145_D-2_18.101.01_E_Technical_Data _LQ_

Technical Data

Contents 1 For ewo eword rd ................................................................................ ........................................ 3 2 General Charact eris ti cs ....... .............. .............. .............. .............. .............. .............. .............. .............. .............. ............. ............. .............. ........... .... 13 2.1 2.2 2.3 2.4 2.5 2.6 2.7

Cockpit and Cabin Layouts ................................... ..... .............................. ............................ ............................. ...... Weight ........................... .............................. .............................. ............................ ............... Power Ratings ............................ ............................. .............................. ............................... Fuel Capacities ...................................... .......... ............................ .............................. .............................. .................. External Dimensions ............................ .............................. ............................. ..................... Internal Dimensions ................ ............................ ............................ ............................ ......... External Sound Levels .................... ............................... ............................... .......................

13 13 13 14 15 16 17

3 Baseli ne Airc Ai rc raft Defin Definit it io ion n ........ ............... .............. .............. .............. .............. ............. ............. .............. .............. .............. ............. ........... ..... 19 4 Miss io ion n Confi Con fi gu gurati rati on ons s ...... ............. .............. .............. .............. .............. .............. ............. ............. .............. .............. .............. .............. ............ ..... 21 4.1 4.2 4.3 4.4

Emergency Medical Medical Services Services - EMS Mission ................................ ................................ ...... Offshore Transportation Mission .................................... ............................ .......................... Law Enforcement Mission ................................. ............................. ............................. ......... Aerial Work Mission ................................... ... ................................ ............................... ............................... ............

22 29 37 45

5 Equ ip ipment ment Inf Infor ormati mati on ....... .............. .............. .............. .............. ............. ............. .............. .............. .............. .............. ............... .............. ........... ..... 51 5.1 5.2 5.3 5.4 5.5

General Available Equipment ........................ .............................. .............................. .......... Avionics Layouts ............................ ............................ .............................. ............................ Antenna Layout ............................................. ............................. ............................ .............. NVG friendly & NVIS Certification ......................................... ......... ................................ ............................... ................ Disclaimers .......................... ............................. .............................. .....................................

51 57 59 59 60

6 Main Perfo rm ance ....... ............. ............. .............. .............. .............. ............. ............. .............. .............. .............. .............. .............. ............. ............. ......... 63 6.1 Performance Summary Tables ............................... ................................ ............................. 63 6.2 Operating Limitations ................................. ............................... ............................. .............. 66 6.3 Performance Charts ................................................ .............................. ............................... 67

7 Servi ce and Suppo rt Inf or ormati mati on ........ ............... .............. .............. .............. .............. ............... .............. ............. .............. .............. ....... 79 7.1 Assets ............................................ ............................ .............................. ............................ 7.2 H145 Inspection Programs ........................... ............................. ............................ .............. 7.3 Main Components ........................................... ............................. .............................. .......... 7.4 HCare - Material Management ............................ ............................ ............................. ....... 7.5 Engine Service and Support Programs ............................ .............................. ..................... 7.6 HCare - Helicopter Maintenance ...................................... ................................ .................... 7.7 HCare - Technical Support ............................ .............................. .............................. .......... 7.8 HCare - Training Training & Flight Ops ...................................................... ................................ ........ 7.9 Flight Operations Services ........................ ............................ .............................. ................ 7.10 HCare - Connected Services .......................... .............................. ............................. ........

79 80 82 84 87 89 90 92 94 95

8 Ab Abbr breviat eviat io ions ns ....... .............. ............... ............... ............. ............. .............. .............. .............. ............... ............... ............. ............. .............. .............. ............ ..... 97

145 D-2 18.101.01 E

1

The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. 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 ® 2018 – All rights reserved.

Technical Data

Blank

2

145 D-2 18.101.01 E

The data set forth in t his 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 ® 2018 – All rights reserved.

Technical Data

1

Foreword

Figure 1.1: Example of the H145

The H145® is Airbus® new 3-4 ton class twin-engine, multi-purpose helicopter. It can accommodate up to 12 seats for pilot/s and passengers. It is certified under the name BK117 D-2. The H145 represents a major evolution in terms of flight performance, mission capability, flight safety and cost of operations. As a further evolution of the BK117 family, the H145 provides latest technologies, like the advanced cockpit design with the most modern Human Machine Interface (HMI) and state-of-the-art Helionix ® avionics, new more powerful engines, an enhanced transmission system and a Fenestron ® antitorque-device. These new technologies are combined with the rugged and proven design elements of the EC145®, as for example the main rotor system and the multipurpose cabin. The innovative Helionix avionics system has an open architecture and modular design with very high redundancy (double duplex) incorporating embedded functions as well as the capability for further integration of mission functions. The most significant embedded function is the 4-axis dual duplex AFCS. The functionalities, level of safety and the mission capability enhancements offered by this autopilot are the most performing in the helicopter industry. The H145's hingeless rotor system with its monolithic titanium hub ('System Bölkow') is proven worldwide. Furthermore, the rotor blades are optimized to provide high performance with low sound and vibration levels. These features, combined with a Fenestron with unequal blade spacing makes the H145 the quietest helicopter in its class. In addition to environmental aspects, the rugged rotor system and airframe components together with the enhanced main gear box grant for low maintenance costs and high in-service-time of the helicopter. The new engines also significantly contribute to the reduced maintenance costs through high TBO and an evolved maintenance concept with usage monitoring, which increases the availability of the engine.

145 D-2 18.101.01 E

3

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 ® 2018 – All rights reserved.

Technical Data

The H145 is equipped with two very powerful Safran Helicopter Engines Arriel 2E engines, each controlled by a dual channel FADEC, which, in combination with its lifting system, provide outstanding performance in AEO operations and vital power reserves in One Engine Inoperative (OEI) scenarios. The H145 allows Cat. A VTOL operation up to the level of performance class 1 according to EASA OPS with full MTOW at SL and ISA. Twin-engine reliability is complemented by a fully separated fuel supply system, a duplex hydraulic system, dual electrical system and redundant lubrication for the main transmission. A key safety aspect of the H145 is its inherent crashworthiness thanks to energy absorbing fuselage and seats, as well as crash resistant fuel cells. The Fenestron anti-torque-device increases significantly the safety in flight and on ground. A wide range of rapidly interchangeable optional equipment, such as emergency floats, rescue hoist, searchlight and cargo hook is available for the H145. Together with its inherently versatile cabin layout, the H145 is ready to take on diverse missions; from EMS, passenger transport, to internal and external load transport, law enforcement and offshore transportation.

Spacious cabin The H145 cabin is in a class of its own and features: • Excellent outside visibility for pilot/s, crew and/or passengers • Roomy cabin with no partitions or protrusions, no center post, no door post • Unrivalled side loading (no door posts) and rear loading capability • Flat floor all over the entire cabin area

Figure 1.2: View from rear into the empty cabin

4

145 D-2 18.101.01 E


Technical Data

Ad vanced gl ass co ck pit - f li ght an d mis si on management The H145 offers a glass cockpit solution with a highly efficient HMI designed to reduce the pilot workload and increase the flight safety. The avionics system, Helionix, is the latest generation of Airbus avionics family, designed to provide enhanced safety and mission capability along with simplified maintainability. Helionix benefits from the long experience accumulated by Airbus in the development of innovative avionics. The Helionix Flight Display Subsystem (FDS) is composed of 3 Smart Multifunction Displays (MFD) providing state-of-the-art quality and precision imaging of flight parameters, as well as mission equipment from a moving map functionality to a High Definition (HD) Electro Optical System. The pilot display offers all the flight, navigation and vehicle relevant data while the remaining displays are configurable for flight, vehicle or mission data. All Active Matrix Liquid Crystal Displays (AMLCD) feature perfect readability from any angle and in any light condition. With the Helionix suite, the flight crew will experience: • Enhanced pilot assistance thanks to the most advanced 4-axis digital AFCS with innovative upper modes expanding the aircraft capabilities in particular in low visibility conditions and over water, SAR, for both day and night missions • Enhanced situation awareness with integrated Helicopter Terrain Awareness and Warning System (H-TAWS), Synthetic Vision System (SVS) and moving map as optional equipment. • Reduced pilot workload with innovative crew alerting concept such as the one hundred feet alert (required by EASA OPS) and Vehicle Management System (VMS) • Reduced pilot workload with an intuitive Human Machine Interface (HMI) • Unrivalled level of redundancy with all functions embedded in each MFD, dual duplex aircraft management computers and 3 Attitude and Heading Reference Sensors (AHRS), plus one Integrated Electronic Stand-by Instrument (IESI) • Full Usage Monitoring System (UMS) included in the basic Helionix package • A new concept for enhanced maintainability with user-friendly software management, failure codes recording and trouble shooting algorithm The unique color coding, warning and information concept helps the pilot/s to collect all relevant parameters while suppressing presentation of non-relevant information. Additionally, the H145's unique First Limit Indicator (FLI) considerably simplifies engine and torque monitoring. The pilot/s workload is minimized thus allowing their attention to be concentrated on the mission. A NVG layout is optionally available. In addition, the H145 digital avionics initialization procedures and self-test sequences are automatically performed in the background, minimizing the time to become airbone.

145 D-2 18.101.01 E

5


Technical Data

Ab le t o s afely f ly in IMC co ndit io ns With the autopilot, the advanced rate command / attitude and heading hold mode and upper modes significately enhance the capabilities for flight in Instrument Meteorological Conditions (IMC) and other degraded visual environments (e.g with night vision goggles).

Figure 1.3: Typical instrument panel

H145 is Airbus answer for medium weight mission systems for high demanding multipurpose requirements. Airbus has already delivered around 169 H145/H145M helicopters with total flight hours of approximately 81,000 Fh by the end of 2017.

6

145 D-2 18.101.01 E


Technical Data

Highlights and Main Improvements Al ter nat e gr os s w eight 3,800 kg For the H145 an alternate gross weight of 3,800 kg is available for customers as selectable option. With this option customers can perform day and night flights with a gross weight between 3,700 kg and 3,800 kg under Visual and Instrument Flight Rules (VFR/IFR) for Category B operations. The alternate gross weight is certified under EASA regulations. FAA certification is ongoing. The certification includes a flight envelope up to ISA +25°C and a maximum operating altitude for hover, takeoff and landing up to 5,000 ft density altitude (DA). The maximum operating altitude allows flights up to 8,000 ft pressure altitude (PA). Flights with a gross mass above 3,700 kg can be done with open or removed doors, using NVG´s and with load on the single or dual cargo hook. Not included in the certification of the alternate gross weight are operations with load on t he hoist and operations over water in a hostile environment requiring an emergency flotation system. Due to the higher loads on the helicopter a penalty factor has to be applied for each flight above 3,700 kg reducing the life time of certain components.

Offshore seating arrangement The H145 has reached certification for specific offshore seating arrangements for up to 8 passengers which are meeting the requirements of CAA Safety Directive 2015/005 and CAP 1145. Different layouts are available depending on the customer needs. Below examples show an 8 passengers offshore seating arrangement suitable for passenger transportation and a 4 passengers seating configuration suitable for offshore windfarm operations with hoist.

Figure 1.4: 8 passengers seating arrangement (left), 4 passengers seating arrangement (right)

145 D-2 18.101.01 E

7


Technical Data

DLE PC2 procedur e The DLE PC2 procedure for takeoff and landing for offshore operations on/to helidecks is now available for the H145. This procedure is characterized by: • PC2 offshore classical profiles including a low rotation point (RP), which is also in effect of the Takeoff Decision Point (TDP). • Exposure time quantification depending on takeoff and landing weight. The PC2 DLE procedure is compliant with the JAR-OPS 3 "PC2 Enhanced" (PC2e) as well as with the EASA Air Operations Regulation (EASA-OPS), Part CAT (Commercial Air Transport) which applies from 28 October 2012.

Impro ved Human External Cargo (HEC) perfo rmance The H145 flight envelope has been extended by increasing its human external cargo (HEC) capability. The H145 now offers an increased hover performance capability in One Engine Inoperative (OEI) mode within the two minutes power band (@ SL/ISA+20) allowing an additional 230 kg useful load. The upgrade was certified by the European Airworthiness Safety Agency (EASA) in March 2017. The H145' s enhanced power and load capabilities will in particular bring benefit to commercial winch operators for missions such as harbour pilot or powerline maintenance.

Electro Optic al System (EOS) Star Safir e 380HDc The Star Safire 380HDc basic system has the same technical characteristics as the Star Safire 380HD, but in a smaller and lighter turret and except for these features: • The zoom of the infrared sensor (Medium-Wafe Infra-Red - MWIR) is continuous instead of stepwise and with following zoom ranges: • 640 MWIR: 29° - 1.47° (down to 0.75° with electronic zoom) • 1280 MWIR: 40° - 2° (down to 1° with electronic zoom) • The FOV of the long range digital color camera are 25°, 3.9°, 0.7°, 0.4° and 0.2° (electronic). • Additionally a digital color camera sensor is installed: The digital color TV camera operates in the visible waveband. It provides optical zoom and the following modes and features: manual focus, manual and automatic sensitivity. These modes and features are selectable by the operator. The digital color TV camera provides a continuous zoom of 45°-1.2° (down to 0.6° with electronic zoom).

Figure 1.5: EOS, Star Safire 380HDc - Turret

8

145 D-2 18.101.01 E


Technical Data

External cameras External cameras can be mounted on the helicopter, e.g. to monitor external loads or helicopter loading observation by the crew or to support identification of obstacles behind the helicopter. The color camera provides a picture, which can be indicated on the center MFD in the cockpit. Two different camera installations are offered: • External multi-purpos e camera on tail boom The camera is installed on the tail boom in the fenestron area and features observation of the cargo hook, hoist or rope down missions and helicopter rear loading. The camera angle is pre-adjusted by means of three adjustment screws. • External rear-view camera The camera is installed under the helicopter clam-shell doors and features observation of the area behind the helicopter, which may be beneficial for rearward takeoffs.

Figure 1.6: External rear-view camera (left); external multi-purpose camera on tail boom (right)

145 D-2 18.101.01 E

9


Technical Data

Helionix improv ements The Helionix avionic system is now available in its step 3 version. It enhances the basic as well as the optional mission functions for additional safety and mission capability. • new Time Limited Dispatch for engines in order to reduce AOG • UMS data exceedance communication over satellite (requires EuroNav Skytrack Iridium satcom option) • Bigger maps (1,000 NM x 1,000 NM) • SVS with indication of obstacles, runway and helipads, cultural data (urban areas, roads, rail roads) and enhanced graphics and texture • Optional Helionix moving map with indication of airspaces and fuel range, pointer position sent to FMS, map back ground in NAVD and improved color rendering

Figure 1.7: Example of Helionix step 3

10

145 D-2 18.101.01 E


Technical Data

Basic platform computer The basic platform computer is a multipurpose airborne computer interfaced with Wi-Fi and LTE (4G) on which various applications can be installed: • Hot spot / router: provide a Wi-Fi access point for the connection of Wi-Fi capable devices and allows data exchange with the ground LTE network • Real time overlay download: allow the wireless update of different data (e.g. weather data or JEPPESEN database) from the customer ground server to the EuroNav 7. The database download is performed via Wi-Fi or LTE. If both networks are available, priority is given to Wi-Fi. • Voice over IP: allow VoIP over the LTE connection. In this case the control of the communication is done from the cockpit via EuroNav 7 where the contacts and their associated telephone numbers are saved. The communication is realized over the intercom system. • Fleet tracking: allow to receive data from the EuroNav 7 and to transmit them via the basic platform computer on the LTE network to a ground station

Figure 1.8: Flight path tracking shown on ground station (example)

Note: The basic platform computer is available on request. Please contact your Airbus helicopter sales representative.

145 D-2 18.101.01 E

11


Technical Data

Full flight s imulator The H145 simulator at the Airbus Helicopters Training Academy in Germany has been awarded level D status by the German Federal Aviation Office - the highest possible certification for a full flight simulator. With such airworthiness authority approval, more training hours accumulated by pilots in the full flight simulator are now authorized to be logged as actual flight hours. The simulator provides customers with a wide range of training opportunities, in particular for missions under extreme flight conditions and f or practicing various emergency procedures. As level D helicopter simulator it meets a number of criteria, including the ability to move in six directions, to provide a field of view of at least 180°, to work with realistic acoustic and visual simulations, and to perform several special motion effects. The H145 simulator is suitable for pilots' initial training and refresher courses, for specific instruction on emergency procedures, for flights according to Instrument Flight Rules (IFR), in offshore conditions and at night (with night vision goggles), as well as for Cat. A operations.

Blank Figure 1.9: H145 Full Flight Simulator level D

Emergency floats with integrated life rafts (DART - STC) Emergency floats with integrated life rafts (DART - STC) are available on request. The floats and the life rafts are installed on the landing gear in order to save cabin space. The system includes 4 tri bag floats for improved stability and integrated life rafts for ease of access and weight savings. The system is certified up to sea state 6. Please contact your Airbus helicopter sales r epresentative.

Figure 1.10: Emergency floats with integrated life rafts (DART - STC)

12

145 D-2 18.101.01 E


Technical Data

2

General Characteristics

2.1

Cockpit and Cabin Layouts Seats & equipment as optio n

Passenger transportation

1 or 2 pilots + up to 8 passengers in passenger seating configuration (energy absorbing individual seats) + 1.31 m³ cargo

High-density seating

1 or 2 pilots + up to 10 passengers in high-density seating configuration (energy absorbing individual troop seats)

Emergency Medical Services - 1 or 2 pilots + up to 2 stretcher patients + up to 3 HEMS crew EMS

2.2

Weight kg

lb

• Empty weight, Baseline Aircraft Definitiona

1,919

4,231

• Useful load, Baseline Aircraft Definition

1,781

3,926

85

187

1,696

3,739

• Maximum Takeoff Weight (MTOW)

3,700

8,157

• Maximum Takeoff Weight (MTOW) with external loadb

3,700

8,157

• Maximum dual cargo hook load (single hook operation)

1,600

3,527

800

1,764

• Pilot • Payload and/or fuel b

• Maximum dual cargo hook load (HEC class D operation) a. Margin ± 1,5% b. Within the AGW flight envelope up to 3,800 kg

2.3

Po wer Rat in gs Engine Ratings 2 Safran Helicopter Engines ARRIEL 2E turboshaft engines Al l En gi nes Oper ati ve (A EO)

kW

sh p

• Takeoff Power (TOP)a

667

894

• Maximum Continuous Power (MCP)

575

771

One Engine Inoperative (OEI)

kW

shp

• OEI 30 sec

800

1072

• OEI 2 min

775

1038

• OEI MCP

710

951

a. for up to 30 min

Note: Thermodynamic values per engine, in standard atmosphere, at sea level.

