,510*
m ft m ft
5,940 19,500 5,155 16,915
4,975 16,335 4,165 13,675
4,060 13,325 3,225 10,585
3,625 11,905 2,770 9,090
3,210 10,540 2,325 7,640
2,950* 9,675* 2,040* 6,700*
m ft m ft
>7,010 >23,000 7,010 23,000
7,010 23,000 6,605 21,678
6,685 21,945 5,760 18,903
6,295 20,660 5,340 17,531
5,885 19,320 4,925 16,168
5,510 18,085 4,550 14,942
km n.m
424 229
625 337
617 333
614 331
610 329
606 327
km n.m
437 236
642 346
632 341
626 338
621 335
616 332
h / min
2:52
4:12
4:08
4:06
4:03
4:00
z
Hover ceiling O.G.E. at Take-Off Power z ISA z
ISA + 20°C
Service ceiling (Vz = 0,5 m/sec. – 100 ft/min.) z ISA z
ISA + 20°C
ISA+ 20°C
Range (without fuel reserve, at fast cruise speed) z with standard tanks Range (without fuel reserve, at recommended cruise speed) z with standard tanks Endurance (without reserve)
*
287 155
287 155
287 155
287 155
287 155
287 155
Performance demonstrated for 2,465 kg (5,434 lb).
130 T2 14.101.01 E
31
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.
Technical Data
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 z Flight
7,010 m – 23,000 ft (PA)
Temperature z Maximum z Minimum
ISA + 35°C limited to 50°C - 40°C (basic)
Units nm kts: ft/min m/s °C
32
nautical miles Knots feet/minute meters per seconds degrees Celsius
hr:min kg lb km
hours:minutes kilograms pounds kilometers
130 T2 14.101.01 E
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.
Technical Data
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
130 T2 14.101.01 E
33
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.
Technical Data
HOVER CEILING I.G.E. at maximum TOP (Height 5 ft)
Zp (m) 7000
17 00
ISA
20000
5 +3
5000
15 00
00
20
6000
0 20 00 21 00 22 00 23 00 24 0 24 0 65
16
+ ISA
19 0
ISA
18 00
ISO-(kg) (ft)
15000
4000
3000
10000
25 00
2000 5000 1000
0 -40 -30 -20 -10 0
0 10 20 30 40 50 OAT (°C)
Note:
34
Approved performance, as long as the engine meets the power check criteria, as defined in the Flight Manual.
130 T2 14.101.01 E
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.
Technical Data
HOVER CEILING O.G.E. at maximum TOP
Zp (m) 7000
0
00
20000
5 +3
20
19
ISA
18 0
15 00 + ISA
0
ISA
6000
16 00
17 0
ISO-(kg) (ft)
20 00 21
00
5000
22
4000
24 0 24 0 65
3000
00 23 00
15000
10000
25 00
25 00
26 00 27 0 28 0 00
2000
5000
29 00
1000
3 30 000 50
0 -40 -30 -20 -10 0
0 10 20 30 40 50 OAT (°C)
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.
130 T2 14.101.01 E
35
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.
Technical Data
FAST CRUISE SPEED ISA
Zp (m) 7000
20 00
19
00
18 00
17 00
00 15 00
21 00 22 00 23 00
16
6000
ISO-Weight (kg) (ft)
20000
24 00 25 00
5000
15000 4000 10000
3000 2000
5000 1000 0
0 140 160 180 200 220 240 260 280 True Air Speed (km/h) 80
Note:
36
90 100 110 120 130 140 150 (kt)
Typical performance, with clean baseline aircraft and new engine.
130 T2 14.101.01 E
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.
Technical Data
FAST CRUISE SPEED ISA+20°C
Zp (m) 7000
18
00
17 00
16
00
00
5000
19 00 20 00 21 00
15
6000
ISO-Weight (kg) (ft)
20000
22 00 23 00 24 00
25
4000
15000
00
10000
3000 2000
5000 1000 0
0 140 160 180 200 220 240 260 280 True Air Speed (km/h) 80
Note:
130 T2 14.101.01 E
90 100 110 120 130 140 150 (kt)
Typical performance, with clean baseline aircraft and new engine.
37
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.
