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H135 Ahc

TECHDATA

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100% found this document useful (1 vote)

936 views106 pages

H135 Ahc

TECHDATA

Uploaded by

jorge.salvatori

We take content rights seriously. If you suspect this is your content, claim it here.

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Download as PDF, TXT or read online on Scribd

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CORPORATE

HELICOPTERS

ACH135
Technical Data
2018
AC
Technical Data

Contents

1 Foreword...................................................................................................................................................... 3
1.1 Baseline Aircraft Highlights and Main Improvements ........................................................................... 6
2 General Characteristics............................................................................................................................ 15
2.1 Cockpit and Cabin Layouts ................................................................................................................ 15
2.2 Weight................................................................................................................................................. 15
2.3 Power Ratings..................................................................................................................................... 15
2.4 Fuel Capacities ................................................................................................................................... 16
2.5 External Dimensions ........................................................................................................................... 17
2.6 Internal Dimensions ............................................................................................................................ 18
2.7 External Sound Levels ........................................................................................................................ 18
2.8 Touch Down Forces............................................................................................................................ 19
3 Baseline Aircraft Definition...................................................................................................................... 21
4 Mission Configuration .............................................................................................................................. 23
4.1 Stylence®, 5 Passengers Solution Including one Cabinet .................................................................. 25
4.2 Stylence®, 4 Passengers Solution Including one Cabinet and one Multifunctional Box ..................... 31
4.3 Stylence®, 4 Passengers Solution Including two Cabinets................................................................. 37
5 Further Equipment Information ............................................................................................................... 43
5.1 General Available Equipment ............................................................................................................. 43
5.2 Avionics Layout................................................................................................................................... 47
5.3 Antenna Layout................................................................................................................................... 48
5.4 Disclaimers ......................................................................................................................................... 49
6 Main Performance..................................................................................................................................... 51
6.1 Performance Summary Tables ........................................................................................................... 51
6.2 Operating Limitations .......................................................................................................................... 63
6.3 Performance Charts............................................................................................................................ 64
7 Service and Support Information ............................................................................................................ 77
7.1 Assets ................................................................................................................................................. 77
7.2 Inspection Programs ........................................................................................................................... 77
7.3 Main Components Limitations............................................................................................................. 79
7.4 HCare - Material Management ........................................................................................................... 81
7.5 Engine Service and Support Programs............................................................................................... 83
7.6 HCare - Helicopter Maintenance......................................................................................................... 86
7.7 HCare - Technical Support ................................................................................................................. 87
7.8 HCare - Training & Flight Ops............................................................................................................. 89
7.9 Flight Operations Services.................................................................................................................. 91
7.10 HCare - Connected Services ............................................................................................................ 92
8 Abbreviations ............................................................................................................................................ 95

135 T3H/P3H 18.ACH.01 E 1

Preliminary Data
The data provided in this document is under validation. Final confirmation of the data after finalization of flight
test program.

2 135 T3H/P3H 18.ACH.01 E

1 Foreword

Figure 1.1: Example of the ACH135®

Efficient, reliable - and affordable

The ACH135® newly equipped with Helionix® is Airbus‘® 3 ton class light twin Best Seller.
It represents the perfect balance between flight performance, flight safety, reliability and cost of
operations while maintaining its unmatchable agility.
You can expect advantages in every aspect of ownership, from the moment you purchase to the day
you realize its higher residual value.
The ACH135 delivers exceptional power reserves including full class 1 and 2 performances, enhanced
safety margins, best in class payload and the industry benchmark in precision and control.

Quietest in its class

Thanks to its all composite main rotor blades with advanced tip geometry design and Airbus‘
Fenestron® anti-torque system, its sound signature is well below the ultra-stringent ICAO limit causing
least disturbance to residences or businesses in the operating area.

Safety by design
The ACH135 is certified to the latest CS 27/FAR27 standards including energy absorbing fuselage,
seats and crash resistant fuel cells. The safety of twin engine performance is complemented with
redundancy incorporated in the hydraulics, electrics, main transmissions oil cooling and lubrication
systems.
The innovative Helionix flight deck has an open architecture and modular design with dual duplex
redundancy incorporating embedded functions. It features advanced intuitive software and a four axis
autopilot with complete envelope protection for ultimate precision and control with lowest pilot
workload.

135 T3H/P3H 18.ACH.01 E 3

The ACH135 can be powered by either Safran Helicopter Engines Arrius 2B2plus or Pratt & Whitney
Canada PW206B3 engines - both are FADEC controlled and provide efficient fuel burn characteristics.
These powerful and reliable engines, combined with the improved dynamic lifting system components,
provide outstanding performance and vital power reserves even in demanding High and Hot
conditions.
The exceptional payload of the aircraft is the result of modern technology fabrication in conjunction with
an extensive use of composite materials. The high degree of composite usage in the fuselage does not
only result in a low empty weight but it also provides a high degree of safety and resistance against
corrosive operating environments.
The ACH135 high rotor clearance and Fenestron facilitate safe ground operations for passengers and
crews on prepared and unprepared surfaces.