145 D-2 18.101.01 E

13


Technical Data

Main Transmissi on Ratings Al l En gi nes Oper ati ve (A EO)

kW

sh p

• Takeoff Power (TOP)

2 x 420

2 x 563

• Maximum Continuous Power (MCP)

2 x 327

2 x 438

kW

shp

• OEI 30 sec

1 x 662

1 x 887

• OEI 2 min

1 x 630

1 x 845

• OEI MCP

1 x 442

1 x 592

One Engine Inoperative (OEI)

2.4

Fuel Capacities Standard fuel tank configuration

Usable fuel liters

US gal

kg

lb

• Standard fuel tanks

903.8

238.8

723.0

1,593.9

• Internal long range fuel tank (option)

219.0

57.9

175.0

385.8

Note: Tolerance of fuel figures: ± 2% Fuel density used is 0.8 kg / liter

14

145 D-2 18.101.01 E


Technical Data

2.5

External Dimensions

Figure 2.1: External dimensions 145 D-2 18.101.01 E

15


Technical Data

2.6

Internal Dimensions

Figure 2.2: Internal dimensions

Floor area

16

Volume

Cabin & cargo compartment (Cargo compartment with 8 seats installed)

4.72 m² 0.84 m²

50.77 ft² 9.07 ft²

6.03 m³ 1.31 m³

212.83 ft³ 46.40 ft³

Copilot

0.72 m²

7.73 ft²

0.80 m³

28.25 ft³

Pilot (not shaded)

1.09 m²

11.80 ft²

1.24 m³

43.76 ft³

Total (undivided)

5.43 m²

58.50 ft²

6.83 m³

241.08 ft³

Total (incl. pilot station)

6.52 m²

70.30 ft²

8.07 m³

284.84 ft³

145 D-2 18.101.01 E


Technical Data

2.7

External Sound Levels Flight Phase

Measurements according ICAO An nex 16 [EPNdB]

ICAO limit s at 3,700 kg [EPNdB]

Measurements according FAR Part 36 [EPNdB]

FAR 36 limits at 3,700 kg [EPNdB]

Takeoff

86.5

95.7

86.5

95.7

Overflight

84.7

94.7

84.7

94.7

Ap pr oac h

90.3

96.7

90.3

96.7

145 D-2 18.101.01 E

17


Technical Data

Blank

18

145 D-2 18.101.01 E


Technical Data

3

Baseline Aircraft Def inition GENERAL • Energy absorbing fuselage • Tail boom with fixed horizontal stabilizer and vertical fin with faired-in Fenestron® • Upper deck with fittings for main gearbox, engines, hydraulic and cooling system • Cowlings for main transmission and engines

• Skid-type landing gear with skid protectors, capable of taking ground-handling wheels • Long boarding steps, LH and RH • Cold weather kit • Built-in maintenance steps and grips • Exterior painting (single color)

COCKPIT, CABIN AND CARGO COMPARTMENT • One-level cabin and cargo compartment floor with integrated rails • Glazed canopy • Two hinged cockpit doors with sliding window • Map case in pilot´s door • Two wide passenger sliding doors with window of pushout type • Two rear hinged clam-shell doors • Longitudinally adjustable energy absorbing pilot and copilot seats with head rest and 4-point safety belts with automatic locking system; seat color grey or blue • Cabin & cockpit boarding grips (LH and RH) • Flight controls (pilot side) • Single pilot instrument panel with glare shield

• Interior paneling • Ram-air and electrical ventilating system for cockpit and cabin • Bleed air heating system • Ventilation for avionics decka • Helmet holder in the cockpit, rotatable • Portable fire extinguisher • Stowage net for first aid kit at the LH rear clam-shell door • 2 flashlights (torches) • Slant console • Center console • Windscreen wiper for pilot and copilot • Door open warning

a. If required by final configuration

INSTRUMENTS • Flight Display Subsystem (FDS) composed of 2 smart multifunction displays (6 x 8 inch) providing the following functions: • Flight Navigation Display (FND) format (incl. PFD, FLI, Master list, NAV, RPM, mast moment & fuel indication) • Vehicle Monitoring System (VMS) format (incl. engine, gearbox, hydraulic, fuel, electrical system, RPM and clock indication) • Vehicle Management System (VMS) including: • 2 duplex Aircraft Management Computer (AMC) • Reference sensors: • 3 Attitude and Heading Reference Systems (AHRS) • 2 Air Data sensors (electrically heated pitot tube and static port) • 2 Three Axis Magnetometers (TAM) • Stand-by instruments: • Integrated Electronic Standby Instrument (IESI) • Stand-by compass

• • • •

•

Usage Monitoring System (UMS) „One hundred feet“ alert Directional Gyro Free Steering Mode Warning unit: • Engine fire warning with fuel emergency shut-off • Warning lights • Fire extinguishing system warning Cockpit Control Panel (CCP) for FDS Data Transfer Device (DTD) Engine switch panel: • Digital engine control (FADEC) Radar altimeter

• • • • • •

Chip detectors with quick-disconnect plugs Twin-engine OEI-training mode Automatically controlled variable rotor speed system Cycle counter Drain system Fire walls

• • •

POWER PLANT • Two Safran Helicopter Engines ARRIEL 2E turbine engines with electronic engine control (double channel FADEC) • Crash resistant fuel system with a flexible bladder-type fuel main tank and supply tank (split into two sections) • Two independent oil cooling and lubrication systems of the engines • Fire detection and extinguishing system

145 D-2 18.100.01 E

19


Technical Data

TRANSMISSION SYSTEM • Main transmission including an independent redundant lubrication system and monitoring sensors • Chip detector system with quick-disconnect plug (main transmission) • Free wheel assemblies in the engine input drives

• Rotor brake system • Tail rotor transmission system with splash lubrication and oil level sight gauge • Chip detector system with quick-disconnect plug (tail rotor gearbox)

ROTOR AND FLIGHT CONTROLS • Hingeless main rotor (System Bölkow) with 4 glass and carbon fiber reinforced blades with erosion protection strip • Fenestron®-type tail rotor with ten composite blades (asymmetric blade spacing) and stator • Tail rotor gearbox cover • Basic provisions for an easy integration of a balancing system • Dual hydraulic boost system for cyclic and collective blade control of the main rotor

• Tail rotor control system with flexball cable and dual hydraulic booster • Main rotor blade tip painting (yellow) • Vector Mast Moment System (VMMS) • Dual Duplex 4-axis Digital Automatic Flight Control System including upper modes

ELECTRICAL INSTALLATION • Power generation system: • Two starter/generators (2 x 200 A, 28 VDC) • Nickel-Cadmium battery, (24 VDC, 40 Ah) • External power connector (STANAG 3302) • Power distribution system: • Two main busbars • Two essential busbars • Two shedding busbars • Two non-essential busbars (80 A) for optional equipment only • Battery bus • One utility receptacle in cargo compartment (28 VDC, 20 A)

• DC power control • Lighting: • Anti-collision warning light (red flashing), LED • Fixed landing light, LED • Three position lights (red, green, white), LED • Adjustable instrument lighting • One utility light in the cockpit, LED • Lights in the cabin and cargo compartment • Boarding illumination • Emergency lights • Radio: • Two radio master switches

GROUND HANDLING K ITa • Two ground-handling wheels • Basic aircraft covers (short term incl. Main Rotor Blade tie down) • Oil drain hoses • Keys for cockpit, cabin, clam-shell doors and tank flap (one-key system) • Battery key • Lifting points

• • • • • • •

Compass compensation key Fuel drain device Maintenance Ground Station (MGS) software Airbus Helicopters Data Loader (AHDL) Flight Data Continuous Recorder (FDCR) converter Fleet keeper ® applicationb Flight planner applicationc

a. Weight not included in the standard helicopter empty weight. b. License for one year and one helicopter included. c. Two licenses for one year and one helicopter included.

DOCUMENTATION (in English) • One Flight Manuala b (on paper) • One Pilots Checklistc (on paper) • One Master Minimum Equipment List (MMEL)a online via T.I.P.I. • One Logbook (on paper, CD-ROM on demand) • One Historical Record (on paper, CD-ROM on demand) • Technical Documentationad incl. AMM, SDS, WDM, IPC, MSM, CECG, SRM online via Keycopter ® portal • Service Bulletin Catalogue (SB) online via T.I.P.I. a. b. c. d. e. 20

• One List of Applicable Publications (LOAP)a online via Keycopter portal • One Avionics Manuale (for avionics installed by Airbus) (on CD-ROM) • One ECMMc (Electronic Component Maintenance Manuals) for vendor manuals • One Engine Documentationc (USB stick, paper on demand), furnished by supplier, including: • Maintenance Manual • Illustrated Parts Catalogue (IPC)

Revision service included as long as the aircraft is operational One Flight Manual included in the standard helicopter empty weight Revision service for 3 years Customized AMM, SDS, WDM and IPC versions available on request Customized documentation 145 D-2 18.100.01 E


Technical Data

4

Mission Configurations Airbus offers the following configurations for specific H145 missions. The created mission configurations should be regarded as a first proposal for customers to evaluate the suitability of the H145 for their operational fields. The shown mission configurations comprise the Baseline Aircraft and a list of Mission Equipment which can be complemented by additional equipment from their Further Available Equipment list. The following mission configurations are available: • Emergency Medical Services - EMS • Offshore Transportation • Law Enforcement • Aerial Work Please note that the EMS Mission configuration includes equipment requested by EASA OPS. They do not cover oxygen equipment and equipment required for extended over water operation. As the national operating rules may differ from EASA OPS, the operator has to contact his national authority to assure that the planned equipment configuration is acceptable for the intended kind of operation.

General rules for adding options to the mission c onfigur ation Some simple rules have to be considered when adding options from t he Further Available Equipment list to the mission configuration: • Only options from the respective Further Available Equipment list may be added to the mission configuration. • Mixing options of different Further Available Equipment lists could lead to product incompatibilities. • Detachable parts always require the relevant fixed provisions. Modified configuration to be confirmed by Airbus helicopter sales representative.

Performance calculation All data used for mission performance calculations in this document are for information purpose only and Airbus takes no responsibility for the correctness of this information as far as the applicability to the receiving party’s individual case is concerned. The present use of the named data shall not be construed as expressly or impliedly granting the receiving party any rights nor be deemed to constitute any kind of obligation or commitment of Airbus.

Further individual configurations In chapter 5 the reader will find a General Available Equipment list including additional available equipments suitable for the H145. She / he may choose further items and add them to the mission configuration. Please note that there are various items, which may be ordered for one helicopter, but their installation at the same time would not be possible completely or only partly. A detailed discussion is highly recommended in order to adapt the H145 to the customer's wishes and needs and to avoid misunderstandings which could lead to unsatisfactory configurations. Any modification and/or complement of the proposed mission configuration must be done with the assistance of an Airbus helicopter sales representative.

145 D-2 18.101.01 E

21


Technical Data

4.1

Emergency Medical Services - EMS Mission

Figure 4.1: Emergency Medical Services - EMS configuration - external view (example)

The H145 is particularly adapted to primary and secondary EMS missions. Due to its extremely low sound level, operation over cities and landing in the hospital area is supported. With its high set main rotor and Fenestron anti-torque-device easy loading and unloading of patients is provided even with rotors turning. The two large rear clam-shell doors enable quick, easy and safe patient loading. The spacious and unobstructed cabin allows all the necessary medical life-saving treatment to patients during flight. In this chapter you will find the basic configuration possibilities for the EMS helicopter and some interior layout examples of possible EMS configurations. A fixed provisions package has been created for the H145 to prepare the helicopter for the installation of various EMS packages. As the EMS interior itself is a complex part of the configuration a detailed EMS equipment catalogue has been established to show different variants of interior for different EMS missions from different suppliers. The customer shall discuss his needs with the Airbus helicopter sales representative so that the customer individual configuration can be prepared. In general the H145 is appropriate for following missions: • Helicopter Light Emergency Medical Service for rapid transport of the patient to the hospital. • Helicopter Emergency Medical Service (HEMS) for rapid transport of medical personnel and equipment to the scene and rapid transport of the patient to the hospital. • Helicopter Intensive Care Medical Service (HICAMS) for air ambulance transport of patients, medics as well as organs from a hospital or a prepared site to a hospital.

22

145 D-2 18.101.01 E


Technical Data

4.1.1 Mission Parameter • Flight Rules

Single / Dual Pilot IFR Night

• Cat. A

Yes

• Instrumentation

Glass Cockpit

• NVG friendly

Yes

• EASA OPS

Yesa

a. Please refer to chapter 5.5

Figure 4.2: EMS configuration - cabin layout

4.1.2 EMS Configuration Baseline Aircraft Qt y Do cu men t Reference

Commercial Reference

Product Title

kg

lb

Baseline Aircraft 1

00-10042-A

D0000-002-00

H145 Baseline Aircraft 145 D-2 18.100.01 E

1,919.0 4,231.4 Subtotal Weight:

1.5 % Weight margin: Subtotal Weight (incl. margin):

1,919.0 4,231.4 28.8

63.5

1,947.8 4,294.9

Mission Equipment Qt y Do cu men t Reference


Product Title

kg

lb

Mandatory Equip ment General Equi pment 1

05-03015-B

D2562-000-00

First aid kita

1.2

2.6

1

05-22028-B

D7935-000-00

Fuzz burner for engines, main transmission and Fenestron® gearbox

1.2

2.6

1

05-22029-A

D7114-001-00

Improved engine cowling heat protection, LH

0.4

0.9

1

05-22029-A

D7114-002-00

Improved engine cowling heat protection, RH

0.4

0.9

1

05-23008-B

D7165-000-00

Engine compressor wash kit

1.0

2.2

1

05-31121-A

D2514-200-00

Tinted sun shades for cockpit windshield roof section

2.1

4.6

1

05-37027-A

D6701-001-00

Copilot flight controls

5.6

12.3

1

05-38024-C

D3111-101-00

Instrument panel extension on copilot side

1.0

2.2

1

05-39017-A

D2513-001-00

Map case in copilot door

0.5

1.1

1

05-41012-A

D2143-000-00

Electrical Heating System

4.2

9.3

145 D-2 18.101.01 E

23


Technical Data

Q ty Do cu men t Reference


1

D3343-000-00

05-68012-A

Product Title

kg

lb

Additional electrical unit

0.9

2.0

6.5

14.3

0.0

0.0

2.6

5.7

Specific Mission Equipment 1

06-45068-A

D3343-600-00

Search & landing light

1

06-45086-A

D3343-800-00

Search & landing light, IR mode

1

06-65013-A

D2625-200-00

b

2nd portable fire extinguisher

c

1

06-67064-A

D2563-100-00

Emergency Locator Transmitter (ELT)

1.6

3.5

1

06-71001-B

D2517-000-10

Separation curtain for cockpit / cabin, fixed provisions

0.3

0.7

1

06-71001-B

D2517-100-20

Separation curtain for cockpit / cabin, washable, detachable parts

0.3

0.7

1

06-74029-B

D3312-020-00

Standard cockpit, cabin and cargo compartment - NVG

0.5

1.1

26.5

58.4

Digital Voice Control System (DVCS 6100), incl. ACU 6100 (Becker), pilot + copilot

7.2

15.9

Interior Layout 1

07-00029-A

D1830-000-00

Active vibration control system

Avionics Package DP IFR GTN 750 / GTX 335R

Av io ni cs 1

08-00449-A

D2300-000-08

1

08-16116-B

D2352-000-00

1

08-22077-A

D2325-700-00

Transponder GTX 335R (Garmin)d

2.9

6.4

1

08-25035-A

D3455-000-00

Distance Measuring Equipment (DME) DME-4000 (Rockwell Collins)

2.9

6.4

1

08-26058-A

D3431-000-00

Marker beacon receiver MKR3300-1 (Becker)

1.1

2.4

1

08-43063-C

D3463-311-00

GPS/NAV/COM GTN 750 (Garmin), copilot

5.8

12.8

1

08-43063-C

D3463-312-00

GPS/NAV/COM GTN 750 (Garmin), pilot

7.9

17.4

1

08-43079-A

D3464-000-00

Wireless connectivity Connext (Garmin)

0.1

0.2

1

08-65048-B

D3161-000-00

Flight Display Subsystem (FDS), copilot

5.1

11.2

1

08-99003-B

D0000-151-08

23.9

52.7

1

08-35055-C

D3446-000-00

0.1

0.2

0.0

0.0

1

08-35057-C

D3446-100-00

Avionics Package DP IFR GTN Series interconnection / wiring Helicopter Terrain Awareness and Warning System (H-TAWS) Helionixe e

Synthetic Vision System (SVS) - Helionix f

1

08-41031-A

D3160-000-00

SBAS RNP approach capability

0.0

0.0

1

08-65056-C

D3113-102-00

iPad Air holder, pilot

0.7

1.5

1

08-65056-C

D2491-002-00

Electrical fixed provisions, 5 VDC, pilot

0.7

1.5

g

1

08-81036-C

D3132-000-00

Cockpit Voice and Flight Data Recorder (CVFDR)

8.0

17.6

1

08-82000-B

D3139-000-00

Lightweight Aircraft Recording System (LARS) Alerts Vision 1000 (Appareo)

0.6

1.3

Reference Equi pment General Equipm ent 1

05-02063-B

D1113-200-00

Enhanced exterior painting instead of standard painting

2.2

4.9

1

05-02065-B

D6214-000-00

High visibility paint for main rotor blades

0.0

0.0

1

05-21021-A

D8541-000-10

Cable cutter system, fixed provisions

2.9

6.4

1

05-21021-A

D8541-000-20

Cable cutter system, detachable parts

7.7

17.0

1

05-31123-A

D5633-001-00

Window in clam-shell door, LH

0.3

0.7

1

05-31123-A

D5633-002-00

Window in clam-shell door, RH

0.3

0.7

1

05-85017-B

D2841-000-00

Fuel management system (Fuel flow meters)

0.2

0.4

Specific Mission Equipment

24

1

06-40002-A

D3347-100-00

Tail flood light for clam-shell doors

0.5

1.1

1

06-46010-B

D3347-000-00

White strobe lights

1.4

3.1

145 D-2 18.101.01 E


Technical Data

Qt y Do cu cu me men t Reference


Pr o d u c t Ti t l e

kg

lb

Interior Layout 1

07-15028-B

D2512-101-00

Height ad adjustable co copilot se seat in instead of of st standard co copilot se seat

1.8

4.0

1

07-15028-B

D2512-102-00

Height adjustable pilot seat instead of standard pilot seat

1.8

4.0

1

07-40033-A

D2525-000-00

Sealed cabin floor

0.4

0.9

h

1

07-70070-A

D8521-000-00

EMS Fixed Provisions Package

1

07-73077-A

D2512-201-10

Lengthened seat rails for copilot seat, fixed provisions

0.1

0.2

1

07-90030-B

D2508-401-00

Multi-purpose fittings in cabin, LH

3.1

6.8

1

07-90030-B

D2508-402-00

Multi-purpose fittings in cabin, RH

3.1

6.8

1

07-75110-B

D2524-400-00

4.7

10.4

1

07-50079-A

D5231-100-00

Clam-shell doors hinges, reinforced

0.1

0.2

1

05-34009-A

D2162-200-10

Ventilation of aft avionic bay, fixed provisions

0.5

1.1

1

05-34010-A

D5337-000-00

Multi-purpose attachment points at aft avionic bay

0.1

0.2

1

05-67033-A

D2465-300-00

Two power sockets (28 VDC, 40 A) at aft avionic bay

3.2

7.1

1

07-78010-A

D3314-000-00

Discrete signal interface for EMS illumination

0.3

0.7

D4321-100-00

Tactical radio, fixed provisions, power supply (28 VDC) & intercom interfacei

0.5

1.1

Attachment rails in cabin ceiling, reinforced

Av io ni cs 1

08-12090-A

i

1

08-12090-A

D4322-100-00

Tactical radio, fixed provisions, antenna for frequency band tbc

0.8

1.8

1

08-16116-B

D2343-400-00

Digital Voice Control System (DVCS 6100), ACU 6101 (Becker), pax j

1.1

2.4

Cabin panel, center

0.4

0.9

0.1

0.2

0.2

0.4

0.6

1.3

GSE

GSE

Su b t o t al We W ei g h t :

162.2

357.7

3.0 % Wei g h t m ar g i n :

4.9

10.7

Su bt bt ot ot al al We Wei gh gh t (i nc nc l. l. m ar ar gi gi n) n):

167.1

368.4

1

08-16161-B

D2343-000-00

k

1

08-16161-B

D2343-100-00

Cabin panel, center, cutout, FWD

2

08-18064-D

D2333-000-02

Headset adapter cable crew GLENAIR / U92

3

08-18064-D

D2333-100-02

Headset adapter cable pax GLENAIR / U92

1

08-80009-A

D3132-400-00

l

Professional Ground Station (PGS) Vision System

Tota To tall Wei Weight ght::

2,11 2, 114. 4.9 9 4,6 ,66 63. 3.2 2

a. Customization of first first aid kit content necessary to comply with EASA OPS OPS requirements. Medications Medications may have to be removed for export. b. Required for seating configuration configuration with 7 passengers or more. c. ELT code to be provided provided by the customer customer latest 4 months prior to helicopter delivery. d. Inc Incl. l. ADS-B ADS-B out e. The database update service is provided under a dedicated service contract. contract. Please contact your Airbus helicopter sales representative for further information. f. SBAS RNP approach local service service availability verification verification through your your Airbus helicopter helicopter sales representative representative on request. g. Grou Ground nd station station not include included. d. h. Requ Required ired for for any EMS soluti solution. on. i. Onboard HF/tactical HF/tactical radio transmission can influence radio navigation systems systems (MKR, VOR, ILS, ADF) ADF) and communication communication systems (VHF radio, other tactical radio). Depending on National Aviation Authorities certification requirements, tactical radio systems must either be turned off during IFR approaches/departures or deactivated. j. Requires cabin panel and cabin panel cutout. k. Requi Requires res cabin cabin panel, panel, center. center. l. Recom Recommend mended ed 1 per customer customer base base if CVFDR CVFDR is selecte selected d

145 D-2 18.101.01 E

25


Technical Te chnical Data

4.1. 4. 1.3 3 Furthe Furtherr Available Available Equipme Equipment nt Q ty ty Do cu cu me men t Reference


Pr o d u c t Ti t l e

kg

lb

23.9

52.7

0.2

0.4

-3.5

-7.7

8.7

19.2

63.0

138.9

Generall Equipm ent Genera 1

05-21034-A

D7162-000-00

Inlet Barrier Filter (IBF) system

1

05-31120-B

D5204-301-00

Sliding door fastener, max. position, LH

1

05-37028-A

D6721-001-00

a

Pedal cover for copilot flight controls

Specific Spe cific Mission Equipment 1

06-21037-B

D8512-001-10

External hoist, LH, fixed provisionsb c d

1

06-21037-B

D8512-000-20

External hoist (without hook), detachable parts

1

06-21037-B

D8512-100-00

External hoist hook and standard damper

3.6

7.9

1

06-26025-C

D3181-000-00

External multi-purpose camera on tail boom

1.4

3.1

1

06-26025-C

D3181-100-00

External rear-view camera

1.6

3.5

1

06-27044-C

D8511-400-10

Dual cargo hook system, fixed provisions

5.9

13.0

1

06-27044-C

D8511-400-20

Dual cargo hook system, detachable parts

29.6

65.3

1

06-31025-C

D8531-000-00

External loudspeaker system with siren

10.9

24.0

15.2 15 .2

33.5 33 .5

0.2

0.4

0.2

0.4

2.2

4.9

0.4

0.9

1.0

2.2

2.2

4.9

0.6

1.3

0.4

0.9

0.2

0.4

Interior Layout 1

07-40031-A

D2515-000-00

Wash Wa shab able le fl floo oorr co cove veri ring ng fo forr co cock ckpi pit, t, ca cabi bin n & ca carg rgo o co comp mpar artm tmen entt

1

07-50074-A

D8512-401-00

External protection for cabin frame, LH

1

07-50074-A

D8512-402-00

External protection for cabin frame, RH

1

07-50081-A

D5231-200-00

1

07-75128-B

D8512-800-00

1

07-90030-B

e

One-hand latching system for clam-shell doors (ADAC - STC) Attachment ring in cabin ceiling LH

D2508-101-00

Multi-purpose fittings in cabin, FWD LH

f

Av io ni cs 1

08-16172-B

D4361-950-00

Wireless intercom system PNG (Axnes), basic systemg

1

08-16172-B

D4361-960-00

Wireless intercom system PNG (Axnes), cockpit control panel CP50

1

08-16172-B

D4361-970-00

Wireless intercom system PNG (Axnes), mobile transceiver MP50

1

08-18064-D

D2333-100-02

Headset adapter cable pax GLENAIR / U92 i

1

08-46063-D

D3168-400-00

Moving map EuroNav 7 – RN7 (EuroAvionics), basic version

7.2

15.9

1

08-46063-D

D3168-500-00

Moving map EuroNav 7 – RN7 (EuroAvionics), Iridium satcom module j

0.7

1.5

Moving map EuroNav 7 – RN7 (EuroAvionics), GSM / UMTS module j

0.5

1.1

1

08-46063-D

D3168-600-00

1

08-83042-B

D3171-200-10

Health Monitoring System (HMS), fixed provisions

4.0

8.8

1

08-83042-B

D3171-200-20

Health Monitoring System (HMS), detachable parts

3.6

7.9

a. b. c. d. e. f. g. h. i. j.