Technical Data
FAST CRUISE SPEED ISA+35°C
Zp (m) 7000
ISO-Weight (kg) (ft)
18
00
19
6000
17 00
16 00
15 00
20000
00
20 00 21 00
5000
22 00
4000
15000
23 00
2400
25 00
3000
10000
2000 5000 1000
0
0 140 160 180 200 220 240 260 280 True Air Speed (km/h) 80
Note:
38
90 100 110 120 130 140 150 (kt)
Typical performance, with clean baseline aircraft and new engine.
130 T2 14.101.01 E
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.
Technical Data
RECOMMENDED CRUISE SPEED ISA
Zp (m) 7000
ISO-M (kg) (ft) 210 0 220 0
200 0
190 0
18 00
20000
230 0
6000
240 0
250
5000
0
15000 4000 10000
3000 2000
5000 1000 0
140
160
180
200
220
0
Vp (km/h) 80
Note:
130 T2 14.101.01 E
90
100
110
120 (kt)
Typical performance, with clean baseline aircraft and new engine.
39
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.
Technical Data
RECOMMENDED CRUISE SPEED ISA+20°C
Zp (m)
ISO-Weight (kg) (ft)
7000
180
190 0
210
6000
0
200 0
17 00
0
16 0
0
20000
220 0
5000
240 0
230 0
15000 250
4000
0
10000
3000 2000
5000 1000 0
140
160
180
200
220
0
TAS (km/h) 80
Note:
40
90
100
110
120 (kt)
Typical performance, with clean baseline aircraft and new engine.
130 T2 14.101.01 E
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.
Technical Data
RECOMMENDED CRUISE SPEED ISA+35°C
Zp (m) 7000
ISO-Weight (kg) (ft) 180 0
17 00
0
15 00
20000
19 00
6000
21
5000
20 00 00
22
4000
16 0
23
15000
00
00
2400
3000
10000
25 00
2000 5000 1000
0
140
160
180
200
220
0
TAS (km/h) 80
Note:
130 T2 14.101.01 E
90
100
110
120 (kt)
Typical performance, with clean baseline aircraft and new engine.
41
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.
Technical Data
RATE OF CLIMB IN OBLIQUE FLIGHT ISA
Zp (m) 7000
ISO-Weight (kg) (ft)
00 15 00 16 00 17 00 18 00 19 00 20 00 21 0 0 0 22 230
6000
20000
00 00 2 4 25
5000
15000 4000
10000
3000
2000 5000 1000
0
0
0 500 1000 1500 2000 2500 3000 Rate of Climb (ft/mn)
0
10 (m/s)
Note:
42
Approved performance, as long as the engine meets the power check criteria, as defined in the Flight Manual.
130 T2 14.101.01 E
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.
Technical Data
RATE OF CLIMB IN OBLIQUE FLIGHT ISA + 20°C
Zp (m)
ISO-Weight (kg) (ft)
7000 0 15
0
00 16
00 17 00 18 00 19 00 0 20 10 00 2 22
6000
20000
00 0 23 240 500 2
5000
15000
4000
10000
3000
2000 5000 1000
0
0
0 500 1000 1500 2000 2500 3000 Rate of Climb (ft/mn)
0
10 (m/s)
Note:
130 T2 14.101.01 E
Approved performance, as long as the engine meets the power check criteria, as defined in the Flight Manual.
43
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.
Technical Data
RATE OF CLIMB IN OBLIQUE FLIGHT ISA + 35°C
Zp (m)
ISO-Weight (kg) (ft)
7000 00
00
00 15
16
17
20000
6000
5000 15000 4000
1800 00 19 00 20 00 21 200 2 00 23 400 0 0 2 25
3000
2000
10000
5000 1000
0
0
0 500 1000 1500 2000 2500 3000 Rate of Climb (ft/mn)
0
10
15 (m/s)
Note:
44
Approved performance, as long as the engine meets the power check criteria, as defined in the Flight Manual.
130 T2 14.101.01 E
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.