The benchmark in reliability

The extensive fleet experience and high level of product maturity has enabled the ACH135's
maintenance scheme to be "trimmed to perfection" delivering high intervals for the scheduled
inspections, excellent maintainability, high TBO times, outstanding reliability and availability.

Style and Comfort

Its cabin is elegant and modern with the comfort and the refinement you need for your helicopter
travels. Its large sliding doors and rear clamshell doors provide a convenient boarding and
disembarking while luggage can be loaded and retrieved safely and easily, even when the rotors are
running.
Enjoy the view - ACH135's large windows offer exceptional visibility for passengers while relaxing in
their comfortable seats.

Figure 1.2: View from rear into the empty cabin

Advanced glass cockpit - flight and mission management

The ACH135 offers a glass cockpit solution with a highly efficient Human Machine Interface (HMI)
designed to reduce the pilot workload and increase the flight safety. The avionics system, Helionix, is
the latest generation of Airbus avionics, 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

4 135 T3H/P3H 18.ACH.01 E

equipment from a moving map functionality to external cameras.

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, for
both day and night missions
• Enhanced situation awareness with integrated Helicopter Terrain Awareness and Warning System
(H-TWAS), 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)
• Unrivalled level of redundancy resulting from all functions embedded in each MFD, dual duplex air-
craft management computers and 2 Attitude and Heading Reference Systems (in IFR configuration),
plus an Integrated Electronic Stand-by Instrument (IESI).
• Full Usage Monitoring System (UMS) included in the basic Helionix package
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 ACH135'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 ACH135 digital avionics initialization procedures and self-test sequences are
automatically performed in the background, minimizing the time to become airbone.

Figure 1.3: Typical instrument panel

135 T3H/P3H 18.ACH.01 E 5

1.1 Baseline Aircraft Highlights and Main Improvements

Maintenance Reduction
Benefitting from the experience of more than 1,250 aircraft in service and over 4.4 million flight hours,
Airbus has further streamlined the ACH135 maintenance requirements to ensure lowest Direct
Maintenance Costs (DMC) and lowest Direct Operating Costs (DOC) in the light twin helicopter class
without compromising safety. Thanks to the extensive experience in close collaboration with Airbus
customers overhaul times and/or Service Life Limits (SLL) of the following components were
increased:

Airframe main components TBO /SLL Old value New value

Control rod SLL 19,200 Fh on condition
Hinged support SLL 12,300 Fh 30,000 Fh
Main rotor blade SLL 12,400 Fh on condition
Main rotor blade damper SLL 4,800 Fh or 10 years 12 years
Main transmission housing SLL 7,000 Fh on condition
Mixing lever gear unit forked lever SLL 11,500 Fh 30,000 Fh
Swash plate bearing & control ring SLL 6,700 Fh on condition
Starter / generator TBO 1,000 Fh usage based
Main transmission TBO 4,000 Fh 5,000 Fh
Tail rotor transmission TBO 3,600 Fh 5,000 Fh

By streamlining the scheduled inspection tasks also the required mean man hours could be reduced:

Scheduled airframe inspections Old estimated New estimated

mean man hours mean man hours
12-month inspection 20 19
Intermediated inspection every 500 Fh 28 26
Periodical inspection every 1,000 Fh or 3 years 111 80
plus
Engine Arrius 2B2 500 Fh inspection 4 2.5

Pratt & Whitney Canada has extended the previous 800 Fh inspection to 1,000 Fh for the PW206B3
engine, thus now aligning with the airframe inspection interval schedule.

Flight Data Continuous Recorder (FDCR)

The Flight Data Continuous Recorder (FDCR), built into the Helionix avionics, collects vehicle and
engine parameters, records the data continuously and downloads the data onto the Compact Flash
card in the Data Transfer Device (DTD). Analysis of the recorded data post flights supports operator
programs, including Helicopter Flight Data Monitoring (HFDM) and maintenance activities.

6 135 T3H/P3H 18.ACH.01 E

Fleet Keeper®
Fleet Keeper is a user-friendly electronic Technical LogBook (TLB) application, completely replacing
the paper TLB and improving the process by delivering a cockpit view of customers' fleet status. It
enables real-time data exchange between pilots, line mechanics and airworthiness managers.

Figure 1.4: Fleet keeper example

Fleet Keeper is a secured cloud-based solution in combination with a user-friendly web and mobile
application. It handles pilot tasks like pre- and post-flight checks, recording of flight data and events as
well as line maintenance and airworthiness duties, including management of line maintenance, events
and discrepancies or electronic signatures.
Data download from Fleet Keeper enables easy and quick transfer into Maintenance Information
Systems (e.g. CAMO tools). It is compatible with all Airbus helicopter models, as well as those of other
manufacturers.
Fleet Keeper is a deployable tool ready to replace operators' paper technical logbooks, by meeting
EASA M.A.306 & FAA Part 135 regulations.

135 T3H/P3H 18.ACH.01 E 7

Flight Planner®
Flight Planner is Airbus' comprehensive application for helicopter portable Electronic Flight Bag (EFB).
This software, running on mobile devices, is dedicated to flight crews, and is fully adapted for an
efficient mission preparation. The all-in-one application provides useful features reducing significantly
crew workload such as:
• Interactive flight & mission planning with feasibility check,
• Helicopter performance and weight & balance calculation,
• Maps and terrain display, navigation data, airport charts,
• Electronic documents display (eTechPub…),
• Weather and NOTAM access and consultation.