26

h

Requires copilot Requires copilot flight flight controls. controls. Requires Requi res sliding sliding door fastene fastener. r. Weight, in combination combination with Emergency floats, floats, detachable parts: 11.5 kg. Requires external hoist damper & hook. Hoist operation and maintenance training included. This STC is EASA certified. certified. Prices and lead times times for national certifications certifications are available on request. request. Required for external hoist installation if multi-purpose fittings fittings LH are not installed. Requires wireless intercom intercom system PNG PNG (Axnes), cockpit cockpit control panel. Mobile Mobile transceiver not included. included. Mobile transceiver with with defined frequency range between 440 – 450 MHz in yellow yellow color. Incl. 512 GB flash flashdisk disk and and Global Global Map Packag Package. e. Requires EuroNav 7 - RN7 (EuroAvionics) (EuroAvionics) basic version.

145 D-2 18.101.01 E


Technical Data

4.1. 4. 1.4 4 EM EMS S Mission Pe Performance rformance Weight We ight brea breakdown kdown (with payload and fuel) Weight basis for Payload range diagram

Payload

Fuel

Equipped empty weight EMS configuration (incl. en engine oil, unusable fuel and weight ma margin) 2 Pilots (2 x 85 kg) Medical Equipment (incl. stretcher; cabinet; 2 seats; oxygen; medical devices) 2 Medical crew (2 x 85 kg) 1 Stretcher patient (1 x 85 kg) Reserve fuel: 30 min in 1,500 ft with VBR, mean 131 KTAS Trip fuel Miss Mi ssio ion n Ta Take keof offf we weig ight ht

kg

lb

2,114 170

4,663 375

180 170 85

397 375 187

123 600 3,44 3, 442 2

271 1 ,323 1, 7,59 7, 590 0

Mission profile • • • • •

Takeoff Cat. A VTOL Takeoff VTOL at SL (maximum (maximum 3,700 3,700 kg) kg) Climb Clim b flight flight AEO-MCP AEO-MCP from SL to 5,000 5,000 ft with VY, mean 70 KIAS Levell flight Leve flight in 5,000 5,000 ft ft with VBR, mean 134 KTAS Descent from 5,000 5,000 ft to SL with R/D of 1,000 fpm, fpm, mean 80 KIAS KIAS Landing Land ing Cat. A VTOL VTOL at SL

Payload range diagram

Figure 4.3: EMS configuration - Payload range diagram

Relevant Re levant flight data

• Calculated max. range (without payload, with trip fuel): • Corresponding flight time (incl. climb / descent phases): 145 D-2 18.101.01 E

Ar ri el 2E 2E 340 NM (629 km) 2 h 35 min 27


Technical Data

4.1.5 Typical Cabin Layouts (for more details see EMS Equipment Catalogue)

Figure 4.4: Helicopter Light Emergency Medical Services (Light EMS) - cabin layout

Figure 4.5: Helicopter Emergency Medical Services (HEMS) - cabin layout

Figure 4.6: Helicopter Intensive Care Medical Services (HICAMS) - cabin layout

28

145 D-2 18.101.01 E


Technical Data

4.2

Offshore Transportation Mission

Figure 4.7: Offshore Transportation configuration (with external hoist selected) - external view (example)

The H145 offers exceptional reliability and performance parameters in extreme weather conditions. An optimal level of safety in One Engine Inoperative (OEI) scenarios is provided by the powerful Safran Helicopter Engines Arriel 2E engines. Furthermore the high-set main rotor and the Fenestron improve safety for the personnel on the platform. The compact size allows to land on very small platforms, while still carrying a large number of passengers. The fixed landing gear facilitates landings on unprepared terrain. The presented Offshore Transportation configuration features a seating layout for eight passengers. To enhance the safety for over water flights a color weather radar, an emergency floatation system, an helicopter emergency egress lighting system as well as an automatic deployable ELT is proposed. Additionally an emergency floats system with integrated life rafts (DART - STC) can be proposed on request. Alternative seating arrangements can be selected for up to 10 passengers in the cabin.

145 D-2 18.101.01 E

29


Technical Data



• Cat. A

Yes

• Instrumentation

Glass Cockpit

• NVG friendly

No

• EASA OPS

No

Figure 4.8: Offshore Transportation configuration - cabin layout

4.2.2 Mission Configuration Baseline Aircraft Q ty Do cu men t Reference


Product Title

kg

lb

Baseline Aircraft 1

00-10042-A

D0000-002-00



1.5 % Weight margin:

1,919.0 4,231.4 28.8

63.5

Subtotal Weight (incl. margin): 1,947.8 4,294.9

Mission Equipment Q ty Do cu men t Reference


Product Title

kg

lb

Mandatory Equipment General Equipm ent

30

1

05-03015-B

D2562-000-00

First aid kita

1.2

2.6

1

05-22028-B

D7935-000-00


1.2

2.6

1

05-22029-A

D7114-001-00


0.4

0.9

1

05-22029-A

D7114-002-00


0.4

0.9

1

05-23008-B

D7165-000-00


1.0

2.2

1

05-31121-A

D2514-200-00


2.1

4.6

1

05-37027-A

D6701-001-00


5.6

12.3

1

05-38024-C

D3111-101-00


1.0

2.2

1

05-39017-A

D2513-001-00


0.5

1.1

1

05-41012-A

D2143-000-00

Electrical heating system

4.2

9.3

1

05-68012-A

D3343-000-00

0.9

2.0


145 D-2 18.101.01 E


Technical Data

Qt y Do cu men t Reference


Product Title

kg

lb

6.5

14.3

8.0

17.6

26.5

58.4

7.2

15.9

2.9

6.4

Specific Mission Equipment 1 1

06-45086-A 06-67065-A

D3343-600-00

Search & landing light b

D2563-200-00

Automatic Deployable Emergency Locator Transmitter (ADELT)

D1830-000-00



Interior Layout 1

07-00029-A

Av io ni cs 1

08-00449-A

D2300-000-08

1

08-16116-B

D2352-000-00

Digital Voice Control System (DVCS 6100), incl. ACU 6100 (Becker), pilot + copilot c

1

08-22077-A

D2325-700-00

Transponder GTX 335R (Garmin)

1

08-25035-A

D3455-000-00


2.9

6.4

1

08-26058-A

D3431-000-00


1.1

2.4

1

08-43063-C

D3463-311-00


5.8

12.8

1

08-43063-B

D3463-312-00


7.9

17.4

1

08-43079-A

D3464-000-00


0.1

0.2

1

08-65048-B

D3161-000-00


5.1

11.2

1

08-99003-B

D0000-151-08

23.9

52.7

1

08-35055-C

D3446-000-00

0.1

0.2

0.0

0.0

1

08-35057-B

D3446-100-00

Avionics Package DP IFR GTN Series interconnection / wiring Helicopter Terrain Awareness and Warning System (H-TAWS) Helionixd d

Synthetic Vision System (SVS) - Helionix e

1

08-41031-A

D3160-000-00


0.0

0.0

1

08-65056-C

D3113-102-00


0.7

1.5

1

08-65056-C

D2491-002-00


0.7

1.5

1

08-82000-B

D3139-000-00


0.6

1.3

Reference Equi pment General Equi pment 1

05-02063-B

D1113-200-00


2.2

4.9

1

05-02065-B

D6214-000-00

High visibility paint for main rotor blades

0.0

0.0

1

05-31124-A

D5621-000-00

Push-out cabin windows

3.3

7.3

1

05-62026-A

D2420-000-00

1.6

3.5

1

05-85017-B

D2841-000-00


0.2

0.4

1

05-93014-C

D1021-100-00

Lashing points

1.1

2.4

2.3

5.1

67.3

148.4

2.9

6.4

Alternating Current (AC) systemf


06-61032-B

D3214-000-10

Emergency floats, fixed provisions

1

06-61032-B

D3214-000-20

Emergency floats, detachable parts

1 1

06-65013-A 06-66022-A

D2625-300-00

nd

2 portable fire extinguisher, high-density seating, 10 seats BAE g

D3353-000-00

Helicopter Emergency Egress Lighting System (HEELS)

6.3

13.9

Interior Layout 1

07-15028-B

D2512-101-00

Height adjustable copilot seat instead of standard copilot seat

1.8

4.0

1

07-15028-B

D2512-102-00


1.8

4.0

1

07-27021-C

D2522-000-00

Passenger seating, 8 club seats (standard arrangement)

94.7

208.8

1

07-27039-A

D2521-100-00

Offshore Seating Arrangement, basic kit

2.3

5.1

1

07-50071-A

D5221-000-00

Jettisonable cockpit doors

0.6

1.3

1

07-50074-A

D8512-401-00


0.2

0.4

145 D-2 18.101.01 E

31


Technical Data



Product Title

kg

lb

1

D8512-402-00


0.2

0.4

D4321-320-00

Tactical radio VHF-FM NPX138N - NVG (Cobham)h

2.6

5.7

07-50074-A

Av io ni cs 1

08-12093-C

i

1

08-17091-A

D2334-000-00

Passenger address interface

0.9

2.0

2

08-18064-D

D2333-000-02


0.2

0.4

8

08-18064-D

D2333-100-02


1.6

3.5

8

08-18065-B

D2315-300-00

Headset H10-76 (David Clark), low impedance

4.8

10.6

1

08-31065-A

D3443-200-00

Search and rescue weather radar RDR-1600 (Telephonics)

16.0

35.3

1

08-31065-A

D3443-300-00

Search and rescue weather radar RDR-1600 (Telephonics), radar radome

6.3

13.9

0.0

0.0

0.7

1.5

1 1

08-46058-B 08-65056-C

D3168-100-00 D2491-100-00

d

Moving map - Helionix

j

Electrical fixed provisions, 5 VDC, center console

k

1

08-81036-C

D3132-000-00

Cockpit Voice and Flight Data Recorder (CVFDR)

8.0

17.6

1

08-83042-B

D3171-200-10


4.0

8.8

1

08-83042-B

D3171-200-20


3.6

7.9

GSE

GSE

Subt otal Weight:

356.0

785.0


10.7

23.5

Su bt ot al Wei gh t (i nc l. m ar gi n):

366.7

808.5

1

08-83046-A

D3171-100-00

l

Helicopter Flight Data Monitoring (HFDM)

Total Weight: 2,314.5 5,103.4

a. Customization of first aid kit content necessary to comply with EASA OPS requirements. Medications may have to be removed for export. b. ELT code to be provided by the customer latest 4 months prior to helicopter delivery. c. Incl. ADS-B out. d. The database update service is provided under a dedicated service contract. Please contact your Airbus helicopter sales representative for further information. e. SBAS RNP approach local service availability verification through your Airbus helicopter sales representative on request. f. Required for RDR-1600 installation. g. Weight, in combination without push-out cabin windows: 5.7 kg. h. Onboard HF/tactical radio transmission can influence radio navigation systems (MKR, VOR, ILS, ADF) and communication systems (VHF radio, other tactical radio). Depending on National Aviation Authorities certification requirements, tactical radio systems must either be turned off during IFR approaches/departures or deactivated. i. Requires electrical fixed provisions 5 VDC at center console. j. Required for passenger address interface. k. Ground station not included. l. Instead of PGS Vision System.

32

145 D-2 18.101.01 E


Technical Data

4.2.3 Further Available Equipment Qt y Do cu men t Reference


Product Title

kg

lb

General Equi pment 1

05-31120-B

D5204-301-00


0.2

0.4

1

05-31120-B

D5204-302-00

Sliding door fastener, max. position, RH

0.2

0.4

9.8

21.6

63.0

138.9


06-21037-B

D8512-002-10

External hoist, RH, fixed provisions a b c

1

06-21037-B

D8512-000-20


1

06-21037-B

D8512-100-00


3.6

7.9

1

06-21037-B

D8512-200-00

External hoist hook damper floating device

0.4

0.9

3.0

6.6

0.7

1.5

0.8

1.8

0.5

1.1

d

1

06-21037-B

D8512-900-00

External hoist hook damper weight kit

1

06-21038-A

D8512-302-10

External hoist observation light, RH, fixed provisions

1

06-21038-A

D8512-300-20

External hoist observation light, detachable parts

e f

1

06-21039-A

D8510-020-00

Teflon coating for cable deflector on floats landing gear, RH

1

06-26025-C

D3181-000-00


1.4

3.1

1

06-27042-D

D8511-200-10

Single cargo hook system (Onboard), fixed provisions

8.9

19.6

1

06-27042-D

D8511-200-20

Single cargo hook system (Onboard), detachable parts

7.7

17.0

2.6

5.7

123.5

272.3

67.5

148.8

75.4

166.3

1

06-65013-A

nd

g

D2625-200-00

2 portable fire extinguisher

D2520-000-01

High-density seating, 10 seats (BAE Systems - STC), 3 FWD / 2 LH / 2 RH / 3 AFT hi

Interior Layout 1 1

07-27022-B 07-27022-B

D2520-600-04

High-density seating, 6 seats (BAE Systems - STC), 3 FWD / 3 AFTh hi

1

07-27022-B

D2520-600-05

High-density seating, 6 seats (BAE Systems - STC), 3 LH / 3 RH

1

07-27022-B

D2520-800-03

High-density seating, 8 seats (BAE Systems - STC), 3 FWD / 3 LH / 2 RH hi

99.3

219.0

High-density seating, 9 seats (BAE Systems - STC), 3 FWD / 3 LH / 3 RH hi

109.0

240.3

5.9

13.0

2.2

4.9

1.0

2.2

1 1 1

07-27022-B 07-30067-B 07-50081-A

D2520-900-01 D2581-000-00 D5231-200-00

Sound proofing kit j

One-hand latching system for clam-shell doors (ADAC - STC) k

1

07-90030-B

D2508-102-00

Multi-purpose fittings in cabin, FWD RH

1

07-90030-B

D2508-401-00


3.1

6.8

1

07-90030-B

D2508-402-00


3.1

6.8

D4321-000-00

Tactical radio, fixed provisions, power supply (12 VDC) & intercom interfacel

1.4

3.1

Tactical radio, fixed provisions, power supply (28 VDC) & intercom interfacel

0.5

1.1

0.8

1.8

2.2

4.9

0.6

1.3

0.4

0.9

3.0

6.6

08 Avionics 1 1 1

08-12090-A 08-12090-A 08-12090-A

D4321-100-00 D4322-100-00

l

Tactical radio, fixed provisions, antenna for frequency band tbc m

1

08-16172-B

D4361-950-00

Wireless intercom system PNG (Axnes), basic system

1

08-16172-B

D4361-960-00


1

08-16172-B

D4361-970-00


1

08-15564-A

D2316-000-00

Iridium satellite transceiver GSR 56 (Garmin) o

n

1

08-17090-B

D2331-010-00

Cabin loudspeaker

2.1

4.6

1

08-18064-D

D2333-100-02


0.2

0.4

1

08-65056-C

D2491-001-00

Electrical fixed provisions, 5 VDC, copilot

0.7

1.5

145 D-2 18.101.01 E

33


Technical Data



Product Title

kg

lb

1

D3113-101-00

iPad Air holder, copilot

0.7

1.5

08-65056-C

a. b. c. d. e. f. g. h. i. j. k. l.

Requires sliding door fastener. Weight, in combination with Emergency floats, detachable parts: 12.6 kg. Requires external hoist damper & hook. Hoist operation and maintenance training included. The hoist hook damper can be equipped with 1, 2 or 3 kg additional weight. Requires external hoist, detachable parts. Required if external hoist and emergency floats are selected. Required for seating configuration with 7 passengers or more. This STC is EASA and FAA certified. Prices and lead times for national certifications are available on request. Installation requires multi-purpose fittings in cabin LH and RH. This STC is EASA certified. Prices and lead times for national certifications are available on request. Required for RH hoist installation if multi-purpose fittings RH are not installed. Onboard HF/tactical radio transmission can influence radio navigation systems (MKR, VOR, ILS, ADF) and communication systems (VHF radio, other tactical radio). Depending on National Aviation Authorities certification requirements, tactical radio systems must either be turned off during IFR approaches/departures or deactivated. m. Requires wireless intercom system PNG (Axnes), cockpit control panel. Mobile transceiver not included. n. Mobile transceiver with defined frequency range between 440 – 450 MHz and in yellow color. o. Requires sound proofing kit.

34

145 D-2 18.101.01 E


Technical Data

4.2.4 Offshore Mission Performance Weight breakdown (with payload and fuel) Weight basis for Radius of action diagram

Equipped empty weight Offshore Transportation configuration (incl. engine oil, unusable fuel and weight margin) 2 Pilots (2 x 85 kg) 8 Passengers (8 x 95 kg) Reserve fuel: 30 min in 1,500 ft with VY, mean 72 KIAS Contingency fuel: 10 % Trip fuel Mission Takeoff weight

Payload Fuel

kg

lb

2,314

5,103

170 760 98 33 325 3,700

375 1,676 216 72 716 8,157


Takeoff Cat. A VTOL at SL (maximum 3,700 kg (2x)) Climb flight AEO-MCP from SL to 5,000 ft with VY, mean 70 KIAS Level flight in 5,000 ft with VBR, mean 131 KTAS Descent from 5,000 ft to SL with R/D of 1,000 fpm, mean 80 KIAS Landing Cat. A VTOL at SL (2x)

Radius o f action d iagram

Figure 4.9: Offshore Transportation configuration - Radius of action diagram

Relevant flight data Ar ri el 2E

• Calculated max. radius of action (without payload, with trip fuel): • Corresponding flight time (incl. 2x climb / descent phases):

145 D-2 18.101.01 E

153 NM (283 km) 2 h 29 min

35


Technical Data

4.2.5 Typical Cabin Layouts

Figure 4.10: Offshore seating configuration - 8 Passengers transportation - cabin layout

Figure 4.11: Offshore seating configuration - 6 Passengers transportation - cabin layout

Figure 4.12: Offshore seating configuration - 4 Passengers hoisting - cabin layout

36

145 D-2 18.101.01 E


Technical Data

4.3

Law Enforcement Mission

Figure 4.13: Law Enforcement configuration (with EOS Star Safire 380HDc package selected) external view (example)

Due to its multi-mission flexibility the H145 can be configured to cover the wide range of law enforcement missions ranging from observation and airborne surveillance, Search and Rescue (SAR) to passenger transport and deployment of specialized personnel to inaccessible places. The Law Enforcement configuration in NVG layout is equipped with a powerful Trakka A800 searchlight, an external loudspeaker as well as a moving map system. The provisions for cargo hook, external hoist, external rope down operations and tactical radio are provided. Depending on the required mission, additional mission packages and equipment can be selected such as the Star Safire 380HDc camera package (video recorder, downlink, operator workstation), a variety of seating arrangements, cargo hook, external hoist and external rope down system detachable parts. Additional workstation options (e.g. second monitor) and other camera packages like Star Safire 380HD, MX-10 and MX-15 are available on request.