Technical Data
HOURLY FUEL CONSUMPTION at fast cruise speed ISA, ISA + 20°C, ISA + 35°C
Zp (m)
ISO-ISA (kg) (ft)
7000 A IS 20 A+ IS 35 A+ IS
6000
20000
5000 15000 4000
10000
3000
2000 5000 1000
0 80
100
120
140
160
0 180
Hourly Fuel Consumption (kg/h) 225
Note:
130 T2 14.101.01 E
275
325
375 (lb/h)
Typical consumption with clean baseline aircraft and new engine.
45
The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. 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.
Technical Data
HOURLY FUEL CONSUMPTION at recommended cruise speed ISA
00 20
21 00
5000
20000
00 18 19 00
17 0
1600
0 150
6000
ISO-Weight (kg) (ft)
0
Zp (m) 7000
4000
24 00
23
00
2
15000
0 20
3000
10000
00 25
2000 5000 1000 0 80
90
100
110
120
130
140
150
0 160
Hourly Fuel Consumption (kg/h) 225
Note:
46
275
325
(lb/h)
Typical consumption with clean baseline aircraft and new engine.
130 T2 14.101.01 E
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.
Technical Data
HOURLY FUEL CONSUMPTION at recommended cruise speed ISA + 20°C
Zp (m)
ISO-Weight (kg) (ft)
7000
22 00
210 0
20
4000
15000 00
190 0
18 00
17 00
0
20000
00 15
10000 230 0
3000
250 0
2000
24 00
5000
160
6000
5000
1000 0 80
90
100
110
120
130
140
150
0 160
Hourly Fuel Consumption (kg/h) 225
Note:
130 T2 14.101.01 E
275
325
(lb/h)
Typical consumption with clean baseline aircraft and new engine.
47
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.
Technical Data
HOURLY FUEL CONSUMPTION at recommended cruise speed ISA + 35°C
Zp (m) 00 15
7000
ISO-Weight (kg) (ft)
16 00
20000
17
6000
00 00 18
5000
19
15000
00
00 20
4000
10000
00 21
3000
00 22 00 23
2000
00 24
5000
0 80
00 25
1000
0 90 100 110 120 130 140 150 160 Hourly Fuel Consumption (kg/h) 225
Note:
48
275
325 (lb/h)
Typical consumption with clean baseline aircraft and new engine.
130 T2 14.101.01 E
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.
Technical Data
PAYLOAD RANGE ISA Fast cruise speed
Payload (kg)
(lb)
1000 2000 800 1500 600 5000ft - 1524m
0ft - 0m
400
1000
500
200
0
0
200
400
600
0 800
Range (km) 0
Notes:
x x
130 T2 14.101.01 E
100
200
300
400 (nm)
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.
49
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.
Technical Data
PAYLOAD RANGE ISA + 20°C Fast cruise speed
Payload (kg)
(lb)
1000 2000 800 1500 600 5000ft - 1524m
0ft - 0m
400
1000
500
200
0
0
200
400
600
0 800
Range (km) 0 Notes:
x x
50
100
200
300
400 (nm)
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.
130 T2 14.101.01 E
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.
Technical Data
PAYLOAD RANGE ISA + 35°C Fast cruise speed
Payload (kg)
(lb)
1000 2000 800 1500 600 24m 5000ft - 15
0ft - 0m
400
1000
500
200
0
0
200
400
600
0 800
Range (km) 0
Notes:
x x
130 T2 14.101.01 E
100
200
300
400 (nm)
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.
51
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.
Technical Data
PAYLOAD RANGE ISA Recommended cruise speed
Payload (kg)
(lb)
1000 2000 800 1500 600 m 5000ft - 1524
0ft - 0m
400
1000
500
200
0
0
200
400
600
0 800
Range (km) 0
Notes:
x x
52
100
200
300
400 (nm)
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.
130 T2 14.101.01 E
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.
Technical Data
PAYLOAD RANGE ISA + 20°C Recommended cruise speed
Payload (kg)
(lb)
1000 2000 800 1500 600 24m 5000ft - 15
0ft - 0m
400
1000
500
200
0
0
200
400
600
0 800
Range (km) 0
Notes:
x x
130 T2 14.101.01 E
100
200
300
400 (nm)
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.
53
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.
Technical Data
PAYLOD RANGE ISA + 35°C Recommended cruise speed
Payload (kg)
(lb)
1000 2000 800 1500 600 1524m 5000ft -
0ft - 0m
400
1000
500
200
0
0
200
400
600
0 800
Range (km) 0
Notes:
x x
54
100
200
300
400 (nm)
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.