Figure 1.5: Flight Planner mission computation example

8 135 T3H/P3H 18.ACH.01 E

Optimized aerodynamic
Airbus developed new, optimized aerodynamic elements for ACH135 granting optimal mission
capability. More in detail:
• The vertical fin is extended in its upper section to extend the envelope of the autopilot
• The oil cooler cowling and the engine exhaust pipes are tailored to the specific characteristics of
each engine, with shorter shapes for Safran Helicopter Engines and extended geometries for Pratt
& Whitney Canada engines

Figure 1.6: Example of ACH135 equipped with Pratt & Whitney Canada engines

Figure 1.7: Example of ACH135 equipped with Safran Helicopter engines

135 T3H/P3H 18.ACH.01 E 9

Optional Equipment Highlights and Main Improvements

Wireless connectivity Connext (Garmin)

Garmin's connext is based on Garmin's Flight Stream 210 using Bluetooth technology. The option
enables wireless data exchange between the helicopters built-in GTN 750 and electronic devices, such
as:
• Flight plan up-/download and synchronization
• GPS position transmission

Professional Ground Station (PGS) Vision System and Helicopter Flight Data
Monitoring (HFDM)
Modular ground tools are available, enabling download of helicopter data and their visualization and
analysis on ground:

1. Professional Ground Station (PGS) Vision System:

PGS Vision System is software, enabling users to turn raw binary data into readable charts and
graphs. PGS Vision also converts CVR audio encoded data to standard Microsoft WAV file format
and synchronize audio records to the flight data. PGS Vision System is typically used to visualize
CVFDR data on ground.

2. Helicopter Flight Data Monitoring (HFDM):

HFDM is the process of a systematic, pro-active analyzing of recorded flight data to enhance
aviation safety, enabled by means of the Professional Ground Station (PGS) Analysis System. The
software facilitates flight analysis and detection of events to identify and address operational risks
before they can lead to incidents and accidents. Data recorded during the flight can then be used for
in-depth analysis and subsequent implementation of corrective actions through training programs or
changes to operational procedures. This process is assisted by presenting 3D replay of high fidelity
aircraft models fully animated and synchronized to flight data enabled by the PGS Replay 3D
module. The software enables data visualization, analysis and 3D replay of flight data recorded by
• The Flight Data Continuous Recorder (FDCR), included in the H135 Baseline and/or,
• The optional Cockpit Voice and Flight Data Recorder (CVFDR).

Figure 1.8: PGS Replay 3D: Example of 3D flight replay

10 135 T3H/P3H 18.ACH.01 E

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 with a horizontal and vertical field of view of approx. 70° x 120°,
which can be indicated on the center and/or LH MFD in the cockpit.
Two different camera installations are offered:
• External multi-purpose camera on tail boom
The camera is installed at the lower rear cover of tail boom vertical fin and features observation of
the cargo hook and helicopter rear loading. The camera angle is pre-adjusted by means of three
adjustment screws.
• External rear-view camera on landing gear
The camera is installed at the RH aft landing gear cross tube and features observation of the area
behind the helicopter which may be beneficial for rearward takeoffs.

Figure 1.9: External camera pictures displayed on Multi-Functional Displays

135 T3H/P3H 18.ACH.01 E 11

Offshore
The ACH135 offers several options to increase safety and reliability during offshore missions, or to
comply with customers' or regulations' requirements. Between others:
• Emergency float system with auto-activation and floatation demonstrated up to sea state 6
• Automatic Deployable Emergency Locator Transmitter (ADELT)
• Emergency Life Raft Sytem (ELR) certified up to sea state 6 with optionally available survivor
Emergency Locator Transmitter (ELT)
• Helicopter Emergency Egress Lighting System (HEELS)
• Search and rescue weather radar RDR-1600 by Telephonics
• Lashing points for ship landings
• Corrosion protection for high corrosive environment
• Main rotor blade folding

Figure 1.10: HEEL installation for crew and sliding doors (typical)

12 135 T3H/P3H 18.ACH.01 E

Digital Voice Control System DVCS 6100 (Becker)

Alternatively to the Digital Audio Control System (DACS) from Cobham, the Digital Voice Control
System DVCS 6100 from Becker is available. The DVCS 6100 allows the complete handling of
intercommunication, voice communication and alert monitoring.
The system also provides the following modes of operation / features:
• Intercommunication between pilot, copilot and the passengers
• Handling of up to 8 transceivers and 8 receivers (2 for ACU 6101) with a capability of individual
volume control
• Monitoring of up to 6 fixed inputs
• Main volume control for receiver and intercom audio
• Aircraft intercommunication either "voice operated exchange" (VOX) or "push to talk" (PTT)
controlled mode (VOX setting via individual potentiometer)
• Up to 3 intercom circuits to separate cockpit and cabin communication
• Optical call indication for intercom request plus aural call alert
• Indication of transmission via status lights
• Built in test functionality with optical indication of test status/result
• In case of system failure reduced operation via "SLAVED" or "BACK-UP" mode possible
• Configuration capability for system integration or maintenance shops to configure and adapt the
system to the individual aircraft requirements, stored in the external memory module.
The system includes two Audio Control Units (ACUs) in the cockpit, and one Remote Electronic Unit
(REU). The REU also provides the possibility of communication with a winch operator as well as with
the ground crew (via ground crew connector), if required. When external communication capability from
the cabin is required, additional passenger audio control units ACU 6100 or ACU 6101 can be installed