145 D-2 18.101.01 E

37


Technical Data



• Cat. A

Yes

• Instrumentation

Glass Cockpit

• NVG friendly

Yes

• EASA OPS

No

Figure 4.14: Law Enforcement configuration (with EOS Star Safire 380HDc package selected and installed in rear position) - cabin layout



Product Title

kg

lb

Baseline Aircraft 1

00-10042-A

D0000-002-00




1,919.0 4,231.4 28.8

63.5




Product Title

kg

lb


38

1

05-03015-B

D2562-000-00

First aid kita

1.2

2.6

1

05-22028-B

D7935-000-00


1.2

2.6

1

05-22029-A

D7114-001-00


0.4

0.9

1

05-22029-A

D7114-002-00


0.4

0.9

1

05-23008-B

D7165-000-00


1.0

2.2

1

05-31121-A

D2514-200-00


2.1

4.6

1

05-37027-A

D6701-001-00


5.6

12.3

1

05-38024-C

D3111-101-00


1.0

2.2

1

05-39017-A

D2513-001-00


0.5

1.1

1

05-41012-A

D2143-000-00


4.2

9.3

145 D-2 18.101.01 E


Technical Data



1

D3343-000-00

05-68012-A

Product Title

kg

lb


0.9

2.0

6.5

14.3

0.0

0.0


06-45068-A

D3343-600-00

Search & landing light

1

06-45068-A

D3343-800-00

Search & landing light, IR mode b

1

06-67064-A

D2563-100-00

Emergency Locator Transmitter (ELT)

1.6

3.5

1

06-71001-B

D2517-000-10


0.3

0.7

1

06-71001-B

D2517-100-20


0.3

0.7

1

06-74029-B

D3312-020-00

Standard cockpit, cabin and cargo compartment - NVG

0.5

1.1

26.5

58.4


7.2

15.9

Interior Layout 1

07-00029-A

D1830-000-00



Av io ni cs 1

08-00449-A

D2300-000-08

1

08-16116-B

D2352-000-00

1

08-22077-A

D2325-700-00

Transponder GTX 335R (Garmin)c

2.9

6.4

1

08-25035-A

D3455-000-00


2.9

6.4

1

08-26058-A

D3431-000-00


1.1

2.4

1

08-43063-C

D3463-311-00


5.8

12.8

1

08-43063-C

D3463-312-00


7.9

17.4

1

08-43079-A

D3464-000-00


0.1

0.2

1

08-65048-B

D3161-000-00


5.1

11.2

1

08-99003-B

D0000-151-08

23.9

52.7

1

08-35055-C

D3446-000-00

0.1

0.2

0.0

0.0

1

08-35057-C

D3446-100-00


Synthetic Vision System (SVS) - Helionix e

1

08-41031-A

D3160-000-00


0.0

0.0

1

08-82000-B

D3139-000-00


0.6

1.3


05-02063-B

D1113-200-00


2.2

4.9

1

05-21021-A

D8541-000-10


2.9

6.4

1

05-21021-A

D8541-000-20


7.7

17.0

0.2

0.4

1 1 1

05-31120-B 05-31120-B 05-36032-B

D5204-301-00 D5204-302-00 D3230-301-00

1

05-36032-B

D3230-302-00

1

05-85017-B

D2841-000-00

f



g

0.2

0.4

h

5.3

11.7

i

6.7

14.8

0.2

0.4

8.7

19.2

2.3

5.1

3.5

7.7

Aluminum multifunction step LH instead of standard boarding step

Aluminum multifunction step RH instead of standard boarding step Fuel management system (Fuel flow meters)


08-46063-B

D8512-001-10

External hoist, LH, fixed provisions j k

1

06-24020-B

D8534-002-10

External rope down device, RH, fixed provisions

1

06-24020-B

D8534-200-10

Enhanced external rope down device (ECMS - STC), LH & RH, electrical fixed provisionsl l

1

06-24020-B

D8534-300-00

Enhanced external rope down device (ECMS - STC), control panel

0.5

1.1

1

06-26025-C

D3181-000-00


1.4

3.1

145 D-2 18.101.01 E

39


Technical Data



Product Title

kg

lb

1

06-27044-C

D8511-400-10


5.9

13.0

1

06-45074-D

D3346-000-10

Searchlight A800 (Trakka) basic LH, fixed provisions

5.5

12.1

1

06-45074-D

D3346-000-20

Searchlight A800 (Trakka) basic LH, detachable parts

18.9

41.7

1

06-45074-D

D3346-000-30

Searchlight A800 (Trakka), vendor parts

18.2

40.1

1

06-45074-D

D3346-100-00

Searchlight A800 (Trakka), IR filters

0.0

0.0

1

06-45074-D

D3346-300-00

Searchlight A800 (Trakka), IR laser pointer m

0.0

0.0

1

06-45074-D

D3346-600-10

Searchlight A800 (Trakka), hand controller, fixed provisions

0.6

1.3

1

06-45074-D

D3346-600-20

Searchlight A800 (Trakka), hand controller, detachable parts

0.9

2.0

1

06-45074-D

D3346-700-00

Searchlight A800 (Trakka), covers

GSE

GSE

Interior Layout 1

07-15028-B

D2512-101-00


1.8

4.0

1

07-15028-B

D2512-102-00


1.8

4.0

1

07-50072-D

D5204-100-00

Spoiler position for cockpit doors, intermediate position

1.1

2.4

1

07-50074-A

D8512-401-00


0.2

0.4

1

07-50074-A

D8512-402-00


0.2

0.4

1

07-90030-B

D2508-401-00


3.1

6.8

1

07-90030-B

D2508-402-00


3.1

6.8

D4321-100-00

Tactical radio, fixed provisions, power supply (28 VDC) & intercom interfacen

0.5

1.1

Av io ni cs 1

08-12090-A

n

1

08-12090-A

D4322-100-00


0.8

1.8

1

08-16116-B

D2343-400-00

Digital Voice Control System (DVCS 6100), ACU 6101 (Becker), paxo

1.1

2.4

Cabin panel, center

0.4

0.9

0.1

0.2

2.2

4.9

1 1

08-16161-B 08-16161-B

D2343-000-00 D2343-200-00

Cabin panel, center, cutout, AFT

p q

1

08-16172-B

D4361-950-00

Wireless intercom system PNG (Axnes), basic system

1

08-16172-B

D4361-960-00


0.6

1.3

1

08-16172-B

D4361-970-00

Wireless intercom system PNG (Axnes), mobile transceiver MP50r

0.4

0.9

2

08-18064-D

D2333-000-02


0.2

0.4

s

1

08-46063-D

D3168-400-00

Moving map EuroNav 7 – RN7 (EuroAvionics), basic version

7.2

15.9

1

08-46063-D

D3168-500-00

Moving map EuroNav 7 – RN7 (EuroAvionics), Iridium satcom modulet

0.7

1.5

Moving map EuroNav 7 – RN7 (EuroAvionics), GSM / UMTS modulet

0.5

1.1

Cockpit Voice and Flight Data Recorder (CVFDR), fixed provisions

3.0

6.6

1 1

08-46063-D 08-81036-C

D3168-600-00 D3132-000-10

Subt otal Weight:

232.6

512.9


7.0

15.4


239.6

528.3

Total Weight: 2,187.4 4,823.1

a. Customization of first aid kit content necessary to comply with EASA OPS requirements. Medications may have to be removed for export. b. ELT code to be provided by the customer last 4 month prior to helicopter delivery. c. Incl. ADS-B out d. The database update service is provided under a dedicated service contract. Please contact your Airbus helicopter sales representative for further information. e. SBAS RNP approach local service availability verification through your Airbus helicopter sales representative on request. f. Required for hoist operations. g. Required for rope down operations. h. Required for A800 (Trakka) installation. 40

145 D-2 18.101.01 E


Technical Data

i. Required for electro optical system installation. j. Weight, in combination with Emergency floats, detachable parts: 11.5 kg. k. Weight, in combination with Emergency floats, detachable parts: 5.0 kg. l. This STC is EASA certified. Prices and leadtimes for national certifications are available on request. m. The laser pointer function is delivered inoperative. The responsibility for the laser activation and usage remains with the operator and user. n. Onboard HF/tactical radio transmission can influence radio navigation systems (MKR, VOR, ILS, ADF) and communication systems (VHF radio, other tactical radio). Depending on National Aviation Authorities certification requirements, tactical radio systems must either be turned off during IFR approaches/departures or deactivated. o. Requires cabin panel and cabin panel cutout. p. Requires cabin panel, center. q. Requires wireless intercom system PNG (Axnes), cockpit control panel. Mobile transceiver not included. r. Mobile transceiver with defined frequency range between 440 – 450 MHz in yellow color. s. Incl. 512 GB flashdisk and Global Map Package. t. Requires EuroNav 7 - RN7 (EuroAvionics), basic version.

4.3.3 Further Available Equipment Qt y Do cu men t Reference


Product Title

kg

lb

23.9

52.7

General Equi pment 1

05-21034-A

D7162-000-00

Inlet Barrier Filter (IBF) system

1

05-36029-C

D3211-001-00

Flat step patches on multifunction step, LH

1.9

4.2

1

05-36029-C

D3211-002-00

Flat step patches on multifunction step, RH

1.9

4.2

1

05-67030-B

D2465-200-00

Power sockets (14 VDC & 28 VDC) at center console and LH rear cabin walla

2.6

5.7

63.0

138.9


06-21037-B

D8512-000-20

External hoist (without hook), detachable partsb

1

06-21037-B

D8512-100-00


3.6

7.9

1

06-21037-B

D8512-200-00


0.4

0.9

c

1

06-21037-B

D8512-900-00


3.0

6.6

1

06-21038-A

D8512-301-10

External hoist observation light, LH, fixed provisions

0.7

1.5

1

06-21038-A

D8512-300-20

External hoist observation light, detachable partsd

0.8

1.8

1

06-24020-B

D8534-201-20

Enhanced external rope-down device for 2/1 persons (ECMS - STC), LH, retractable, detachable parts ef

20.3

44.8

Enhanced external rope-down device for 2/1 persons (ECMS - STC), RH, retractable, detachable parts e

20.3

44.8

1

06-24020-B

D8534-202-20

1

06-27044-C

D8511-400-20


29.6

65.3

1

06-31025-C

D8531-000-00


10.9

24.0

nd

g

1

06-65013-A

D2625-200-00

2 portable fire extinguisher

2.6

5.7

1

06-81031-A

D8511-600-10

Electrical release for fire extinguishing bucket (Bambi Bucket), fixed provisionsh

0.6

1.3

0.0

0.0

1

06-90013-A

145 D-2 18.101.01 E

D0000-600-00

Alternate gross weight 3,800 kg

41


Technical Data



Product Title

kg

lb

22.5

49.6

0.2

0.4

Mission Equipment - EOS Star Safire 380HDc Soluti oni 1

07-27034-A

D2526-000-00

Operator seat

1

08-18064-C

D2333-100-05

Headset adapter cable pax GLENAIR / U92 without IC/TX-Box j

1

06-50023-A

D8532-272-00

EOS Star Safire 380HDc Package

1

06-51199-C

D8532-200-11

EOS, RH step, fixed provisions

9.0

19.8

1

06-51199-C

D8532-200-21

EOS, RH step, detachable parts

8.5

18.7

1

06-51199-C

D8532-200-90

EOS, safety circuit for laser

0.7

1.5

1

06-50018-B

D8532-272-32

EOS, Star Safire 380HDc, basic system (MWIR, 1280)

28.0

61.7

1

06-50018-B

D8532-271-41

EOS, Star Safire 380HD series, continuous zoom TV camera (HDLL)

0.0

0.0

EOS, Star Safire 380HD series, short wave infrared camera (SWIR, 640)

0.0

0.0

1

06-50018-B

D8532-271-42

1

06-50018-B

D8532-271-52

EOS, Star Safire series, compact laser range finder

0.0

0.0

1

06-50018-B

D8532-271-53

EOS, Star Safire series, laser illuminator

0.0

0.0

1

06-50018-B

D8532-271-54

EOS, Star Safire series, laser pointer

0.0

0.0

1

06-50018-B

D8532-271-61

EOS, Star Safire series, video autotracker

0.0

0.0

1

06-50018-B

D8532-271-63

EOS, Star Safire series, digital image blending

0.0

0.0

1

06-50018-B

D8532-270-82

EOS, Star Safire Series, geo reference system with integrated IMU/GPS

0.0

0.0

1.1

2.4

GSE

GSE

9.8

21.6

1

06-50018-B

D8532-271-71

EOS, Star Safire series, universal hand controller

1

06-50018-B

D8532-271-91

EOS, Star Safire series, purge kit

1

06-52002-C

D8532-261-21

Operator workstation PD DZUS, basic

1

06-52002-C

D8532-261-26

Operator workstation PD DZUS, EOS control, holder

0.4

0.9

1

06-52002-C

D8532-261-28

Operator workstation PD DZUS, monitor, provisions

2.9

6.4

1

06-52002-C

D8532-261-30

Operator workstation PD DZUS, table for monitor installation

9.3

20.5

1

06-52002-C

D8532-261-33

Operator workstation PD DZUS, keyboard, provisions

0.4

0.9

1

06-52002-C

D8532-261-41

Operator workstation PD DZUS, stowage case lateral

0.3

0.7

1

06-52002-C

D8532-261-42

Operator workstation PD DZUS, searchlight control, holder

0.1

0.2

1

06-52002-C

D8532-261-63

22" Full-HD monitor

7.6

16.8

1

06-52002-C

D3168-300-01

Keyboard - NVG

0.9

2.0

1

06-53003-E

D8532-252-56

Downlink (BMS), transmission system (Helicoder4), vendor parts

3.6

7.9

1

06-53003-E

D8532-254-11

Downlink (BMS), operator workstation installation, fixed provisions

1.3

2.9

1

06-53003-E

D8532-254-26

Downlink (BMS), operator workstation installation, detachable parts

1.3

2.9

1

06-54002-C

D8532-261-34

Video recorder, provisions, operator workstation compatible

0.1

0.2

1

06-54002-C

D8532-261-62

Video recorder

0.7

1.5

Mission Equipment - EOS UltraForce 350 HD Solution

42

k

i

1

06-50007-A

D8532-251-00

EOS UltraForce 350 HD Package j

0.0

0.0

1

06-51199-C

D8532-200-11

EOS, RH step, fixed provisions

9.0

19.8

1

06-51199-C

D8532-200-21

EOS, RH step, detachable parts

8.5

18.7

1

06-51235-A

D8532-251-38

EOS, UltraForce 350 HD, basic system

31.4

69.2

1

06-51235-A

D8532-250-61

EOS, UltraForce 350 Series, video autotracker

0.0

0.0

1

06-51235-A

D8532-250-63

EOS, UltraForce 350 Series, IMU/geo package

0.0

0.0

1

06-51235-A

D8532-250-52

EOS, UltraForce 350 Series, EuroNav moving map interface

0.0

0.0

1

06-51235-A

D8532-250-53

EOS, UltraForce 350 Series, searchlight slaving interface

0.0

0.0

145 D-2 18.101.01 E


Technical Data



Product Title

D2522-000-00

Passenger seating, 8 club seats (standard arrangement)i

kg

lb

94.7

208.8

75.4

166.3

109.0

240.3

2.2

4.9

0.4

0.9

1.0

2.2

Interior Layout 1

07-27021-C

ilm

1

07-27022-B

D2520-600-05

High-density seating, 6 seats (BAE Systems - STC), 3 LH / 3 RH

1

07-27022-B

D2520-900-01

High-density seating, 9 seats (BAE Systems - STC), 3 FWD / 3 LH / 3 RH ilm

1

07-50081-A

D5231-200-00

1

07-75128-B

D8512-800-00

1

07-90030-B

One-hand latching system for clam-shell doors (ADAC - STC)

e

Attachment ring in cabin ceiling LH

D2508-101-00


n

Av io ni cs 1

08-18064-D

D2333-100-02


0.2

0.4

1

08-35066-A

D2327-100-00

Traffic Advisory System TAS620A (Avidyne)

6.1

13.5

1

08-65056-C

D2491-002-00


0.7

1.5

1

08-65056-C

D3113-102-00


0.7

1.5

GSE

GSE

o

1

08-80009-A

D3132-400-00

Professional Ground Station (PGS) Vision System

1

08-81036-C

D3132-000-20

Cockpit Voice and Flight Data Recorder (CVFDR), detachable partsp

0.2

0.4

Cockpit Voice and Flight Data Recorder (CVFDR), vendor parts

4.8

10.6

1

08-81036-C

D3132-000-30

a. The power sockets are normally secured with a 20 A circuit breaker. Depending on the final helicopter configuration the circuit breaker value may vary. b. Requires external hoist damper & hook. Hoist operation and maintenance training included. c. The hoist hook damper can be equipped with 1, 2 or 3 kg additional weight. d. Requires external hoist, detachable parts. e. This STC is EASA certified. Prices and lead times for national certification are available on request. f. Non simultaneous fitment with hoist, detachable parts g. Required for seating configurations with 7 passengers or more. h. Requires single cargo hook system (Onboard) or dual cargo hook system. i. Non simultaneous fitment of / with several seating arrangements. j. Export control approval must be checked with Airbus Helicopters representatives. k. Weight, if installed in the forward position: 12.7 kg. l. This STC is EASA and FAA certified. Prices and lead times for national certifications are available on request. m. Requires multi-purpose fittings in cabin LH and RH. n. Required for hoist installations, if multi purpose fittings in cabin are not installed. o. Recommended 1 per customer base if CVFDR is selected. p. Ground station not included.

4.3.4 Typical Cabin Layout The operator workstation can be installed either in forward (see figure below) or in rear position (see figure in chapter 4.3.1).

Figure 4.15: Law Enforcement configuration (with EOS Star Safire 380Hc package selected and installed in forward position) - cabin layout

145 D-2 18.101.01 E

43


Technical Data

4.3.5 Law Enforcement Mission Performance Weight breakdown (with payload and fuel) Weight basis for Payload range diagram

Equipped empty weight Law Enforcement configuration (incl. engine oil, unusable fuel and weight margin) 2 Pilots (2 x 85 kg) EOS Star Safire 380HDc solution (selected) EOS operator (1 x 85 kg) Payload Reserve fuel: 20 min in 1,500 ft with VY, mean 72 KIAS Trip fuel Mission Takeoff weight

Payload Fuel

kg

lb

2,187

4,823

170 112 85 423 62 661 3,700

375 247 187 932 136 1,457 8,157


Takeoff Cat. A VTOL at SL (maximum 3,700 kg) Climb flight AEO-MCP from SL to 5,000 ft with VY, mean 70 KIAS Level flight in 5,000 ft with VBR, mean 130 KTAS Descent from 5,000 ft to SL with R/D of 1,000 fpm, mean 80 KIAS Landing Cat. A VTOL at SL


Figure 4.16: Law Enforcement configuration - Payload range diagram

Relevant flight data

• Calculated max. range (without payload, with trip fuel): • Corresponding flight time (incl. climb / descent phases): 44

Ar ri el 2E 360 NM (666 km) 2 h 49 min 145 D-2 18.101.01 E


Technical Data

4.4

Aerial Work Mission

Figure 4.17: Aerial Work configuration (with external hoist and cargo hook mirrors selected) - external view (example)

The unobstructed cabin of the H145 is easily reconfigurable to maximize mission flexibility and the sliding and rear clam-shell doors optimize access to the cabin. The high-set main rotor and Fenestron anti-torque-device provide high safety, while loading and unloading passengers or cargo even when rotors are running. The empty weight of the Aerial Work configuration, equipped with the provisions for cargo hook and external hoist, is intentionally kept low to maximize the payload for external and internal transport missions. For further adaptation to customers mission needs, the configuration can be complemented with stretchers, bambi bucket and a variety of seating arrangements.

145 D-2 18.101.01 E

45


Technical Data



• Cat. A

Yes

• Instrumentation

Glass Cockpit

• NVG friendly

No

• EASA OPS

No

Figure 4.18: Aerial Work configuration - cabin layout



Product Title

kg

lb

Baseline Aircraft 1

00-10042-A

D0000-002-00




1,919.0 4,231.4 28.8

63.5




Product Title

kg

lb


46

1

05-03015-B

D2562-000-00

First aid kita

1.2

2.6

1

05-22028-B

D7935-000-00


1.2

2.6

1

05-22029-A

D7114-001-00


0.4

0.9

1

05-22029-A

D7114-002-00


0.4

0.9

1

05-23008-B

D7165-000-00


1.0

2.2

1

05-31121-A

D2514-200-00


2.1

4.6

1

05-37027-A

D6701-001-00


5.6

12.3

1

05-38024-C

D3111-101-00


1.0

2.2

1

05-39017-A

D2513-001-00


0.5

1.1

1

05-41012-A

D2143-000-00


4.2

9.3

145 D-2 18.101.01 E


Technical Data

Qt y Do cu m en t Reference


1

D3343-000-00

05-68012-A

Product Title


kg

lb

0.9

2.0

6.5

14.3

1.6

3.5

26.5

58.4

7.2

15.9

2.9

6.4

Specific Mission Equipment 1 1

06-45086-A 06-67064-A

D3343-600-00 D2563-100-00

Search & landing light Emergency Locator Transmitter (ELT)

b

Interior Layout 1

07-00029-A

D1830-000-00



Av io ni cs 1

08-00449-A

D2300-000-08

1

08-16116-B

D2352-000-00

Digital Voice Control System (DVCS 6100), incl. ACU 6100 (Becker), pilot + copilot c

1

08-22077-A

D2325-700-00


1

08-25035-A

D3455-000-00


2.9

6.4

1

08-26058-A

D3431-000-00


1.1

2.4

1

08-43063-C

D3463-311-00


5.8

12.8

1

08-43063-C

D3463-312-00


7.9

17.4

1

08-43079-A

D3464-000-00


0.1

0.2

1

08-65048-B

D3161-000-00


5.1

11.2

1

08-99003-B

D0000-151-08

23.9

52.7

1

08-35055-C

D3446-000-00

0.1

0.2


1

08-35057-C

D3446-100-00

Synthetic Vision System (SVS) - Helionix

0.0

0.0

1

08-41031-A

D3160-000-00

SBAS RNP approach capabilitye

0.0

0.0

1

08-82000-B

D3139-000-00


0.6

1.3


2.2

4.9

0.2

0.4


05-02063-B

D1113-200-00

f

1

05-31120-B

D5204-301-00


1

05-85017-B

D2841-000-00


0.2

0.4


08-46063-B

D8512-001-10

External hoist, LH, fixed provisionsg

8.7

19.2

1

06-26025-C

D3181-000-00


1.4

3.1

1

06-27042-D

D8511-200-10


8.9

19.6

1

06-27042-D

D8511-300-10

Single cargo hook weighing system, fixed provisions

0.7

1.5

Interior Layout 1

07-50074-A

D8512-401-00


0.2

0.4

1

07-90030-B

D2508-401-00


3.1

6.8

1

07-90030-B

D2508-402-00


3.1

6.8

145 D-2 18.101.01 E

47


Technical Data



Product Title

kg

lb

2.2

4.9

0.6

1.3

0.4

0.9

Av io ni cs 1

08-16172-B

D4361-950-00

Wireless intercom system PNG (Axnes), basic systemh

1

08-16172-B

D4361-960-00

Wireless intercom system PNG (Axnes), cockpit control panel CP50 i

1

08-16172-B

D4361-970-00


2

08-18064-D

D2333-000-02


0.2

0.4

d

1

08-46058-B

D3168-100-00

Moving map - Helionix

0.0

0.0

1

08-81036-C

D3132-000-10

Cockpit Voice and Flight Data Recorder (CVFDR), fixed provisions

3.0

6.6

Subt otal Weight:

145.8

321.5


4.4

9.6


150.2

331.1

Total Weight: 2,098.0 4,626.0

a. Customization of first aid kit content necessary to comply with EASA OPS requirements. Medications may have to be removed for export. b. ELT code to be provided by the customer latest 4 months prior to helicopter delivery. c. Incl. ADS-B out. d. The database update service is provided under a dedicated service contract. Please contact your Airbus helicopter sales representative for further information. e. SBAS RNP approach local service availability verification through your Airbus helicopter sales representative on request. f. Required for hoist operation. g. Weight, in combination with Emergency floats, detachable parts: 11.5 kg. h. Requires wireless intercom system PNG (Axnes), cockpit control panel. Mobile transceiver not included. i. Mobile transceiver with defined frequency range between 440 – 450 MHz in yellow color.