130 T2 14.101.01 E
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.
Technical Data
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:
130 T2 14.101.01 E
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.
55
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.
Technical Data
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:
56
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.
130 T2 14.101.01 E
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.
Technical Data
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
Main rotor blade Sleeve Main rotor shaft unit
SLL (h) as per ASL 000 20000 4400 58000 cycles
Starflex hub Spherical thrust bearing Main gearbox bevel reduction gear Main gearbox epicyclic reduction gear Tail gearbox Blade,tail rotor Servo control, main rotor Tail rotor hub Servo control, main
3000 4600 3000 3000 4000 10000 3000 6900 20000
Engine
TBO (h)
ARRIEL 2D
4000
TBO (h) Target Value 6000
SLL (h)
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.
130 T2 14.101.01 E
57
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.
Technical Data
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 .
58
130 T2 14.101.01 E
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.
Technical Data
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.
130 T2 14.101.01 E
59
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.
Technical Data
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.
60
130 T2 14.101.01 E
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.
Technical Data
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.
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The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is 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.
Technical Data
EC130 - Example of basic training course COURSE TYPE Pilots COURSE TYPE Technicians Blades Note:
7.8
FSTD
FLIGHT INSTRUCTION
Initial Type Rating - VFR
THEORETICAL INSTRUCTION 1 week
6 hours
6 hours
Type Rating Instruction
6 days
-
7 hours
COURSE REFERENCE
COURSE REFERENCE Airframe Type Rating (+ Engine) Avionic Type Rating Maintenance and repair
THEORETICAL INSTRUCTION 5 weeks 3 week up To 2 weeks
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.
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.
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The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is 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.
Technical Data
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
7.11
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.
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.
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The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is 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.
Technical Data
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.
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The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is 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.
Technical Data
8
Abbreviations Abbreviation AEO AFAQ AGL ALS AMM AOG CAA CAI CBT CMM DA DGAC DMC EASA FAA FH FLM GCNP GPS ICAO IFR IGE IPC ISA JAA JAR LBA LOAP MCP MMEL MMH MSM OEI OEM OGE PA PBH RAM SBH SDS SL SLL TAS TAT TBO TIPI TOOLS TOP UMIP
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Meaning All Engines Operative Association Francaise d'Assurance Qualité Above Ground Level Airworthiness Limitations Section Aircraft Maintenance Manual Aircraft On Ground Civil Aviation Authority Computer Aided Instruction Computer Based Training Component Maintenance Manual Density Altitude Direction Générale de l´Aviation Civile Direct Maintenance Cost European Aviation Safety Agency Federal Aviation Administration Flight Hour Flight Manual Grand Canyon National Park Global Positioning System International Civil Aviation Organisation Instrument Flight Rules In Ground Effect Illustrated Parts Catalogue International Standard Atmosphere Joint Aviation Authorities Joint Aviation Requirements Luftfahrt-Bundesamt List of Applicable Publications Maximum Continuous Power List of Master Minimum Equipment List Mean Man Hour Master Servicing Manual One Engine Inoperative Original Equipment Manufacturer Out of Ground Effect Pressure Altitude Parts By the Hour Reliability, Availability and Maintainability Support By the Hour System Description Section Sea Level Service Life Limit True Air Speed Turn Around Time Time Between Overhauls Technical Information Publication on Internet Turbomeca Operator On-Line Support Take-Off Power Unscheduled Maintenance Insurance Plan
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The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is 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.
Technical Data
Abbreviation VEMD VFR VNE VTOL Vtoss Vy Vz WDM
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Meaning Vehicle and Engine Multifunction Display Visual Flight Rules Never Exceed Speed Vertical Take-Off and Landing Take-off safety speed Optimum climbing speed Rate-of-climb Wiring Diagram Manual
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The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is 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.
Technical Data
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.
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The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is 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.
Technical Data
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The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. 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.
© 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. Designed by AIRBUS HELICOPTERS Photos: © AIRBUS HELICOPTERS Cover photo: © Anthony Pecchi - 2013 Printed by I & D (France)
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