Figure 1.11: Audio Control Unit (ACU) 6100 pilot, copilot or pax (Becker)

135 T3H/P3H 18.ACH.01 E 13

Single pilot IFR cockpit

The flexibility of ACH135 is underlined by the different avionic solutions available. The instrument panel
can be freely configured for single or single/dual pilot operations. All solutions are IFR certified:
Three flight displays can be installed in the extended instrument panel, providing the highest mission
capability for single or dual pilot operations.
The Extended instrument panel in combination with two displays provides plenty of space for the
customization with STC equipment.
The installation of two displays on the standard instrument panel offers the lightest possible solution,
combined with extraordinary external field of view.

Blank

Figure 1.12: Example of extended instrument panel with two MFD

Figure 1.13: Example of standard single pilot instrument panel with two MFD

14 135 T3H/P3H 18.ACH.01 E

2 General Characteristics

2.1 Cockpit and Cabin Layouts

Seats & equipment as option

1 or 2 pilots + up to 5 passengers in energy absorbing individual seats

2.2 Weight

kg lb
• Empty weight, Baseline Aircraft Definitiona 1,563 3,446
• Useful load, Baseline Aircraft Definition 1,417 3,124
• Pilot 85 187
• Payload and / or fuel 1,332 2,937
• Maximum Takeoff Weight (MTOW) 2,980 6,570
• Maximum Takeoff Weight (MTOW) with external load 2,980 6,570
• Maximum taxi weight 3,000 6,614
• Maximum cargo-sling load (single hook) 1,200 2,646
a. Margin ±1.5 %.

2.3 Power Ratings

Engine Ratings (Uninstalled)1

The ACH135 can be equipped with either two Pratt & Whitney Canada PW206B3 or two Safran
Helicopter Engines ARRIUS 2B2plus turboshaft engines. Values are per engine manufacturer
specification.

Pratt & Whitney Canada PW206B3 turboshaft engines

All Engines Operative (AEO) kW shp

• Takeoff-Power (TOP) 528 708
• Maximum Continuous Power (MCP) 457 613

One Engine Inoperative (OEI) kW shp

• OEI 30 s 610 818
• OEI 2 min 582 780
• OEI MCP 528 708

Safran Helicopter Engines ARRIUS 2B2plus turboshaft engines

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

135 T3H/P3H 18.ACH.01 E 15

All Engines Operative (AEO) kW shp

• Takeoff-Power (TOP) 492 660
• Maximum Continuous Power (MCP) 464 622

One Engine Inoperative (OEI) kW shp

• OEI 30 s 606 812
• OEI 2 min 589 790
• OEI MCP 538 721

Main Transmission Ratings

All Engines Operative (AEO) kW shp

• Takeoff Power (TOP) 2 x 320 2 x 429
• Maximum Continuous Power (MCP) 2 x 283 2 x 380

One Engine Inoperative (OEI) kW shp

• OEI 30 s 1 x 526 1 x 705
• OEI 2 min 1 x 513 1 x 687
• OEI MCP 1 x 368 1 x 493

2.4 Fuel Capacities

Usable fuel
liters US gal kg lb
• Standard fuel tanks 700.5 185.1 560.4 1,235.4
• Internal long range fuel tank (option) 212.7 56.2 170.2 375.2

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

16 135 T3H/P3H 18.ACH.01 E

2.5 External Dimensions

Figure 2.1: External dimensions

135 T3H/P3H 18.ACH.01 E 17

2.6 Internal Dimensions

Figure 2.2: Internal dimensions

Floor area Volume

Cabin & cargo compartment 4.35 m² 46.83 ft² 4.90 m³ 173.04 ft³
Cockpit (pilot side) 1.15 m² 12.38 ft² 1.00 m³ 35.31 ft³
Total (undivided) 5.50 m² 59.21 ft² 5.90 m³ 208.35 ft³

2.7 External Sound Levels

Flight phase Certified Sound ICAO Annex 16, Chapter ICAO Annex 16, Chapter
Levels 8.4.1 & FAR 36 H, Stage 2 8.4.2 & FAR 36 H, Stage 3
limits at 2,980 kg limits at 2,980 kg
[EPNdB] [EPNdB] [EPNdB]
Takeoff [EPNL] 86.1 94.8 91.8
Overflight [EPNL] 82.7 93.8 89.8
Approach [EPNL] 90.3 95.8 94.8

18 135 T3H/P3H 18.ACH.01 E

2.8 Touch Down Forces

The touch down forces will be mainly transferred to a solid landing site via the four skid shoes on the
landing gear.