4.4.3 Further Available Equipment Q ty Do cu men t Reference


Product Title

kg

lb

General Equipm ent 1

05-21021-A

D8541-000-10


2.9

6.4

1

05-21021-A

D8541-000-20


7.7

17.0

63.0

138.9


06-21037-B

D8512-000-20

External hoist (without hook), detachable partsa

1

06-21037-B

D8512-100-00


3.6

7.9

1

06-21037-B

D8512-200-00


0.4

0.9

3.0

6.6

0.7

1.5

0.8

1.8

1

06-21037-B

D8512-900-00


1

06-21038-A

D8512-301-10


1

48

b

06-21038-A

D8512-300-20

c


d

1

06-21039-A

D8510-010-00

Teflon coating for cable deflector on floats landing gear, LH

0.5

1.1

1

06-26025-C

D3181-100-00


1.6

3.5

1

06-27042-D

D8511-200-20


7.7

17.0

1

06-27042-D

D8511-300-20

Single cargo hook weighing system, detachable parts

0.3

0.7

1

06-61032-B

D3214-000-10


2.3

5.1

1

06-61032-B

D3214-000-20


67.3

148.4

2.6

5.7

0.6

1.3

nd

e

1

06-65013-A

D2625-200-00

2

portable fire extinguisher

1

06-81031-A

D8511-600-10

Electrical release for fire extinguishing bucket (Bambi Bucket), fixed provisionsf

145 D-2 18.101.01 E


Technical Data



Product Title

D2522-000-00

Passenger seating, 8 club seats (standard arrangement)g

kg

lb

94.7

208.8

37.7

83.1

109.0

240.3

2.2

4.9

18.7

41.2

4.4

9.7

1.0

2.2

Interior Layout 1

07-27021-C

ghi

1

07-27022-B

D2520-300-02

High-density seating, 3 seats (BAE Systems - STC), 3 RH

1

07-27022-B

D2520-900-01

High-density seating, 9 seats (BAE Systems - STC), 3 FWD / 3 LH / 3 RH gij

1

07-50081-A

1

07-74092-A AA T-45120-014-2

1 1

07-75110-B 07-90030-B

D5231-200-00

D2524-000-00

One-hand latching system for clam-shell doors (ADAC - STC)

k

Foldable stretcher for helicopter floor incl. Locker Systems (AAT - STC), LH/RHgk Attachment rails in cabin ceiling l

D2508-101-00


D4321-000-00

Tactical radio, fixed provisions, power supply (12 VDC) & intercom interfacem

1.4

3.1

Tactical radio, fixed provisions, power supply (28 VDC) & intercom interfacem

0.5

1.1

Av io ni cs 1 1

08-12090-A 08-12090-A

D4321-100-00

m

1

08-12090-A

D4322-100-00


0.8

1.8

1

08-15564-A

D2316-000-00

Iridium satellite transceiver GSR 56 (Garmin)

3.0

6.6

1

08-18064-D

D2333-100-02


0.2

0.4

GSE

GSE

n

1

08-80009-A

D3132-400-00

Professional Ground Station (PGS) - Vision System

1

08-81036-C

D3132-000-20

Cockpit Voice and Flight Data Recorder (CVFDR), detachable partso

0.2

0.4

Cockpit Voice and Flight Data Recorder (CVFDR), vendor parts

4.8

10.6

1

08-81036-C

D3132-000-30

a. Requires external hoist damper & hook. Hoist operation and maintenance training included. b. The hoist hook damper can be equipped with 1, 2 or 3 kg additional weight. c. Requires external hoist, detachable parts. d. Required if external hoist and emergency floats are selected. e. Required for seating configuration with 7 pax or more. f. Requires single cargo hook system (Onboard) or dual cargo hook system. g. Non simultaneous fitment of several seating arrangements. h. Requires multi-purpose fittings in cabin RH. i. This STC is EASA and FAA certified. Prices and lead times for national certifications are available on request. j. Requires multi-purpose fittings in cabin LH and RH. k. This STC is EASA certified. Prices and lead times for national certifications are available on request. l. Required for hoist installations, if multi pupose fittings in cabin are not installed. m. Onboard HF/tactical radio transmission can influence radio navigation systems (MKR, VOR, ILS, ADF) and communication systems (VHF radio, other tactical radio). Depending on National Aviation Authorities certification requirements, tactical radio systems must either be turned off during IFR approaches/departures or deactivated. n. Recommended 1 per customer base if CVFDR is selected. o. Ground station not included.

145 D-2 18.101.01 E

49


Technical Data

4.4.4 Aerial Work Mission Performance Weight breakdown (with payload and fuel) Weight basis for Payload range diagram Payload Fuel

Equipped empty weight Aerial Work configuration (incl. engine oil, unusable fuel and weight margin) 1 Pilot (1 x 85 kg) Payload Reserve fuel: 20 min in 1,500 ft with VBR, mean 131 KTAS Trip fuel Mission Takeoff weight

kg

lb

2,098

4,626

85 794 83 640 3,700

187 1,750 183 1,411 8,157


Takeoff Cat. A VTOL at SL (maximum 3,700 kg) Climb flight AEO-MCP from SL to 5,000 ft with VY, mean 70 KIAS Level flight in 5,000 ft with VBR, mean 134 KTAS Descent from 5,000 ft to SL with R/D of 1,000 fpm, mean 80 KIAS Landing Cat. A VTOL at SL


Figure 4.19: Aerial Work configuration - Payload range diagram

Relevant flight data

• Calculated max. range (without payload, with trip fuel): • Corresponding flight time (incl. climb / descent phases):

50

Ar ri el 2E 367 NM (680 km) 2 h 47 min

145 D-2 18.101.01 E


Technical Data

5

Equipment Information

5.1

General Available Equipment The following list presents the General Available Equipment which may be added to customize the mission configuration or to build specific configurations. For further mission adaptation specific items are also available on request. Please take into account that there may be incompatibilities between various optional equipment items. Any modification and/or complement of the proposed mission configuration must be done with the assistance of an Airbus helicopter sales representative. The General Available Equipment are categorized as shown in the following table: Ab br evi ati on

Av ail abi li ty

R

Included in the Mandatory or Reference Equipment of the mission confi guration

F

Incl uded i n the Further Avail abl e Equip ment of the mission configurati on

G

General Available Equipment for the mission configuration

Document Reference


t k lb S n r o n M i e o E t a m W t l r e a o c i r p r o s f e n n A a r E T w a e r L o h s f f O

Product Title

kg

0.5

1.1

G

0.0

0.0

G

General Equi pment

05-02066-A

D1113-500-00

Surface protective coating (Airglaze)

05-02072-B

D6211-000-00

Main Rotor Blade Erosion Protection Paint a

05-12008-B

D8513-000-10

Multi-purpose pylon LH & RH, fixed provisions

12.6

27.8

05-12008-B

D8513-000-20

Multi-purpose pylon LH & RH, detachable parts incl. aerodynamic fairingsa

25.2

55.6

G

G

G

G

G

05-21021-A

D8541-000-10


2.9

6.4

R

G

R

F

05-21021-A

D8541-000-20


7.7

17.0

R

G

R

F

05-21034-A

D7162-000-00

Inlet Barrier Filter (IBF) System

23.9

52.7

F

G

F

G

05-31120-B

D5204-301-00


0.2

0.4

F

F

R

R

05-31120-B

D5204-302-00


0.2

0.4

G

F

R

G

05-31124-A

D5621-000-00

Push-out cabin windows

3.3

7.3

G

R

G

05-31125-A

D5632-101-00

Sliding window with ram air deflector in sliding door, LH

0.8

1.8

G

G

G

G

05-31125-A

D5632-102-00

Sliding window with ram air deflector in sliding door, RH

0.8

1.8

G

G

G

G

05-31126-B

D5634-100-00

Tinted windows in cockpit doors

0.0

0.0

G

G

G

G

05-31126-B

D5634-200-00

Tinted windows in sliding doors

0.0

0.0

G

G

G

G

05-31126-B

D5634-400-00

Tinted windows in cabin

1.3

2.9

G

G

G

G

05-31126-B

D5634-501-00

Tinted window in clam-shell door, LH

0.3

0.7

G

G

G

G

05-31126-B

D5634-502-00

Tinted window in clam-shell door, RH

0.3

0.7

G

G

G

G

05-31126-B

D5634-600-00

Tinted push-out cabin windows

3.2

7.1

G

G

G

05-31133-A

D5611-000-00

Windscreen hard coating

0.0

0.0

G

G

G

05-36029-C

D3211-001-00

Flat step patches on multifunction step, LH

1.9

4.2

G

G

F

05-36032-B

D3230-301-00

5.3

11.7

G

G

R

-3.5

-7.7

F

G

G

05-37028-A

145 D-2 18.101.01 E

D6721-001-00

Aluminum multifunction step LH instead of standard boarding step Pedal cover for copilot flight controls

G

G

51


Technical Data

t k lb S n r o n M i e o E t m a W t r e c l a o r r p o i s f e n n A a r E T w a e r L o h s f f O

Document Reference


Product Title

kg

05-39018-A

D3318-101-00

Illuminated chart holder, copilot side

0.8

1.8

G

G

G

G

05-39018-A

D3318-102-00

Illuminated chart holder, pilot side

0.8

1.8

G

G

G

G

05-39019-A

D2514-100-00

Map case on instrument panel glare shield

0.6

1.3

G

G

G

G

05-41011-A

D2142-100-00

Performance improvement kit for bleed air heating system

3.9

8.6

G

G

G

G

05-42048-A

D2111-000-00

44.3

97.7

G

G

G

G

05-42048-A

D2122-200-00

14.1

31.1

G

G

G

G

05-62026-A

D2420-000-00

1.6

3.5

G

R

G

G

0.6

1.3

G

G

G

G

Air Conditioning System (ACS) Environmental Control System (ECS) Alternating Current (AC) system b

05-67030-B

D2465-000-00

Power socket (28 VDC) at LH rear cabin wall

05-67030-B

D2465-100-00

Power sockets (28 VDC) at center console and LH rear cabin wallb

1.1

2.4

G

G

G

G

Power sockets (14 VDC & 28 VDC) at center console and LH rear cabin wall b

2.6

5.7

G

G

F

G

2.2

4.9

G

G

G

38.0

83.8

G

G

G

05-67030-B

D2465-200-00

05-81044-A

D2818-100-10

Internal long range fuel tank system, fixed provisions

05-81044-A

D2818-100-20

Internal long range fuel tank system, detachable parts

05-81045-A

D2812-000-00

Self-sealing fuel supply tanksc

8.5

18.7

05-92018-C

D6611-000-00

Main rotor blade folding, basic kit

0.3

0.7

G

G

G

G

05-92018-C

D6611-100-10

Main rotor blade folding, fixed provisions for ground handling kit

0.7

1.5

G

G

G

G

GSE

GSE

G

G

G

G

G

05-92018-C

D6611-100-20

Main rotor blade folding, ground handling kit

05-93014-C

D1021-100-00

Lashing points

1.1

2.4

G

R

G

G

05-36034-A

D5310-000-00

Step areas on cabin roof

0.1

0.2

G

G

G

G

05-36034-A

D7113-000-00

0.8

1.8

G

G

G

G

Additional maintenance handles on transmission cowling

Specific Mission Equipment

52

06-11042-A

D3275-000-10

Settling protectors, fixed provisions

0.2

0.4

G

G

G

G

06-11042-A

D3275-000-20

Settling protectors, detachable parts

7.9

17.4

G

G

G

G

06-11043-A

D3272-000-00

Snow skids

22.5

49.6

G

G

G

G

08-46063-B

D8512-001-10

External hoist, LH, fixed provisions

8.7

19.2

F

G

R

R

08-46063-B

D8512-002-10

External hoist, RH, fixed provisions

9.8

21.6

G

F

G

G

06-21037-B

D8512-000-20


63.0

138.9

F

F

F

F

06-21037-B

D8512-100-00


3.6

7.9

F

F

F

F

06-21037-B

D8512-200-00


0.4

0.9

G

F

F

F

06-21037-B

D8512-900-00


3.0

6.6

G

F

F

F

06-21038-A

D8512-301-10


0.7

1.5

G

G

F

F

06-21038-A

D8512-302-10

External hoist observation light, RH, fixed provisions

0.7

1.5

G

F

G

G

06-21038-A

D8512-300-20


0.8

1.8 G

F

F

F

06-21039-A

D8510-010-00

Teflon coating for cable deflector on floats landing gear, LH

0.5

1.1

G

G

G

F

06-21039-A

D8510-020-00

Teflon coating for cable deflector on floats landing gear, RH

0.5

1.1

G

F

G

G

06-24020-B

D8534-001-10

External rope down device, LH, fixed provisions

2.3

5.1

G

G

06-24020-B

D8534-002-10

External rope down device, RH, fixed provisions

2.3

5.1

R

G

06-24020-B

D8534-101-20

External rope-down device for 2/1 persons (ECMS -STC), LH retractable, detachable parts d

17.3

38.1

G

G

145 D-2 18.101.01 E


Technical Data

Document Reference


Product Title

06-24020-B

D8534-102-20

External rope-down device for 2/1 persons (ECMS - STC), RH retractable, detachable parts d

kg


17.3

38.1

G

G

06-26023-A

D8511-000-10

Cargo hook mirrors, fixed provisions

1.1

2.4

G

G

G

G

06-26023-A

D8511-000-20

Cargo hook mirrors, detachable parts

4.0

8.8

G

G

G

G

06-26023-A

D8511-100-00

Cover for cargo hook mirrors

GSE

GSE

G

G

G

G

06-26025-C

D3181-100-00


1.6

3.5

F

G

G

F

06-27042-D

D8511-200-10


8.9

19.6

G

F

G

R

06-27042-D

D8511-200-20


7.7

17.0

G

F

G

F

06-27042-D

D8511-300-10

Single cargo hook weighing system, fixed provisions

0.7

1.5

G

G

G

R

06-27042-D

D8511-300-20

Single cargo hook weighing system, detachable parts

0.3

0.7

G

G

G

F

06-27044-C

D8511-400-10


5.9

13.0

F

G

R

G

06-27044-C

D8511-400-20


29.6

65.3

F

G

F

G

06-27044-C

D8511-500-10

Dual cargo hook weighing system, fixed provisions

0.3

0.7

G

G

G

G

06-27044-C

D8511-500-20

Dual cargo hook weighing system, detachable parts

0.2

0.4

G

G

G

G

06-31025-C

D8531-000-00


10.9

24.0

F

G

F

G

06-45074-D

D3346-000-10

Searchlight A800 (Trakka) basic LH, fixed provisions

5.5

12.1

G

G

R

06-45074-D

D3346-000-20

Searchlight A800 (Trakka) basic LH, detachable parts

18.9

41.7

G

G

R

06-45074-D

D3346-000-30

Searchlight A800 (Trakka), vendor parts

18.2

40.1

G

G

R

06-45074-D

D3346-600-10

Searchlight A800 (Trakka), hand controller, fixed provisions

0.6

1.3

G

G

R

Searchlight A800 (Trakka), hand controller, detachable parts

0.9

2.0

G

G

R

GSE

GSE

G

G

R

1.4

3.1

R

G

G

G

06-45074-D

D3346-600-20

06-45074-D

D3346-700-00

Searchlight A800 (Trakka), covers

06-46010-B

D3347-000-00

White strobe lights ®

06-46011-A

D3347-400-00

Fenestron light

0.7

1.5

G

G

G

G

06-61032-B

D3214-000-10


2.3

5.1

G

R

G

F

06-61032-B

D3214-000-20


67.3

148.4

G

R

G

F

06-61038-A

D2565-100-10

Emergency floats with integrated life rafts (DART - STC), fixed provisionsa e f

3.5

7.6

Emergency floats with integrated life rafts (DART - STC), detachable partsa f

78.0

172.0

2 portable fire extinguisher, high-density seating, 10 seats BAE

2.9

6.4

R

G

G

06-61038-A 06-65013-A

D2565-100-20 D2625-300-00

nd

06-71001-B

D2517-000-10


0.3

0.7

R

G

R

G

06-71001-B

D2517-000-20

Separation curtain for cockpit / cabin, detachable parts

0.8

1.8

G

G

G

G

06-71001-B

D2517-100-20


0.3

0.7

R

G

R

G

0.0

0.0

G

G

F

G


1.8

4.0

R

R

R

G


1.8

4.0

R

R

R

G

06-90013-A

D0000-600-00

Alternate gross weight 3,800 kg

Interior Layout

07-15028-B 07-15028-B

145 D-2 18.101.01 E

D2512-101-00 D2512-102-00

53


Technical Data

Document Reference


Product Title

kg

07-27021-C

D2522-000-00

Passenger seating, 8 club seats (standard arrangement)

07-27021-C

D2522-800-01


94.7

208.8

G

R

F

F

Passenger seating, backrest cover with literature stowage net

0.8

1.8

G

G

G

G

07-27021-C

D2522-800-02

Passenger seating, lumbar support

0.2

0.4

G

G

G

G

07-27021-C

D2522-800-03

Passenger seating, armrests

1.4

3.1

G

G

G

G

07-27021-C

D2522-800-05

Passenger seating, tray table

0.5

1.1

G

G

G

G

07-27021-C

D2522-800-06

Passenger seating, stowage drawer below seat

0.8

1.8

G

G

G

G

07-27021-C

D2522-800-07

Passenger seating, stowage pocket below seat

0.1

0.2

G

G

G

G

07-27022-B

D2520-000-01

High-density seating, 10 seats (BAE Systems - STC), 3 FWD / 2 LH / 2 RH / 3 AFT f

123.5

272.3

F

G

G

High-density seating, 3 seats (BAE Systems - STC), 3 RHf

37.7

83.1

G

G

F

High-density seating, 6 seats (BAE Systems - STC), 3 FWD / 3 AFT f

67.5

148.8

F

G

G

High-density seating, 6 seats (BAE Systems - STC), 3 LH / 3 RH f

75.4

166.3

F

F

G

High-density seating, 8 seats (BAE Systems - STC), 3 FWD / 3 LH / 2 RH f

99.3

219.0

F

G

G

G

07-27022-B 07-27022-B 07-27022-B 07-27022-B

D2520-300-02 D2520-600-04 D2520-600-05 D2520-800-03

G

07-27038-A

D2521-000-00

Offshore Seating Arrangement, enhanced kit

7.0

15.4

07-30067-B

D2581-000-00

Sound proofing kit

5.9

13.0

G

F

G

G

07-40031-A

D2515-000-00

Washable floor covering for cockpit, cabin & cargo compartment

15.2

33.5

F

G

G

G

G

07-40033-A

D2525-000-00

Sealed cabin floor

0.4

0.9

R

G

07-50071-A

D5221-000-00

Jettisonable cockpit doors

0.6

1.3

G

R

G

07-50072-D

D5204-100-00

Spoiler position for cockpit doors, intermediate position

1.1

2.4

G

R

07-50072-D

D5204-200-00

Spoiler position for cockpit doors, intermediate and max. position

1.2

2.6

G

a

07-50073-B

D5223-000-00

Jettisonable sliding doors

2.9

6.4

G

07-50074-A

D8512-401-00


0.2

0.4

F

R

R

R

07-50074-A

D8512-402-00


0.2

0.4

F

R

R

G

07-60046-A

D8504-100-00

Universal cargo net

2.5

5.5

G

G

G

G

18.7

41.2

G

F

G

G

F

07-74092-A AA T-45120-014-2 Foldable stretcher for helicopter floor incl. Locker Systems (AAT - STC), LH/RH d 07-75110-B