Figure 2.3: Touch down forces

Skid shoe position FWD LH FWD RH AFT LH AFT RH

Max. occurring force 17 kN 17 kN 24 kN 24 kN

135 T3H/P3H 18.ACH.01 E 19

Blank

20 135 T3H/P3H 18.ACH.01 E

3 Baseline Aircraft Definition

GENERAL
• Energy absorbing fuselage • Skid-type landing gear with skid protectors, capable of
• Tail boom with fixed horizontal stabilizer taking ground-handling wheels
• Vertical fin with faired-in Fenestron • Long boarding steps, LH and RH
• Upper deck with fittings for main gearbox, engines, • Maintenance built-in steps and grips
hydraulic and cooling system • Exterior painting (single color)
• Cowlings for main transmission and engine

COCKPIT, CABIN AND CARGO COMPARTMENT

• One-level cabin and cargo compartment floor with Covers for copilot collective lever & cyclic stick
integrated rails Engine controls with manual engine back-up system at pilot's
• Glazed canopy collective pitch lever
• Two hinged cockpit doors with sliding window Single pilot instrument panel with glare shield and slant
• Map case in pilot's door console
• Two wide passenger sliding doors Ram-air and electrical ventilating system for cockpit and
• Two rear hinged clam-shell doors cabin
Helmet holder in the cockpit
• Longitudinally adjustable energy absorbing pilot and copilot
seats with head rest and 4-point safety belts with automatic Headset holder in the cabin
locking system Portable fire extinguisher
• Cabin boarding grips LH and RH Stowage net for first aid kit at the LH rear clam-shell door
• Interior paneling with integrated basic sound insulation Flash light (torch) for pilot side
• Flight controls for pilot side; fixed provisions of flight
controls for copilot side

INSTRUMENTS
• Flight Display Subsystem (FDS) composed of 2 smart • Standby instruments:
multifunction displays (6 x 8 inch) providing the following • Integrated Electronic Standby Instrument (IESI)
functions: • Standby compass
• Flight and Navigation Display (FND) format (incl. PFD, • Usage Monitoring System (UMS) - Helionix
FLI, Master List, NAV, RPM, mast moment & fuel
indication) • Flight Data Continuous Recorder (FDCR) - Helionix
• Vehicle Management System (VMS) format (incl. engine, • "One hundred feet" alert
gearbox, fuel, electrical system, RPM & clock indication) • Directional Gyro Free Steering Mode
• Vehicle Management System (VMS) including:
• Warning unit:
• 2 duplex Aircraft Management Computer (AMC)
• Engine fire warning with fuel emergency shut-off
• Reference sensors: • Warning lights
• 1 Attitude and Heading Reference System • Fire extinguishing system warning
• Air Data sensor pilot side (electrically heated pitot tube
• Cockpit Control Panel (CCP) for FDS
and static port)
• 1 Magnetometer • Data Transfer Device (DTD)
• Engine switch panel

POWER PLANT
• Two Pratt & Whitney Canada PW206B3 turbine engines or • Twin-engine OEI-training mode
two Safran Helicopter Engines ARRIUS 2B2plus turbine • Oil cooling and lubricating system with thermostatic valve
engines
• Crash resistant fuel system with a flexible bladder-type
These two engines are equipped with: main tank and supply tank (split into two sections)
• Fire detectors • Automatically controlled variable rotor speed system
• Full Authority Digital Engine Control (FADEC) • Fuel tank filler flap, lockable
• Chip detectors with quick-disconnect plugs • Drain system
• Overspeed protection system
• Cycle indication on FDS • Fire walls

TRANSMISSION SYSTEM
• Flat-shaped main gearbox with two stages • Free wheel assemblies in the engine input drives
• Chip detector system with quick-disconnect plug (main • Tail rotor drive shaft
gearbox) • Tail rotor gearbox with splash lubrication and oil level sight
• Redundant oil cooling and lubrication system gauge
• Main gearbox attachment with Anti-Resonance Isolation • Chip detector system with quick-disconnect plug (tail rotor
System (ARIS) gearbox)

135 T3H/P3H 18.100.01 E 21

ROTOR AND FLIGHT CONTROLS

• Bearingless Main Rotor system (BMR) with improved • Basic provisions for an easy integration of a track and
dynamic characteristics, consisting of: balance system
• Rotor head / mast in one piece • Fenestron-type tail rotor with ten metal blades
• Four fiber-reinforced composite main rotor blades with (asymmetric blade spacing) and stator
anti-erosion strips, control cuff, elastomeric lead-lag
• Tail rotor gearbox cover
dampers and special blade tip painting
• Tail rotor control system with flexball cable and single
• Main rotor control system with dual hydraulic boost
system hydraulic booster
• Digital 3-axis SAS (Stability Augmentation System)
• Electrical trim system
• Mast moment system

ELECTRICAL INSTALLATION
• Two starter / generators (2x200 A, 28 VDC) • One utility receptacle in LH side of cargo compartment
• Nickel-Cadmium battery, (24 VDC, 27 Ah) (28 VDC, 10 A)
• External power connector (STANAG 3302, LN9064, SAE • Lighting:
AS 25018, SAE AS 35061) • Anti-collision warning light (red flashing), LED
• Power distribution system: • Fixed, nose-mounted landing light
• Two primary busbars • Three position lights (red, green, white), LED
• Two shedding busbars • Adjustable instrument lighting
• Two essential busbars • One utility light in the cockpit
• Two high load busbars (80 A) - for optional equipment • 5 spot-lights in the cabin
only • One light in cargo compartment RH side
• Two high power busbars (200 A) • Radio:
• Battery bus • Two radio master switches

GROUND HANDLING KITa

• Two ground-handling wheels • Lifting points
• Basic aircraft covers (short term) • Maintenance Ground Station (MGS) software
• Main rotor blade tie-down lash bags • Airbus Helicopters Data Loader (AHDL)
• Oil drain kit • Flight Data Continuous Recorder (FDCR) converter
• Fuel tank drain device • Fleet keeper® applicationb
• Keys for cockpit doors, cabin doors, baggage • Flight Planner applicationc
compartment doors and tank flap (one-key system)
• Battery key
a. Weight not included in the standard helicopter empty weight.
b. Licence for one year and one helicopter included
c. Two licenses for one year and one helicopter included. Availability date to be confirmed.

DOCUMENTATION (in English)

• One Flight Manualab (on paper) • List of Applicable Publications (LOAP)a online via
• One Pilots Checklistc (on paper) Keycopter portal
• One Master Minimum Equipment List (MMEL)a online via • One Avionics Manuald (for avionics installed by Airbus
T.I.P.I. Helicopters) (on CD-ROM)
• One Logbook (on paper, CD-ROM on demand) • One ECMMc (Electronic Component Maintenance
Manuals) for vendor manuals
• One Historical Record (on paper, CD-ROM on demand)
• One Engine Documentatione (format depends on engine
• Technical Documentationa incl. AMM, SDS, WDM, IPC, manufacturer), furnished by supplier, including:
MSM, CECG, SRM online via Keycopter® portal • Maintenance Manual
• Service Bulletin Catalogue (SB) online via T.I.P.I. • Illustrated Parts Catalogue
a. Revision service included as long as the aircraft is operational
b. One Flight Manual included in the standard helicopter empty weight
c. Revision service for 3 years
d. Customized documentation
e. Revision service for 3 years for Safran HE, 2 years for PWC

22 135 T3H/P3H 18.100.01 E

4 Mission Configuration

Airbus offers the following configurations for specific ACH135 missions. The created mission
configurations should be regarded as a first proposal for customers to evaluate the suitability of the
ACH135 for their operational fields. The shown mission configurations comprise the Baseline Aircraft
and a list of Mission Equipment.
The following mission configurations are available:
• Stylence by ACH, 5 passengers and 1 cabinet
• Stylence by ACH, 4 passengers, 1 cabinet and 1 multifunctional box
• Stylence by ACH, 4 passengers and 2 cabinets
Please note that the mission configurations include equipment requested by EASA OPS.
They do not cover oxygen equipment and equipment required for extended over water operations.
The operator shall contact his national authority for the approval of the planned aircraft mission
configuration.

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
equipment suitable for the ACH135. 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 ACH135 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.

135 T3H/P3H 18.ACH.01 E 23

Stylence®

Figure 4.1: Stylence Cabin layout - example

Effortless beauty, maximum performance

Stylence by ACH exudes simplicity. Fluid lines give it a dynamic and contemporary profile: a powerful
look accentuated by impressive space and unmatchable comfort which combines perfectly with the
aircraft design and technology.
It is the class leading combination of style & performance for the most demanding corporate and private
missions.
ACH135 Stylence package offers a functional and refined cabin to enhance passenger cabin
experience while providing the best operational performance.

A world of possibilities
Stylence by ACH is available in 6 harmonies but can also be customized on request through our
"bespoke service".

24 135 T3H/P3H 18.ACH.01 E

4.1 Stylence®, 5 Passengers Solution Including one Cabinet

4.1.1 Mission Parameter

• Flight Rules Single / Dual Pilot IFR Night

• Cat. A Yes
• Instrumentation Glass Cockpit
• NVG friendly No
• EASA OPS Yesa
a. Please refer to chapter 5.4.

Figure 4.2: Stylence, 5 passengers solution including one cabinet

4.1.2 Mission Configuration

Baseline Aircraft

Qty Document Commercial Description kg lb

Reference Reference
Baseline Aircraft
1 00-10048-A E0000-001-00 H135 Baseline Aircraft 135 T3H/P3H 18.100.01 E 1,563.0 3,445.8
plus
1 00-10048-A E0000-003-01 Safran Helicopter Engines ARRIUS 2B2 turbine engines 0.0 0.0
(2 engines)
1 00-10048-A E0000-003-02 Pratt & Whitney Canada PW206B3 turbine engines (2 engines) 0.0 0.0
Subtotal Weight: 1,563.0 3,445.8
1.5 % Weight margin: 23.4 51.7
Subtotal Weight (incl. margin): 1,586.4 3,497.5

Mission Package

Qty Document Commercial Description kg lb

Reference Reference
Mandatory Equipment
General Equipment
1 05-03018-B E2561-000-00 First aid kita 1.2 2.6
1 05-22030-B E2621-000-00 Engine fire extinguishing system 4.0 8.8
1 05-22031-A E7924-000-00 Fuzz burners for engines 1.0 2.2
1 05-22032-B E7111-000-00 Engine cowling heat protection 1.8 4.0
1 05-23009-B E7165-000-00 Engine compressor wash kit 2.0 4.4