D2524-000-00

Attachment rails in cabin ceiling

4.4

9.7

07-75128-B

D8512-800-00

Attachment ring in cabin ceiling LH

0.4

0.9

F

G

F

G

07-90030-B

D2508-101-00


1.0

2.2

F

G

F

F

07-90030-B

D2508-102-00

Multi-purpose fittings in cabin, FWD RH

1.0

2.2

G

F

G

G

07-90030-B

D2508-401-00


3.1

6.8

R

F

R

R

07-90030-B

D2508-402-00


3.1

6.8

R

F

R

R

D2311-000-10

HF system HF-9000 (Rockwell Collins), fixed provisionsc

12.5

27.6

G

G

11.8

26.0

G

G

Av io ni cs

08-10025-B 08-10025-B

54

D2311-000-20

c

HF system HF-9000 (Rockwell Collins), detachable parts

145 D-2 18.101.01 E


Technical Data


Document Reference


Product Title

kg

08-10025-B

D2311-100-00

HF system control unit HF9010 (Rockwell Collins) c

1.0

2.2

08-12090-A

D4321-000-00

Tactical radio, fixed provisions, power supply (12 VDC) & intercom interface

1.4

3.1

Tactical radio, fixed provisions, power supply (28 VDC) & intercom interface

0.5


08-12090-A 08-12090-A

D4321-100-00 D4322-100-00

G

G

G

G

F

G

F

1.1

R

F

R

F

0.8

1.8

R

F

R

F

R

G

G

08-12093-C

D4321-320-00

Tactical radio VHF-FM NPX138N - NVG (Cobham)

2.6

5.7

G

08-14103-A

D4322-000-10

Tactical radio RT-5000 and C-5000 control - NVG, fixed provisionsc

5.9

13.0

G

G

G

10.8

23.8

G

G

G

08-14103-A 08-16161-B

D4322-000-20 D2341-800-00

Tactical radio RT-5000 and C-5000 control - NVG, detachable partsc Audio/Comm. control unit ACU 610X (Becker), EMS fixed provisions

0.4

0.9 G

08-17090-B

D2331-010-00

Cabin loudspeaker

2.1

4.6

G

F

G

G

08-17091-A

D2334-000-00

Passenger address Interface

0.9

2.0

G

R

G

G

08-18065-B

D2315-300-00

Headset H10-76 (David Clark), low impedance

0.6

1.3

G

R

G

G

08-24035-A

D3452-000-00

Automatic Direction Finder (ADF), receiver DF-431B (Cobham)

7.7

17.0

G

G

Automatic Direction Finder (ADF), control unit CDF552 (Cobham)

1.3

2.9

G

G

Color weather radar RDR 2000 (Honeywell), fixed provisions

2.0

4.4

G

G

G

G

Color weather radar RDR 2000 incl. control unit CP466 - NVG (Honeywell), vendor parts

5.8

12.8

G

G

G

G

0.4

0.9

G

G

G

G

08-24035-A 08-31064-A 08-31064-A

D3452-100-00 D3443-000-10 D3443-020-30

08-31064-A

D3443-100-00

Color weather radar RDR 2000 (Honeywell), radar radome

08-31065-A

D3443-200-00

Search and Rescue weather radar RDR-1600 (Telephonics)

16.0

35.5

G

R

G

G

Search and rescue weather radar RDR-1600 (Telephonics), radar radome

6.3

13.9

G

R

G

G

3.1

6.8

0.0

0.0

0.0

0.0

0.0

0.0

0.0

0.0

6.3

13.9

08-31065-A 08-15582-A 08-15582-A 08-15582-A 08-15582-A 08-15582-A 08-35064-C

D3443-300-00 D8548-000-00 D8548-100-00 D8548-200-00 D8548-300-00 D8548-400-00 D8547-200-00

a

Basic platform computer

a

Real time overlay download application a

Hot spot / router application a

Fleet tracking application a

VoIP

a

Enhanced Reality System (EuroAvionics), basic system

a

08-35064-C

D8547-100-00

Enhanced Reality System (EuroAvionics), extension box

2.4

5.3

08-35064-C

D8547-300-00

Enhanced Reality System (EuroAvionics), WIFI video streaminga

0.0

0.0

a

08-35064-C

D8547-400-00

Enhanced Reality System (EuroAvionics), control unit

0.3

0.7

08-35066-A

D2327-100-00

Traffic Advisory System TAS620A (Avidyne)

6.1

13.5

G

G

F

G

08-43076-B

D3463-600-00

0.0

0.0

G

G

G

G

08-46058-B

D3168-100-00

0.0

0.0 G R

145 D-2 18.101.01 E

Approach charts (IFR) georeferenced for GTN 750 Moving map - Helionix

R

55


Technical Data


Document Reference


Product Title

kg

08-46063-D

D3168-200-00

Moving map EuroNav 7 – RN7CM (EuroAvionics), basic version

3.3

7.3

G

G

Moving map EuroNav – RN7 (EuroAvionics), FLARM module

0.7

1.5

G

G

Moving map EuroNav 7 – RN7 & RN7CM (EuroAvionics), weather radar interface

0.0

0.0

G

G

08-46063-D 08-46063-D

D3168-700-00 D3168-900-00

08-65056-C

D2491-001-00

Electrical fixed provisions, 5 VDC, copilot

0.7

1.5

G

F

G

G

08-65056-C

D2491-002-00


0.7

1.5

R

R

F

G

08-65056-C

D2491-100-00

Electrical fixed provisions, 5 VDC, center console

0.7

1.5

G

R

G

G

08-65056-C

D3113-101-00

iPad Air holder, copilot

0.7

1.5

G

F

G

G

08-65056-C

D3113-102-00


0.7

1.5 R

R

F

G

08-83042-B

D3171-200-10


4.0

8.8

F

R

G

G

08-83042-B

D3171-200-20


3.6

7.9

F

R

G

G

08-83046-A

D3171-100-00

Helicopter Flight Data Monitoring (HFDM)

GSE

GSE

G

R

G

G

Operational Equipment

10-20022-B

D8551-000-10

Light armor protection kit, cockpit floor, fixed provisionsac

1.9

4.2

10-20022-B

D8551-000-20

Light armor protection kit, cockpit floor, detachable parts, HPPEac

19.2

42.3

1.2

2.6

Light armor protection kit, cockpit vertical plates, detachable parts, HPPEac

32.1

70.8

Light armor protection kit, cabin floor, fwd, fixed provisionsac

0.1

0.2

21.0

46.3

0.1

0.2

49.2

108.5

34.0

75.0

11.1

24.5

1.4

3.1

10-20022-B 10-20022-B 10-20022-B 10-20022-B

D8551-100-10 D8551-100-20 D8551-200-10 D8551-200-20

Light armor protection kit, cockpit vertical plates, fixed provisionsac

Light armor protection kit, cabin floor, fwd, detachable parts, HPPEac ac

10-20022-B

D8551-300-10

Light armor protection kit, cabin floor, aft, fixed provisions

10-20022-B

D8551-300-20

Light armor protection kit, cabin floor, aft, detachable parts, HPPEac

10-40004-A

D8581-100-00

Self-protection system, core

ac

10-40004-A

D8581-200-00

Missile Launch Detectors (MLD) for self-protection systemac ac

10-40006-A

D8581-300-00

Mission safety system

10-90005-B

D8581-001-00

Pintle mount for 7.62 mm machine gun, MAG58 (M240), LHac

32.1

70.8

Pintle mount for 7.62 mm machine gun, MAG58 (M240), RHac

32.1

70.8

10-90005-B

D8581-002-00

a. This item is available on request. b. The power sockets are normally secured with a 20 A circuit breaker. Depending on the final helicopter configuration the circuit breaker value might vary. c. Export control approval must be checked with Airbus Helicopters representatives. d. This STC is EASA certified. Prices and lead times for national certifications are available on request. e. Requires emergency floats with integrated liferafts (DART - STC) detachable parts, emergency floats fixed provisions and emergency floats landing gear. f. This STC is EASA and FAA certified. Prices and lead times for national certifications are available on request.

56

145 D-2 18.101.01 E


Technical Data

5.2

A vi on ic s L ay ou ts

5.2.1 Single / Dual Pilot IFR with Dual GTN 750 1. Flight Display Subsystem FDS (copilot) 2. GPS / NAV / COM (copilot) GTN750 (Garmin) 3. Audio / Comm. Control Unit ACU6100 (copilot) 4. Cockpit control panel 5. Autopilot control unit 6. GPS / NAV / COM (pilot) GTN750 (Garmin) 7. Audio / Comm. Control Unit ACU6100 (pilot) 8. DTD: Data Transfer Device

Figure 5.1: Avionics Layout - Single / Dual Pilot IFR with Dual GTN 750 (example)

Content of Avi onic s Package for Singl e / Dual Pilot IFR with Dual GTN 750 Qt y Do cu men t Reference


1

08-00449-A

D2300-000-08

1

08-16116-B

D2352-000-00

Product Title

kg

lb


7.2

15.9


1

08-22077-A

D2325-700-00


2.9

6.4

1

08-25035-A

D3455-000-00


2.9

6.4

1

08-26058-A

D3431-000-00


1.1

2.4

1

08-43063-C

D3463-311-00


5.8

12.8

1

08-43063-C

D3463-312-00


7.9

17.4

1

08-43079-A

D3464-000-00


0.1

0.2

08-65048-B

D3161-000-00


5.1

11.2

08-99003-B

D0000-151-08

23.9

52.7

1

145 D-2 18.101.01 E

Avionics Package DP IFR GTN Series interconnection / wiring

57


Technical Data

5.2.2 Single / Dual Pilot IFR with FMS1 1. Flight Display Subsystem FDS (copilot) 2. COM / NAV control unit 3. Audio / Comm. Control Unit ACU6100 (copilot) 4. Autopilot control unit 5. Cockpit control panel 6. DTU: Data Transfer Unit 7. DTD: Data Transfer Device 8. Flight Management System CMA-9000a 9. Audio / Comm. Control Unit ACU6100 (pilot)

Figure 5.2: Avionics Layout - Single / Dual Pilot IFR with FMS (example)

Content of Av ionics Package for Single / Dual Pilot IFR with FMS Q ty Do cu men t Reference


1

08-00045-A

D2300-000-02

1

08-11047-B

D2313-102-00

1

08-11047-B

1

08-16116-B

Product Title

kg

lb

VHF AM/COM system VHF-4000F (Rockwell Collins), pilot

2.8

6.2

D2313-101-00

VHF AM/COM system VHF-4000F (Rockwell Collins), copilot

2.8

6.2

D2352-000-00


7.2

15.9

Avionics Package DP IFR CMA-9000

1

08-22059-A

D2325-100-00

Transponder (Mode S) TDR-94 (Rockwell Collins)

4.5

9.9

1

08-25035-A

D3455-000-00


2.9

6.4

1

08-26059-A

D3432-002-00

VOR/ILS/MKR navigation system NAV-4500 (Rockwell Collins), pilot

3.3

7.3

1

08-26059-A

D3432-001-00

VOR/ILS/MKR navigation system NAV-4500 (Rockwell Collins), copilot

2.1

4.6

1

08-26060-A

D3432-100-00

COM/NAV combined control unit CTL-4000 (Rockwell Collins), pilot

2.1

4.6

a

1

08-44057-A

D3442-100-00

GPS sensor CMA-5024 for CMA-9000 (CMC Electronics)

4.4

9.7

1

08-44057-A

D3463-102-00

Flight Management System (CMA-9000) - Single (CMC Electronics)a

7.0

15.4

1

08-65048-B

D3161-000-00


5.1

11.2

1

08-99003-B

D0000-151-02

24.7

54.5

Avionics Package DP IFR CMA-9000 interconnection / wiring

a. Export control approval must be checked with Airbus Helicopters representatives. 1. Available on request. 58

145 D-2 18.101.01 E


Technical Data

5.3

A nt en na L ay ou t

1. VHF-AM1 antenna 2. Transponder antenna 3. DME antenna

4. Marker antenna 5. Radar altimeter antennas 6. VOR / ILS antenna

7. VHF-AM2 antenna 8. GPS1 antenna 9. GPS2 antenna

Figure 5.3: Typical IFR antenna layout

5.4

NVG friendly & NVIS Certification In order to increase mission capabilities and flight safety during night operations, the H145 can be fitted with NVG friendly cockpit and cabin layouts as well as NVG friendly exterior lighting. Helicopters in an "NVG friendly" configuration are designed and built in order to not degrade the NVG image performance, by considering the design standards detailed hereafter: • The internal lighting of the cockpit is designed and built in order to fulfill RTCA/DO-275 "Minimum Operational Performance Standard for Integrated Night Vision Imaging System Equipment". • All NVIS equipment items installed (excluding BFE) are not degrading the NVG image performance or the NVG image performance degradation is kept within acceptable limits in NVG mode. Note: BFE might not be compliant in accordance with the applicable specifications and requirements. Airbus does not perform any actions to ensure the NVG performance degradation is being kept within acceptable limits.

• The interior of the helicopter is kept in dark, matt colors, showing no or only little reflectance of radiation, not degrading the NVG image performance in NVG mode. • An appropriate Day/Night/NVG switch is provided. • The external lighting of the cockpit is designed and built in order to fulfill SAE-ARP 4392, "Lighting, Aircraft Exterior, Night Vision Imaging System (NVIS) Compatible", i. e. the NVG performance degradation caused by the external lighting system in NVG mode is kept within acceptable limits.

145 D-2 18.101.01 E

59


Technical Data

May 31, 2007, the first NVIS certification providing the H145 predecessor EC145 with a NVG aided operation capability was granted from EASA, FAA and TCCA (Canada). Thus Airbus Helicopters is the first Original Equipment Manufacturer (OEM) to offer this capability to civil operators. The EASA NVIS certification is based on one customer specific NVIS configuration; any additional changes to the configuration following EASA NVIS certification may require additional certification effort. EASA NVIS certification is based on night vision goggles with class B filter from well-known manufacturers (certified goggles include ITT F4949 and L3 Communications M949). On customer's request, Airbus can develop and certify also night vision goggle systems from other manufacturers. Please note that classic night flight capability remains unrestricted. For the avoidance of doubt, configurations marked as being "NVG friendly" in this document do not include a helicopter NVIS certification. Such "Night Vision Imaging System (NVIS) certification" is only provided by Airbus, if it is explicitly listed in the individual customer's contract. The "Night Vision Imaging System (NVIS) certification" includes delivery of a customer configuration specific Flight Manual Appendix ("Appendix for Night Vision Imaging Systems (NVIS) / NVG - Operator") and "Operator Substantiation Report for Night Vision Imaging System (NVIS) / NVG" and provides proof of compliance with the airworthiness requirements for t he NVG operations capabilities of the helicopter. Note that the "Night Vision Imaging System (NVIS) certification" does not constitute an approval for NVG operations as per Commission Regulation No 965/2012, SPA.NVIS.100 ("Helicopters shall only be operated under VFR at night with the aid of NVIS if the operator has been approved by the competent authority").

5.5

Disclaimers EASA OPS The EMS and Offshore Transportation mission configuration is derived from the conditions stated in EASA OPS. This package does not cover oxygen equipment and the entire equipment required for extended over water or offshore operations. For approval of the aircraft configuration for the intended mission, the operator shall contact his national authority. Basic p ackage:

• • • •

60

Illuminated Chart Holder, Pilot or iPad Air holder, Pilot 2nd Portable Fire Extinguisher, if more than seven passengers on board Cockpit Voice and Flight Data Recorder (CVFDR) Emergency Locator Transmitter (ELT)

145 D-2 18.101.01 E


Technical Data

Export control regulations Airbus Helicopters is committed to strict compliance with all applicable export control regulations and requires a corresponding commitment from the Customer. Some items/commodities are controlled under at least one export control law or regulation and therefore may require export authorization(s) and Airbus Helicopters cannot guarantee that they will be granted. Nevertheless Airbus Helicopters will perform all necessary procedures for obtaining such authorization(s). The Customer shall support the authorization(s) application(s) procedure(s) by providing the necessary documentation and information, particularly end-user certificates, undertakings, documents on the utilization of the items/commodities, etc. The Customer shall comply with the conditions of the export authorization(s). Airbus Helicopters reserves the right to deliver the helicopter without the controlled items, should the competent authorities deny or delay export authorization(s). The same is valid if the competent authorities do not react at all or in cases of a return without action or if otherwise the absence of a required authorizations or provisions of any regulations inhibit a delivery in time.

145 D-2 18.101.01 E

61


Technical Data

Blank

62

145 D-2 18.101.01 E


Technical Data

6

Main Performance The performance figures shown hereafter are guaranteed minimum performance data (minimum specificaton engine power). Only the fuel consumption, range, endurance values and figures refer to an H145 equipped with minimum specified new production engines. Unless otherwise specified, the values and figures refer to a clean helicopter at Sea Level (SL), in International Standard Atmosphere (ISA) and zero wind condition.

6.1

Performance Summary Tables Al l Engi ne Operativ e (AEO) - Al ti tu de Gross weight

Hover ceiling IGE (4 ft AGL), TOP • ISA • ISA +20°C Hover ceiling OGE, TOP • ISA

kg lb

2,700 5,952

3,000 6,614

3,300 7,275

3,585 7,904

3,650 8,047

3,700 8,157

m 6,096 5,608 4,785 4,115 3,932 3,825 ft 20,000 18,400 15,700 13,500 12,900 12,550 m 5,395 4,968 4,115 3,353 3,200 3,048 ft 17,700 16,300 13,500 11,000 10,500 10,000 m 6,050 5,151 4,237 3,399 ft 19,850 16,900 13,900 11,150

3,018 9,900

2,667 8,750

• ISA +20°C

m 5,395 4,450 3,566 ft 17,700 14,600 11,700

2,591 8,500

2,332 7,650

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

m 6,096 6,096 6,096 5,593 5,410 5,029 ft 20,000 20,000 20,000 18,350 17,750 16,500

2,789 9,150

Al l Engi ne Operativ e (AEO) - Speed , Fuel Con sump ti on , Range Gross weight

kg lb

2,700 5,952

3,000 6,614

3,300 7,275

3,585 7,904

3,650 8,047

• Maximum speed (VNE), at IAS

km/h kts

278 150

278 150

269 145

267 144

265 143

265 143

• Fast cruise speed (VH), at TAS

km/h kts

253 137

251 135

247 133

242 131

241 130

240 129

• Fuel consumption at fast cruise speed

kg/h lb/h

269 593

269 593

269 593

269 593

269 593

269 593

• Best range speed (VBR), at TAS

km/h kts

241 130

241 130

241 130

241 130

241 130

240 129

• Fuel consumption at best range speed

kg/h lb/h

252 557

256 564

261 575

266 587

269 593

269 593

• Fuel consumption at 70 KIAS

kg/h lb/h

182 402

189 416

196 432

203 448

205 452

207 456

145 D-2 18.101.01 E

3,700 8,157

63


Technical Data

Gross weight

• Maximum range at best range speed (no reserve) • Standard fuel tank (723.0 kg) • Standard fuel tank and long range fuel tank (898.0 kg) • Maximum endurance at best endurance speed = 70 KIAS (no reserve) • Standard fuel tank (723.0 kg) • Standard fuel tank and long range fuel tank (898.0 kg)

kg lb

2,700 5,952

3,000 6,614

3,300 7,275

3,585 7,904

3,650 8,047

km NM km NM

659 356

677 366 847 457

668 360 835 451

656 354 822 444

654 353 819 442

651 352 816 441

h:min

3:53

3:55

3:47

3:40

3:38

3:36

4:56

4:46

4:37

4:35

4:33

h:min

3,700 8,157

Al l En gi ne Operativ e (AEO) - Speed, Fuel Consu mpti on , Rang e at 5,000 ft Gross weight

kg lb

2,700 5,952

3,000 6,614

3,300 7,275

3,585 7,904

3,650 8,047

• Maximum speed (VNE), at IAS

km/h kts

278 150

274 148

261 141

250 135

244 132

244 132

• Fast cruise speed (VH), at TAS

km/h kts

267 144

263 142

257 139

250 135

248 134

248 134

• Fuel consumption at fast cruise speed

kg/h lb/h

254 560

254 560

254 560

253 558

253 558

253 558

• Best range speed (VBR), at TAS

km/h kts

247 134

245 132

241 130

241 130

241 130

241 130

• Fuel consumption at best range speed

kg/h lb/h

230 507

232 511

235 518

242 534

244 538

246 542

• Fuel consumption at 70 KIAS

kg/h lb/h

165 364

172 379

181 399

190 419

195 430

195 430

km NM km NM

750 405

768 415 960 519

752 406 942 509

733 396 920 497

728 393 915 494

725 392 911 492

h:min

4:18

4:19

4:09

3:58

3:56

3:54

5:26

5:14

5:01

4:58

4:55

• Maximum range at best range speed (no reserve) • Standard fuel tank (723.0 kg) • Standard fuel tank and long range fuel tank (898.0 kg) • Maximum endurance at best endurance speed = 70 KIAS (no reserve) • Standard fuel tank (723.0 kg) • Standard fuel tank and long range fuel tank (898.0 kg)