135 T3H/P3H 18.ACH.01 E 25

Qty Document Commercial Description kg lb

Reference Reference
1 05-30004-C E3310-001-00 Flashlight for copilot side 0.3 0.7
1 05-31146-A E2511-000-00 Tinted sun shades for cockpit windshield roof section 1.8 4.0
1 05-32014-A E3042-000-00 Windshield wiper system 4.9 10.8
1 05-33007-B E3113-000-00 Center console 1.4 3.1
1 05-34012-B E2570-000-00 Avionics compartment 4.6 10.1
1 05-37030-B E6700-000-20 Copilot flight controls, detachable parts 6.1 13.4
1 05-38025-B E3111-000-00 Instrument panel extension on copilot side 1.5 3.3
1 05-39021-A E2513-001-00 Map case in copilot door 0.4 0.9
1 05-39022-A E2514-000-00 Map cases on instrument panel glare shield 0.6 1.3
1 05-41013-B E2142-100-00 Bleed air heating system 6.4 14.1
1 05-61026-A E2433-100-00 Battery (40 Ah, 24 VDC) ULM (Saft) instead of standard battery 8.3 18.3
1 05-71003-B E6350-000-00 Rotor brake system 5.7 12.6
Specific Mission Equipment
1 06-45082-B E3343-200-10 Search & landing light, fixed provisions 1.2 2.6
1 06-45082-B E3343-200-20 Search & landing light, detachable parts 3.3 7.3
1 06-67081-A E2562-000-00 Emergency Locator Transmitter (ELT) 1.7 3.7
Interior Layout
1 07-86019-A E1150-000-00 Special interior paintingb 0.0 0.0
Avionics
1 08-00447-B E2300-120-00 Avionics Package DP IFR GC GTN 750 0.0 0.0
1 08-16164-C E2341-000-00 Digital Audio Control System (DACS), incl. ACP53 (Cobham), 5.8 12.8
pilot + copilot
1 08-22083-A E3451-000-00 Transponder GTX 335R (Garmin)c 2.4 5.3
1 08-25519-A E3455-000-00 Distance Measuring Equipment (DME) DME-4000 (Rockwell 2.6 5.7
Collins)
1 08-26063-A E3431-000-00 Marker beacon receiver MKR3300-1 (Becker) 1.2 2.6
d
1 08-43077-C E3463-001-00 GPS/NAV/COM GTN 750 (Garmin), copilot 6.9 15.2
1 08-43077-C E3463-002-00 GPS/NAV/COM GTN 750 (Garmin), pilotd 8.2 18.1
1 08-65054-A E3161-001-00 Flight Display Subsystem (FDS), copilot 5.5 12.1
1 08-99005-B E0000-151-00 Avionics Package DP IFR GTN Series interconnection / wiring 23.5 51.8
1 08-21036-A E3441-000-00 Radar altimeter KRA 405B (Honeywell) 3.3 7.3
1 08-35068-B E3446-000-00 Helicopter Terrain Awareness and Warning System (H-TAWS) - 0.1 0.2
Helionixe
1 08-35069-B E3446-100-00 Synthetic Vision System (SVS) - Helionixe 0.0 0.0
1 08-53010-B E2213-000-00 Additional Attitude and Heading Reference System (AHRS) & 5.4 11.9
magnetometer
1 08-54004-B E3411-000-00 Copilot pitot static system 2.9 6.4
1 08-65068-B E3315-402-00 iPad Air holder, pilot 0.7 1.5
1 08-65068-B E2461-002-00 Electrical fixed provisions, 5 VDC, pilot 0.6 1.3
1 08-72007-A E2212-100-00 4-axis Automatic Flight Control System (AFCS) 17.6 38.8
1 08-81045-A E3139-000-00 Lightweight Aircraft Recording System (LARS) Alerts Vision 0.7 1.5
1000 (Appareo)