64

h:min

3,700 8,157

145 D-2 18.101.01 E


Technical Data

One Engin e Inoperative (OEI) - Alt itu de Gross weight

• Service ceiling OEI, MCP (climb reserve 0.5 m/s - 100 ft/min) • ISA • ISA +20°C

kg lb

2,700 5,952

3,000 6,614

3,300 7,275

3,585 7,904

m ft m ft

5,730 18,800 5,260 17,250

4,875 16,000 4,330 14,200

4,100 13,450 3,430 11,250

3,065 10,050 2,590 8,500

3,650 8,047

3,700 8,157

2,715 2,375 8,900 7,800 2,410 2,180 7,900 7,150

One Engine Inoperativ e (OEI) - Maxim um Gros s Mass

Max. Gross Weight SL, ISA

Max. Gross Weight SL, ISA +20°C

• Hover OGE (OEI 30 sec-power)

kg lb

3,395 7,485

kg lb

3,350 7,385

• Hover OGE (OEI 2 min-power)

kg lb

3,300 7,275

kg lb

3,260 7,187

• Cat. A, VTOL

kg lb

3,700 8,157

kg lb

3,660 8,069

• Hoist, HEC, clear area

kg lb

3,320 7,319

kg lb

3,270 7,209

• Hoist, HEC, confined area

kg lb

3,300 7,275

kg lb

3,260 7,187

145 D-2 18.101.01 E

65


Technical Data

6.2

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

• Maximum operating altitude • Maximum operating altitude for hover, takeoff and landing • Minimum temperature • Maximum temperature • Category A - Maximum temperature for takeoff from Clear Heliport, SL, gross weight 3,700 kg

66

6,096 m PA 20,000 ft PA 6,096 m PA or DA 20,000 ft PA or DA, whichever is less -45°C ISA +35°C (max. +50°C) +50°C

145 D-2 18.101.01 E


Technical Data

6.3

Performance Charts • Hover In Ground Effect (HIGE, TOP)

6.3-1

• Hover Out of Ground Effect (HOGE, TOP)

6.3-2

• Takeoff Weight, Cat. A, Clear Heliport

6.3-3

• Takeoff Weight, Cat. A, VTOL Surface Level Heliport

6.3-4

• Maximum Cruising Speed, MCP, ISA

6.3-5

• Maximum Rate of Climb, TOP, MTOW (3,700 kg)

6.3-6

• Maximum Rate of Climb, MCP, MTOW (3,700 kg)

6.3-7

• Fuel Consumption (AEO), Diagram 1

6.3-8


6.3-9


6.3-10

• Payload Range (AEO)

6.3-11

145 D-2 18.101.01 E

67


Technical Data

6.3-1 Hover In Ground Effect (HIGE, TOP)

Figure 6.1: Hover In Ground Effect (HIGE, TOP)

68

145 D-2 18.101.01 E


Technical Data

6.3-2 Hover Out of Ground Effect (HOGE, TOP)

Figure 6.2: Hover Out of Ground Effect (HOGE, TOP)

145 D-2 18.101.01 E

69


Technical Data

6.3-3 Takeoff Weight, Cat. A, Clear Helipo rt

Figure 6.3: Takeoff Weight, Cat. A, Clear Heliport

70

145 D-2 18.101.01 E


Technical Data

6.3-4 Takeoff Weight, Cat. A, VTOL Surface Level Heliport

Figure 6.4: Takeoff Weight, Cat. A, VTOL Surface Level Heliport

145 D-2 18.101.01 E

71


Technical Data

6.3-5 Maxim um Cruis ing Speed, MCP, ISA

Figure 6.5: Maximum Cruising Speed, MCP, ISA

72

145 D-2 18.101.01 E


Technical Data

6.3-6 Maximu m Rate of Climb, TOP, MTOW (3,700 kg)

Figure 6.6: Maximum Rate of Climb, TOP, MTOW (3,700 kg)

145 D-2 18.101.01 E

73


Technical Data

6.3-7 Maximum Rate of Cl imb, MCP, MTOW (3,700 kg)

Figure 6.7: Maximum Rate of Climb, MCP, MTOW (3,700 kg)

74

145 D-2 18.101.01 E


Technical Data

6.3-8 Fuel Con sum pti on (AEO), Diagram 1

Figure 6.8: Fuel Consumption (AEO) - diagram 1 145 D-2 18.101.01 E

75


Technical Data

6.3-9 Fuel Cons umpt ion (AEO), Diagram 2

Figure 6.9: Fuel Consumption (AEO) - diagram 2

76

145 D-2 18.101.01 E


Technical Data

6.3-10 Fuel Cons umpt ion (AEO), Diagram 3

Figure 6.10: Fuel Consumption (AEO) - diagram 3

145 D-2 18.101.01 E

77


Technical Data

6.3-11 Paylo ad Range (AEO)

Figure 6.11: Payload Range (AEO)

78

145 D-2 18.101.01 E


Technical Data

7

Serv ic e an d Su pp ort In fo rm at io n

7.1

Assets Proven reliabilit y and availability based on experience At Airbus, supporting customer's helicopter operations with the highest level of excellence is our priority. We have developed a strong reputation worldwide for being fully committed to providing customers with mission-efficient aircraft combining both high aircraft availability rate and cost-effective services solutions. This high level of performance has been our main target throughout the years, and therefore Airbus 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.

To ensure the most efficient support of these helicopters whatever the location in the world, Airbus offers: • A worldwide service network of 29 Customers Centers, more than 100 distributors, representatives, training centers, maintenance, repair and overhaul facilities • 8 logistics hubs, central & regional inventories (France, Germany, UK, Hong Kong, Australia, Mexico, Brazil and the USA) • 3 Customer Support Centers in Europe, Asia and the USA offering 24/7 customer assistance, 7 days a week, 365 days a year • A comprehensive service offer HCare®: a wide array of services solutions to meet all operators' needs in terms of material management, helicopter maintenance, technical support, training & flight operations and connected services - at Airbus' facilities or at customer's location.

145 D-2 18.101.01 E

79


Technical Data

7.2

H145 Inspection Programs The maintenance program specifies the intervals between maintenance operations that are recommended by Airbus, 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. For the performance of scheduled and unscheduled maintenance, Airbus has classified the maintenance tasks by the following three maintenance levels:

Organizational L evel (O - Level) This Organizational Level (O-Level) comprises tasks such as the daily servicing, pre-flight checks, visual inspections for condition, replacement of modular components and simple repairs. This work can be performed by trained helicopter mechanics with standard tools only (no special tools necessary).

Intermediate Level (I - Level) This Intermediate Level (I-Level) comprises tasks such as smaller repairs ON / OFF helicopter, periodical inspections and replacement of modular components as well as modifications. This work can be performed by trained and experienced mechanics and may require the usage of special tools and / or test equipment.

Depot Level (D - Level) The Depot Level (D-Level) comprises tasks such as repairs OFF helicopter, overhaul of major components and heavy airframe repair. This work can be performed by Original Equipment Manufacturer (OEM), authorized repair centers or Airbus and requires the usage of special overhaul and repair tools, as well as test benches (if required) according to repair manuals or instructions. The following table provides an overview of all inspections. Scheduled inspections with shorter time intervals are included in those with longer time intervals. Scheduled airframe inspection

Maintenance level

Estimated man hour

Pre-flight check

O - Level

Pilot task

12-month inspection

I - Level

29

Intermediate inspection every 400 Fh

O - Level

33

Periodical inspection every 800 Fh or 3 years

I - Level

143

Note: All the "hands-on" aircraft values mentioned here above are gi ven on the basis of a 20,000 FH 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 mean man hours are without incoming flight, work preparation, reworking, servicing, Service Bulletin (SB) implementation and unscheduled maintenance.

80

145 D-2 18.101.01 E


Technical Data

Engine Inspection Programs The following table provides an overview of all engine inspections. Each inspection has to be performed for the respective time frame. Safran Helicopter Engin es Arriel 2E scheduled inspection

Maintenance level

Estimated mean man hour

Daily checks

O - Level

Pilot Task

Checks before the first flight

O - Level

0.033

Checks between two flights

O - Level

0.017

Safran Helicopter Engi nes periodic inspections

Mai nt en an ce l evel

Est imat ed man h ou r

O - Level

9.55

800 Fh

Note: For further details on the engine inspections and the respective D-Level maintenance please refer to the applicable engine maintenance manual.

145 D-2 18.101.01 E

81


Technical Data

7.3

Mai n Co mp on en ts

7.3.1 Airframe Main Components Time Between Overhaul (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. The given time limit may be exceeded by 3 % of the respective interval. All subcomponents may have a Service Life Limit (SLL), rated above the Time Between Overhaul (TBO) limit. Ai rf ram e mai n c om po nen ts

Cartridge of fuel pump

TBO as per MSM Rev. 10 fro m 2017.05.02

5,000 Fh

Main transmission

3,600 Fh or 18 yearsa

Tail gear box

5,000 Fh or 18 yearsa

Longitudinal actuator

7,500 Fh

Lateral actuator

7,500 Fh

Collective actuator

7,500 Fh

Fenestron actuator

3,000 Fh

a. First limit reached. Note: Non exhaustive list.

Time Change Item (TCI) or Service Li fe Lim it (SLL) A Time Change Item (TCI) is a component, which has an airworthiness Service Life Limit (SLL). The affected component must be removed from service, when it reaches the limit indicated. Ai rf ram e mai n c om po nen ts

TCI or SL L as per Rev. 10 fro m 2017.05.02

Main rotor blade

25,000 Fh

Main rotor shaft

30,000 Fh

Freewheel clutch

3,600 Fh

Note: Non exhaustive list.

82

145 D-2 18.101.01 E


Technical Data

7.3.2 Engine Main Components Time Between Overhaul (TBO) The initial Time Between Overhaul (TBO) values are applicable to the engines / modules / accessories and are summarized in the tables below. Saf ran Heli cop ter Eng in es Arri el 2E overhauls

TB O as per En gin e MM rev 2016

Accessory gearbox (Module 01)

4,000 Fha or 15 yearsb

Axial compressor (Module 02)


Gas generator (Module 03)


Power turbine (Module 04)


Reduction gearbox (Module 05)


a. First limit reached b. TBO extension on-going, to be extended to 6,000 Fh

Service Lif e Limit (SLL) Certain components of the engine, of which failures could cause a hazardous effect to the engine or its regulation, have service life limit expressed in cycles (reference flight cycle). The limited service life to which this term refers is the number of cycles that a critical part can run before having to be withdrawn from service. Saf ran Hel ico pt er En gi nes A rri el 2E c om po nen ts

SL L as p er en gi ne MM r ev 2016

Axial wheel

22,000 cycles

Centrifugal impeller

22,000 cycles

Injection wheel

8,000 cycles

HP turbine disc

17,000 cycles

Power turbine disk

22,000 cycles

Note: Cycles are calculated automatically by the Engine Electronic Control Unit. Average experienced rate is about 0.5 cycles/Fh.

145 D-2 18.101.01 E

83


Technical Data

7.4

HCare - Material Management Airbus offers its clients a comprehensive choice of material management services to ensure availability and costs control. This array of services ranges from basic Original Equipment Manufacturer (OEM) spare parts supply, repair and overhaul services up to comprehensive, "by-the-hour" support programs. The different services are tailored for different user profiles and demands, such as customers: • with a high flying hours level • with a low flying hours level • looking for immediate component availability • wishing optimal budget control To respond to the different customers' demands, Airbus offers the following services:

HCare Easy: Open & seamless access t o all cus tomers under catalogue condit ions • • • •

Easy Easy Easy Easy

Part for spare parts, components repair & overhaul and second hand parts Rental for tools and Ground Support Equipment (GSE) Repair for secured turn-around-times on components Exchange for secured availability on components

HCare Smart: Performance commitment, budget cont rol, suit ed to cus tomers' needs • • • •

Repair By-the-Hour (RBH) Exchange By-the-Hour (EBH) Parts By-the-Hour (PBH) Full By-the-Hour (FBH)

HCare Infinite: Full availability commit ment, all-inclusi ve turnkey solut ions • Fleet availability Note: Specific mission equipment e.g. STC´s might be excluded from above services. Note: Local authority regulations may have an impact on the above described material management services.

Airbus would be pleased to propose further extensive services adapted to specific mission and customer expectations, such as stock and maintenance management.

7.4.1 HCare Easy HCare Easy is a classical way of material support. The material is delivered on demand when needed. It comprises spare parts, components repair & overhaul, second-hand parts, standard exchange and tool/GSE rental. The requested level of operational availability determines provisioning part quantities and therefore the required investment. With this support concept the customers bear the responsibility to monitor repairs; manage obsolescence and procure the right mix and quantity of components and spare parts to ensure availability when required. For specific lists of part numbers, Airbus has invested in dedicated stocks, and offers through Easy Repair & Easy Exchange services, secured turn-around-times, or secured parts availability for standard exchange.

84

145 D-2 18.101.01 E


Technical Data

7.4.2 HCare Smart Repair By-th e-Hour (RBH) The RBH service offers guaranteed repair & overhaul turn-around-times as well as guaranteed prices. This service enables the customer to best size its own inventory of repairable parts, and better schedule its helicopter maintenance while keeping property of its material. The price for this service is calculated per flight hour, thus enabling the customer to spread and predict component scheduled and unscheduled maintenance expenses. The RBH service includes component unscheduled third level repairs (Depot Level maintenance), component scheduled overhauls, life-limited part replacement as well as mandatory modification kits (to the extent covered by the RBH contract). This service is available for dynamic components, blades, basic and optional equipment (covered optional equipment list to be defined with the customer).

Exchange By -the-Hour (EBH) With the Exchange-By-the-Hour (EBH) service, Airbus offers the customer an immediate part replacement, and a controlled budget for unscheduled maintenance while remaining responsible for the scheduled events (overhaul, life limited parts replacement). Price for this service is calculated per flight hour. The EBH service includes component unscheduled third level (Depot Level maintenance) repairs and guaranteed parts delivery within 24 hours FCA (Incoterms 2010) through Standard Exchange based on a dedicated inventory. This service is available for dynamic components, blades, basic and optional equipment (covered optional equipment list to be defined with the customer).

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 for both scheduled and unscheduled events, reduced inventory and minimized helicopter downtime. This service is intended for customers looking for optimized cost control and high level of aircraft readiness. Price for this service is calculated per flight hour. The PBH service includes component unscheduled third level (Depot Level maintenance) repairs; component scheduled overhauls as well as Life Limited Part replacement. Parts delivery is guaranteed within 24 hours FCA (Incoterms 2010) t hrough Standard Exchange based on dedicated inventory. This service is available for dynamic components, blades, basic and optional equipment (covered optional equipment list to be defined with the customer).

Full-By-th e-Hour (FBH) The Full By-the-Hour (FBH) service is an extension of the PBH service including the supply of nonrepairable parts such as consumables and hardware. This service is intended for customers looking for total cost control and high level of aircraft readiness. Price for this service is calculated per flight hour.

145 D-2 18.101.01 E

85


Technical Data

7.4.3 HCare Infinite The HCare Infinite program provides customers a fleet availability commitment from Airbus. It is a turnkey solution, adapted to various customers' needs, enabling them to focus on flights while Airbus takes care of supporting the fleet. The program comprises material support, logistics management and technical services. It can be extended to helicopter maintenance and airworthiness management. Price for this service is usually calculated per flight hour.

7.4.4 Complementary Initial Provisioning of Spare Parts and Tools Within that range, Airbus provides a customized initial provisioning package. It includes spare parts, tools, test equipment, etc. to sustain helicopter operations for a defined initial period of time. The dimensioning of the package is tailored according to the number of helicopters, operational bases, flight hours per year and requested availability.

7.4.5 Logistics Assistance Upon request, Airbus can propose an on-site logistics assistance through a Logistics Field Representative (LFR) detached at customer premises or near the operational base, to optimize logistics flows back and forth. Thanks to unrivalled knowledge of internal processes and logistics tools / network, the LFR is the privileged interface between the customer and Airbus. The LFR is able to assist the customer on material and inventory management, logistics forecasting, order administration and will report on the logistics activities.

7.4.6 Airbus Aircraft-On-Ground (AOG) Service Airbus provides a twenty four hours a day/seven days a week and three hundred and sixty five days per year (24/7/365) AOG service to guarantee an efficient service and respond quickly to any AOG situation. An Aircraft-On-Ground (AOG) service is available for spare orders. The order placed by the customer shall cover an actual failure (and not a scheduled maintenance shortage) and may consist of up to 3 items per grounded aircraft listed in the Illustrated Parts Catalogue (IPC), except main assemblies, raw materials, ingredients and hazardous material. In the case of direct part availability, the parts will be immediately delivered under CIP (Incoterms 2010) conditions to t he nearest international airport with delivery times dependent on the region and export license requirements (normally 48 to 72 hours). The AOG Department is responsible for answering to the following customer requests 24/7/365: • 1st level troubleshooting and diagnosis assistance • Part ordering with immediate information on part availability • Part delivery, delivery of repair solution (even temporary) or any possible service to put helicopter back to flight line.

86

145 D-2 18.101.01 E


Technical Data

7.5

Engine Service and Support Programs Always careful to maximize the efficiency of your operations and reduce your costs, Safran Helicopter Engines, the engine manufacturer has developed and improved its service offering. Safran Helicopter Engines puts at customers' disposal 32 Repair Centers across the globe, supplemented by several new factory-authorized service facilities strategically located near customer's operations. Safran Helicopter Engines range of services covers: • Classical Repair and Overhaul • Standard Exchange • AOG services • By-the-Hour services Within the By-the-Hour coverage, Safran Helicopter Engines developed specific maintenance packages, as summarized hereafter.

Safran Helic opt er Engines Global Suppo rt Package (GSP) For military and parapublic missions, the aircraft must be operational at any time. Safran Helicopter Engines GSP service includes an extensive range of options that can be tailored to customers' needs. To bring more reliability, safety and availability while controlling budget and cost, Safran Helicopter Engines proposes to forge a real partnership through four service packages: • Equipment availability and stock optimization: To control key parameters to reach results on stock optimization and availability equipment. • Up to Depot Level maintenance (from Level 2 to 4): To manage engine maintenance from level 2 to 4, with flying hours invoicing and guaranteed prices. • Financial solutions: To bring visibility and help to finance operational needs. • Support of "O" Level maintenance: To facilitate "O" Level maintenance execution.

Safran Helicopter Engines Support By-the-Hour (SBH) Safran Helicopter Engines SBH is a comprehensive service for civilian missions, providing financial and operational coverage for engine support. • To customers choice, it can cover scheduled as well as unscheduled events, limiting exposure to unexpected expenses. • Customer "pay as customer flies": SBH provides a fixed cost per engine flight hour. It is directly linked to customers' flight activity. One SBH, many solutions: Safran Helicopter Engines SBH is one single name and concept offering flexible and standard combinations between 4 dimensions: • Coverage: scheduled and/or unscheduled events, with flexibility on some engine components. Complete engine or modular maintenance. • Availability: pool access option with standard exchange or rental • Logistics: a choice of transport solutions • Finance: different payment terms, contract duration

145 D-2 18.101.01 E

87


Technical Data

SBH was made to be tailored to customer exact needs. Safran Helicopter Engines SBH benefits: • Predictability: Control of budget and smooth of engine maintenance costs: expenses are clear and predictable • Flexibility: Safran Helicopter Engines SBH offers total modularity, to cover customers' exact needs • Insurance: scheduled and/or unscheduled coverage, with risks partially transferred to Safran Helicopter Engines • Availability: effective replacement solutions including Standard Exchange, available through Safran Helicopter Engines' worldwide pool • Win-win: contractual commitments on hourly rates and lead times • Visibility: clear view of combinations and options

Safran Helicopter Engines Operator Online Support (tools) Customers' feedback has also allowed Safran Helicopter Engines to greatly improve tools, a website dedicated to operator support. Safran Helicopter Engines Operator On Line Support is a fully interactive website developed and programmed specifically for customer support needs. A portion of the site is available to anyone seeking information regarding customer support services and activities. The other portion of the site is exclusively available to clients, providing a wealth of information and services, such as: • Technical Publications • Direct communication access with the needed resources • On-line training • A clear overview of all other Safran Helicopter Engines services such as second hand engines and warranty • ... and much more to serve customers

88

145 D-2 18.101.01 E


Technical Data

7.6

HCare - Helicopter Maintenance

7.6.1 Aircr aft Maintenance, Repair & Overhaul (MRO) Airbus proposes a complete range of industry-leading Maintenance, Repair & Overhaul (MRO) solutions such as: inspection, repair and overhaul capabilities for the full range of Airbus product range, with optimized turn-around-times and cost-efficiency. Approved by the most stringent airworthiness authorities in the world, Airbus industrial facilities ensure the highest quality for the maintenance and repair actions of customers' f leet. Works are performed by our teams of specialized and duly qualified technicians which technicity has been built on long and diverse field experience on the worldwide fleet. Airbus can perform the work within its facilities around the world or at customer premises.

7.6.2 On-Site Assistance When requested, Airbus teams of skilled field service technicians provide the customer with worldclass support and enhanced services for aircraft maintenance, repairs and retrofits at customer's premises. As part of this service Airbus technicians will bring the required parts and tools to carry out the maintenance, repair and upgrade tasks on site.

7.6.3 Upgrades Airbus proposes tailored solutions to increase customers' helicopter overall performance and reduce its maintenance cost, contributing to harmonized fleet or role/mission change, the better to be prepared for missions. Upgrades maintain aircraft at the latest version, benefitting from innovations and advanced technology, perfectly adapted to customers' aircraft configuration and defined by Airbus experienced design office teams. The portfolio of AH Standard Upgrades is available on customer portal Keycopter, allowing direct order of kits or request of customized quotation. The set of upgrades is regularly updated. This portfolio proposes number of equipment that may be installed on helicopters after delivery from Airbus Helicopters in order to fulfil specific operational needs or aircraft upgrades. These equipment are either designed and certified by Airbus Helicopters as SB (Service Bulletin) or by Airbus Helicopters customer centers or third parties as STC's (Supplementary Type Certificate). Please note that some constraints may exist between optional equipment. Technical confirmation by an Airbus Helicopters sales representative is recommended before submitting any purchase order.

145 D-2 18.101.01 E

89


Technical Data

7.7

HCare - Technical Support

7.7.1 Technical Assistance An Airbus Technical Representative can be detached at customers' base to perform On-the-Job Training and ensure an efficient and safe start of the operations. The on-site Technical Representative covers mainly the following activities: • Daily relationship interface with the customer • Aircraft assistance (explanation for usage of special maintenance tools and equipment) • Troubleshooting (assistance in solving technical events and management of the process from the diagnosis up to the solution) • Interface with Airbus mother company (engineering support) • Contribution to fleet technical knowledge management • Local day-to-day recommendations to optimize the customer maintenance efficiency • Safety (analysis of events in case of minor or major incidents to identify airworthiness impact)

7.7.2 Technical Expertise 24/7 Airbus will provide technical knowledge dedicated to your helicopters, aimed at supporting the safe and reliable operations of the aircraft. A team of highly skilled engineers in close and daily relation with design office is committed to answer any t echnical 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 Airbus. Any technical question can be raised 24 hours/7 days, through our toll free number or our Keycopter website for organizations using the internet (eRequests function).

7.7.3 Continuing Airworthiness Management (CAM) Services Airbus consulting & training services improve operational performance of customers' fleet. Such services can be complemented by CAM services offering diagnosis up to full implementation of a full airworthiness follow-up organization.

7.7.4 eTechPub Airbus provides the technical publications required for safe operations and cost-effective maintenance. Airbus technical publications are available on Keycopter® portal within eTechpub service. An interactive electronic browser, O.R.I.O.N, is available. O.R.I.O.N. includes the maintenance and identification information and contains at minimum. • Aircraft Maintenance Manual (AMM), • System Description Section (SDS), • Master Servicing Manual (MSM), • Illustrated Parts Catalog (IPC), • Wiring Diagram Manual (WDM), • Structure Repair Manual (SRM), • Standard Practices Manual (SPM/MTC). The technical publications are available in English. They include the latest information and are regularly updated.

90

145 D-2 18.101.01 E


Technical Data

Keycopter / eTechpub also provide access to the List Of Applicable Publications / Status Revision Documentation (LOAP/SRD), Flight Manual (FLM), Pilot's Check List (PCL) and Master Minimum Equipment List (MMEL). Along with Keycopter / eTechpub, Airbus provides a hard copy of • Flight Manual, • Master Minimum Equipment List (MMEL), • Pilots-Checklist, • Logbooks, • Historical Record. The delivery of hard copies may be cancelled without further notice in case of changes to the legal requirements. As chargeable option, the technical publications are also available on PDF format on Keycopter portal. When online solutions do not fit to user constraints, physical means may be proposed as chargeable options: • O.R.I.O.N. light on USB Key, same content than O.R.I.O.N on line but with a reduced set of functions • O.R.I.O.N. full on USB Key, same content than O.R.I.O.N on line but as local network solutions (full functionalities) • Hard copies Selected Component Maintenance Manuals (CMM) are available on PDF format: • On Keycopter / eTechpub as Online Component Maintenance Manual (OCMM), • On USB key as Electronic Component Maintenance Manual (ECMM). The engine documentation is provided by the engine manufacturer.

7.7.5 Technical Information Publication on Internet (T.I.P.I.) The Technical Information Publication on Internet (T.I.P.I.) website is entirely dedicated to provide a real-time issuing service for the following publications: • Service Bulletin (SB), Alert Service Bulletin (ASB), Emergency Alert Service Bulletin (EASB), Service Letter (SL), Information Notice (IN), Safety Information Notice (SIN), Technical Information Letter (TIL), Flight Operations Briefing Note (FOBN), • Master Minimum Equipment List (MMEL), • Technical Improvement Proposal (TIP), • Revisions of Flight Manual (FLM). The T.I.P.I. application is now also available for tablets and smartphones. The T.I.P.I. application forsmartphones and tablets can be downloaded free of charge by following the link: http://www.airbushelicopters.com/techpub/ or in a mobile equipment application stores (Apple store, Play Store -formerly Android Market, etc.).

Main Features • Each time one of the above listed publications is issued, the customer is automatically informed by an e-mail. • A small summary, already included in the e-mail, helps the customer to quickly understand the subject. • Small icons allow the customer to immediately identify the type of information received. • The download of the publication in PDF format is possible after logging on the T.I.P.I. website. • A keyword search tool is provided (aircraft family, type of publication, date of edition, etc.). • Address: http://www.airbushelicopters.com/techpub/ The publications are available in English.

145 D-2 18.101.01 E

91


Technical Data

7.8

HCare - Training & Flight Ops Training With over 50 years of experience, the Airbus helicopter training centers provide the world's leading helicopter training for pilots and t echnicians, whether civilian or military. Since 2011, a completely new blended learning process based on interactive learning with the latest technology for theoretical and practical instruction is implemented. The instruction team is composed of experts in their fields with the utmost operational experience and knowledge. Although a lot of things have changed in the past 50 years Airbus major goal remains unchanged: to stand up to customers' expectations and to contribute decisively to flight safety. The course catalogue is designed to cover the full range of customers' training needs. Nevertheless, Airbus can also provide customers' organization with the most effective training solution tailored to customers' demand. The high quality of Airbus training courses is assured by a very strict internal quality system and regular audits by national authorities (EASA, FAA, DGAC, LBA, CAA, CAAC…). The main training centers are certified to issue certificates according to EASA Part 147 and Part FCL. Airbus has set up a network of 24 helicopter training centers and 23 Full Flight Simulators (FFS) all over the world. 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) or instructor lead presentation. For detailed information refer to: http://www.helicopters.airbus.com/website/en/ref/Training-&-Flight-Ops_72.html

AIRB US HELICOPTERS NETWORK

Figure 7.1: HCare - Training Centers

92

145 D-2 18.101.01 E


Technical Data

Basic H145 training co urse

COURSE TYPE

COURSE REFERENCE

THEORETICAL INSTRUCTION

FLIGHT INSTRUCTION

Pilots

Type Rating VFR

3 weeks

10 Fh

COURSE TYPE

COURSE REFERENCE

THEORETI CA L A ND PR ACTICA L I NSTRUCTION

Airframe Type Rating B1.3

5 weeks

Avionic Type Rating B2

4 weeks

Technicians

Note: Training duration and content are given as information and depend on pilot or technician qualification or experience and the configuration of the aircraft. Complementary courses may be required.

For detailed information refer to: www.airbushelicopters.com/website/en/ref/Training-&-Flight-Ops_72.html

Engine Training Courses Training courses dedicated to Engine Maintenance are organized by Safran Helicopter Engines Academy and approved centers the world over. Up-to-date course calendars, on-line tests and e-learning modules are also available on the Safran Helicopter Engines Operator On-Line Support (tools web site).

145 D-2 18.101.01 E

93


Technical Data

7.9

Flight Operations Services This set of services activities aims at answering all operational related constraints and issues met by pilots and operations departments.

7.9.1 Pilot Assistance (on site) Through on-site pilot assistance, Airbus provides customers' pilots complementary knowledge on their 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.

7.9.2 Crew Help Desk (on-line support) The Crew Help Desk provides answers to queries relative to best knowledge and operation of the helicopter among e.g. regulations, aircrew publications, aircraft limitations, performance, procedures/ operations and systems. The Crew Help Desk support is ensured through the worldwide Airbus network. This service is provided free of charge. Any question can be raised 24/7 through our toll f ree number or our Keycopter website for organizations using the internet (eRequest function).

7.9.3 Pilots Check-list - PCL - (Operational Documentation) The PCL presents abbreviated standard operating procedures based on the helicopter flight manual (FLM) or the Flight Crew Operating Manual (FCOM). The PCL does not replace nor supersede the current FLM/FCOM. It is updated in accordance with the corresponding FLM/FCOM revisions when applicable. The PCL is provided in PDF/paper format, in English language.

7.9.4 Flight Ops Briefing Note - FOBN - (Operational Documentation) 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.

7.9.5 Flight Crew Operating Manual - FCOM - (Operational Documentation) The FCOM is issued as a guideline for operators to develop their own Standard Operating Procedures in accordance with applicable requirements. It is designed for a specific model, type of operation and configuration. In any case, the approved Flight Manual remains the only official document with regards to certification authorities.

7.9.6 Safety Management System (SMS) 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. Airbus Helicopters International Services (AHIS) consulting division can support the introduction of SMS in Customer's organization. AHIS consulting experts have extensive operational and technical knowledge and can provide practical solutions tailored to customer's needs. 94

145 D-2 18.101.01 E


Technical Data

7.10 HCare - Connected Services Two families of essential service package (available online or locally) accessible through Keycopter website and/or the e-Apps Apple store:

7.10.1 HCare Fligh t For efficient flight preparation • Flight Planner: Airbus all-in-one portable Electronic Flight Bag for mission planning on ground and mission execution in flight, running on rugged windows tablet. • Flight Perfo: separate iOS app for Performance computation • Flight Balance: separate iOS app for Weight and Balance computation

7.10.2 HCare Fleet More dedicated to support maintenance operations and for a smarter f leet management. • Fleet Keeper ® application: The full e-solution by Airbus for your Technical Log Book linking Flight Operations, Airworthiness and Maintenance Crew (mobile and Web-based). • Monitor & control fleet status in real-time • Record flight reports • Manage technical events • Envision nGen: Airbus trusted solution for aviation management. Powerful all-inclusive software developed for operators in need of a complete Maintenance Information System. This tool is customizable across various modules, and covers any activity related to helicopter operations.

7.10.3 HCare for Helioni x With eAvionics Airbus proposes a set of system and software services: System and conf iguratio n management services: • Support, services or tools related to the system & software configuration management • The configuration management of the loadable/configurable equipment is fully managed in the technical documentation (Technical Logbook, IPC, SB). Loading and log istic services: • Spare & repair (preloaded equipment) • Customer software loading package (loading tool, documentation, training, software distribution). The loading tool provides customers with autonomy for loading/configuring their equipment. • Equipment loading service in Airbus network • Equipment loading by Airbus at customer premises Software maintenance services: • Airbus proposes software maintenance services consisting in regular maintenance releases. Failure Management (Diagnosis & eDynamic Troubleshoot ing)

An online tool accessible via Keycopter which shall help you solve any observed issues with the H/C in a quick and efficient manner. The failure codes recorded within Helionix are available via the online Diagnosis Report and/or Helionix Maintenance Page. The eDynamic Troubleshooting helps to isolate the root cause, either by using the failure codes, or by looking for symptoms. Prerequisite to use the diagnosis report is a data exchange with Airbus via the MGS. Full offline eDynamic Troubleshooting: for customers not able to share their aircraft data via the MGS and /or having no web access, an offline version of the eDynamic Troubleshooting is available on request.

145 D-2 18.101.01 E

95


Technical Data

Aer od ata

This service provides databases and tools for the following enhanced awareness functions of Helionix hosted in the Multi-Functional Display (MFD): • Helicopter Terrain Awareness and Warning System (H-TAWS) • Moving map (DMAP) • Synthetic Vision System (SVS)

96

145 D-2 18.101.01 E


Technical Data

8

Abbreviations Abb rev iat io n

Meani ng

AAT

Air Ambulance Technologies

AC

Alternating Current

ACS

Airconditioning System

ACU

Audio Control Unit

ADELT

Automatic Deployable Emergency Locator Transmitter

ADF

Automatic Direction Finder

ADS

Aeronautical Data Service

ADS-B

Automatic Dependent Surveillance - Broadcast

AEL

Aerolite

AEO

All Engines Operative

AFCS

Automatic Flight Control System

AFT

Aft

AGL

Altitude above Ground Level

AHIS

Airbus Helicopters International Services

AHDL

Airbus Helicopters Data Loader

AHRS

Attitude and Heading Reference Sensors

AM

Amplitude Modulation

AMC

Aircraft Management Computer

AMLCD

Active Matrix Liquid Crystal Display

AMM

Aircraft Maintenance Manual

ANR

Active Noise Reduction

AOG

Aircraft On Ground

ASB

Alert Service Bulletin

BAE

British Aerospace Electronic

BFE

Buyer Furnished Equipment

CAA

Civil Aviation Authority

CAAC

Civil Aviation Administration of China

CAI

Computer Aided Instruction

Cat. A

Category A

CBT

Computer Based Training

CCP

Cockpit Control Panel

CECG

Corrosion and Erosion Control Guide

CIP

Carriage Insurance Paid

CMM

Component Maintenance Manual

COM

Communication

CVFDR

Cockpit Voice and Flight Data Recorder

DA

Density Altitude

DC

Direct Current

DGAC

Direction générale de l'aviation civile

DMAP

Digital MAP

DME

Distance Measuring Equipment

DP

Dual Pilot

DTD

Data Transfer Device

145 D-2 18.101.01 E

97


Technical Data

98

Ab br evi ati on

Meani ng

DTU

Data Transfer Unit

DVCS

Digital Voice Control System

EASA

European Aviation Safety Agency

EASB

Emergency Alert Service Bulletin

EBH

Exchange By-the-Hour

ECMM

Electronic Component Maintenance Manual

ECS

Environmental Control System

ELT

Emergency Locator Transmitter

EMS

Emergency Medical Service

EOS

Electro Optical System

EPNdB

Effective Perceived Noise decibels

FAA

Federal Aviation Administration

FADEC

Full Authority Digital Engine Control

FAR

Federal Aviation Regulations

FBH

Full By-the-Hour

FCL

Flight Crew Licensing

FCA

Free Carrier

FCOM

Flight Crew Operating Manual

FDCR

Flight Data Continuous Recorder

FDS

Flight Display Subsystem

FFS

Full Flight Simulator

FLI

First Limit Indicator

FLM

Flight Manual

FMS

Flight Management System

FND

Flight and Navigation Display

FNPT

Flight Navigation Procedure Trainer

FWD

Forward

GPS

Global Positioning System

GSE

Ground Support Equipment

GSM

Global Systems Mobile

GSP

Global Support Package

H/C

Helicopter

HD

High Definition

HDLL

High Definition Low Light

HEC

Human External Cargo

HEELS

Helicopter Emergency Egress Lighting System

HEMS

Helicopter Emergency Medical Service

HF

High Frequency

HFDM

Helicopter Flight Data Monitoring

HICAMS

Helicopter Intensive Care Medical Service

HIGE

Hover In Ground Effect

HMI

Human Machine Interface

HMS

Health Monitoring System

HOGE

Hover Out of Ground Effect

HP

High Pressure

HPPE

High Performance Polyethylen

145 D-2 18.101.01 E


Technical Data

Abb rev iat io n

Meani ng

H-TAWS

Helicopter Terrain Awareness and Warning System

IAS

Indicated Airspeed

IBF

Inlet Barrier Filter

IC

Inter Communication

ICAO

International Civil Aviation Organization

IESI

Integrated Electronic Standby Instrument

IFR

Instrument Flight Rules

ILS

Instrument Landing System

IMC

Instrument Meteorological Conditions

IMU

Inertial Measurement Unit

IN

Information Notice

IPC

Illustrated Parts Catalog

IR

Infra Red

ISA

International Standard Atmosphere

ITAR

International Traffic in Arms Regulations

KCAS

Knots Calibrated Airspeed

KIAS

Knots Indicated Airspeed

KTAS

Knots True Airspeed

LARS

Lightweight Aircraft Recording System

LBA

Luftfahrt Bundesamt

LED

Light Emitting Diode

LFR

Logistics Field Representative

LH

Left Hand

LOAP

List Of Applicable Publication

max.

Maximum

MCP

Maximum Continuous Power

MFD

Multifunction Display

MGS

Maintenance Ground Station

MKR

Marker

MLD

Missile Launch Detector

MMEL

Master Minimum Equipment List

MRO

Maintenance, Repair and Overhaul

MSM

Master Servicing Manual

MTC

Manuel Techniques Courantes

MTOW

Maximum Takeoff Weight

MWIR

Medium-Wave Infra Red

NAV

Navigation

NVG

Night Vision Goggles

NVIS

Night Vision Imaging System

OAT

Outside Air Temperature

OCMM

Online Component Maintenance Manual

OEI

One Engine Inoperative

OEM

Original Equipment Manufacturer

OPS

Operations

PA

Pressure Altitude

PAX

Passenger

145 D-2 18.101.01 E

99


Technical Data

100

Ab br eviat io n

Meani ng

PBH

Parts By the Hour

PC

Personal Computer

PCL

Pilot's Check List

PFD

Primary Flight Display

PGS

Professional Ground Station

PNG

Polycon New Generation

RAMT

Reliability, Availability and Maintainability/Testability

RBH

Repair By the Hour

R/D

Rate of Descent

Ref.

Reference

Rev.

Revision

RH

Right Hand

RIA

Retractable Interface Adapter

RNP

Required Navigation Performance

RPM

Revolutions Per Minute

SAR

Search and Rescue

SB

Service Bulletin

SBAS

Satellite Based Augmentation System

SBH

Support By the Hour

SDS

System Description Section

SIN

Safety Information Notice

SL

Sea Level

SL

Service Letter

SLL

Service Life Limit

SMS

Safety Management System

SPM

Standard Practices Manual

SRD

Status Revision Documentation

SRM

Structure Repair Manual

STANAG

Standardization Agreement

STC

Supplemental Type Certificate

SVS

Synthetic Vision System

SWIR

Short Wave Infra Red

TAM

Three Axis Magnetometers

TAS

Traffic Advisory System

TAS

True Airspeed

TAT

Turn Around Time

TBO

Time Between Overhaul

TCCA

Transport Canada Civil Aviation

TCI

Time Change Item

TIL

Technical Information Letter

TIP

Technical Improvement Proposal

TOP

Takeoff Power

TX

Transmit

UK

United Kingdom

ULM

Ultra Low Maintenance

UMS

Usage Monitoring System 145 D-2 18.101.01 E


Technical Data

Abb rev iat io n

Meani ng

UMTS

Universal Mobile Telecommunications System

US

United States

USA

United States of America

VBR

Best Range Speed

VDC

Volt Direct Current

VH

Fast Horizontal Speed

VFR

Visual Flight Rules

VHF

Very High Frequency

VMMS

Vector Mast Moment System

VMS

Vehicle Monitoring System

VMS

Vehicle Management System

VNE

Never-Exceed Speed

VOR

VHF Omnidirectional Radio Range

VTOL

Vertical Takeoff and Landing

VY

Best Rate of Climb Speed

WDM

Wiring Diagram Manual

145 D-2 18.101.01 E

101


Technical Te chnical Data

Blank

102

145 D-2 18.101.01 E


Technical Data

Manuf Ma nuf acturer´s Notes This document provides general information on the description, specification, weights, dimensions and performance data of helicopters manufactured by Airbus Helicopters and on related services and support. Depending on the exactly selected configuration and/or the respective mission profile, these data may vary. For specific, individual performance data and operating limitations reference shall be made to the approved flight manual and all appropriate documents. The operational or certification regulations, as defined by competent local authorities, may require as compulsory the installation of some of the recommended or further available equipment equipment as listed in this document, with present document however not being meant to be comprehensive in terms of all worldwide operational requirements. The operator shall be responsible to clarify with its respective local authorities that any potential configuration of the helicopter complies with the regulatory requirements for the area of operation and/or type of mission. The Airbus Helicopters product policy aims at continuous product improvements. Therefore Airbus Helicopters reserves the right to make data changes at any time without any notice being given with reference to present issue of this document. The depicted images (i.e. photos, 3D-pictures, general drawings, diagrams or similar) are for illustration purposes only. The facts and figures contained in this document and expressed in good faith shall not constitute any offer from or the acceptance of an offer leading to a contract with Airbus Helicopters. Airbus Helicopters' logo, H145®, EC145®, Fleet keeper ®, Fenestron®, Helionix®, HCare® and Keycopter ® are registered trademarks of Airbus Helicopters.

145 D-2 18.101.01 E

103


Technical Data

Blank

104

145 D-2 18.101.01 E


145_D-2_18.101.01_E_Technical_Data _LQ_

Recommend Documents