26 135 T3H/P3H 18.ACH.01 E

Qty Document Commercial Description kg lb

Reference Reference
Reference Equipment
General Equipment
1 05-02084-A E1111-300-00 Complex exterior painting instead of standard painting 2.7 6.0
1 05-31149-B E5611-300-00 Tinted front windshields 0.0 0.0
1 05-31149-B E5632-300-00 Tinted windows in cockpit doors 0.0 0.0
1 05-31149-B E5632-305-00 Tinted windows in cabin incl. sliding windows in sliding doors 1.2 2.6
1 05-42051-B E2111-000-00 Air Conditioning System (ACS) 49.7 109.6
1 05-85018-A E2841-000-00 Fuel management system (fuel flow meters) 1.0 2.2
Specific Mission Equipment
1 06-66025-B E3342-400-00 Boarding step illuminations 0.3 0.7
Interior Layout
1 07-30078-B E2581-100-00 Enhanced sound proofing kit 27.0 59.5
1 07-30079-A E2521-100-00 Separation wall for cabin / cargo compartment 4.4 9.7
1 07-60049-B E2513-005-00 Map cases in sliding doors 1.4 3.1
1 07-90036-B E2524-005-00 Retractable coat hooks in rear cabin (2 hooks) 0.1 0.2
Interior Layout - Stylence, 5 passengers
1 07-80056-C AAT-35200-200-2 Stylence®, 5 passengers and 1 cabinet, package (AAT - STC), 0.0 0.0
2018f
1 07-81129-A AAT-35230-200-2 Stylence height adjustable pilot seat instead of standard pilot 3.1 6.8
seat
1 07-81129-A AAT-35230-201-2 Stylence height adjustable copilot seat instead of standard 3.1 6.8
copilot seat
1 07-81130-A AAT-35230-202-2 Stylence front passenger seats (2 seats) 24.8 54.7
1 07-81130-A AAT-35230-203-2 Stylence front middle passenger seat 12.4 27.3
1 07-81131-A AAT-35230-204-2 Stylence rear passenger seats (2 seats) 24.8 54.7
1 07-82022-A AAT-35220-201-2 Stylence armrest in rear window niches 0.3 0.7
1 07-83036-A AAT-35220-208-2 Stylence entrance rails 0.3 0.7
1 07-83037-A AAT-35210-201-2 Stylence carpet for cockpit 5.2 11.5
1 07-83037-A AAT-35210-202-2 Stylence carpet for cabin 3.3 7.3
1 07-83037-A AAT-35210-203-2 Stylence carpet for cargo compartment 4.2 9.3
1 07-83039-A AAT-35220-210-2 Stylence leather cuffs for flight controls 0.0 0.0
1 07-85056-B AAT-35240-202-2 Stylence rear cabinet with USB power socket 12.5 27.6
1 07-86035-A AAT-35260-200-2 Stylence Passenger Service Units (PSU) 0.3 0.7
1 07-86036-A AAT-35220-204-2 Stylence metal placards 0.0 0.0
2 07-81140-A E2512-000-90 Stylence pilot seat protective cover GSE GSE
5 07-81140-A E2522-000-90 Stylence passenger seat protective cover GSE GSE

135 T3H/P3H 18.ACH.01 E 27

Qty Document Commercial Description kg lb

Reference Reference
Avionics
1 08-16166-A E2340-000-00 Headset electrical power supply (28 VDC), fixed provisionsg 0.5 1.1
2 08-18079-B E2342-100-00 Headset adapter cable crew GLENAIR / LEMO ANR 0.2 0.4
5 08-18079-B E2342-105-00 Headset adapter cable pax GLENAIR / LEMO ANR 1.0 2.2
7 08-18080-B E2315-300-00 Headset A20 ANR LEMO (Bose), low impedance 2.1 4.6
1 08-43078-A E3464-000-00 Wireless connectivity Connext (Garmin) 0.3 0.7
Subtotal Weight: 331.8 730.8
3.0 % Weight margin: 10.0 22.0
Subtotal Weight (incl. margin): 341.8 753.5
Total Weight: 1,928.2 4,251.0
a. Customization of first aid kit content necessary to comply with EASA OPS requirements. Medications may have to be
removed for Export.
b. RAL 9006 suitable for Titanium color line.
c. incl. ADS-B out
d. SBAS RNP approach local service availability verification through your Airbus helicopter sales representative on request.
e. The database update service is provided under a dedicated service contract. Please contact your Airbus helicopter sales
representative for further information.
f. This STC is only EASA certified. Prices and leadtimes for national certifications are available on request. Standard color line
is Titanium. Other color lines are available on request.
g. Required for Active Noise Reduction (ANR).

28 135 T3H/P3H 18.ACH.01 E

4.1.3 Stylence, Color Lines

Qty Document Commercial Description kg lb

Reference Reference
Interior Layout - Stylence, Color Lines
1 07-91130-A AAT-35290-110-1 Stylence, Silk Color Line 0.0 0.0
1 07-91130-A AAT-35290-120-1 Stylence, Titanium Color Line 0.0 0.0
1 07-91130-A AAT-35290-130-1 Stylence, Flame Color Line 0.0 0.0
1 07-91130-A AAT-35290-140-1 Stylence, Terra Color Line 0.0 0.0
1 07-91130-A AAT-35290-150-1 Stylence, Cobald Color Line 0.0 0.0
1 07-91130-A AAT-35290-160-1 Stylence, Shadow Color Line 0.0 0.0

135 T3H/P3H 18.ACH.01 E 29

4.1.4 Mission Performance

Weight breakdown (with payload and fuel)
kg lb
Weight basis for Equipped empty weight Stylence 5 passengers (incl. engine
Payload Range oil, unusable fuel and weight margin) 1,928 4,251
Diagram 1 pilots (1 x 85 kg) 85 187
Payload 5 passengers (5 x 85 kg) 425 937
Reserve fuel: 20 min in 1,500 ft with 130 KIAS 67 148
Fuel Contingency fuel: 5% 23 51
Trip fuel 452 996
Mission takeoff weight (MTOW) 2,980 6,570

Mission profile
• Takeoff at SL (maximum 2,980 kg)
• Climb flight AEO MCP from SL to 5,000 ft with VY, mean 65 KIAS
• Level flight in 5,000 ft with VBR (PW206B3: 133 KTAS; Arrius 2B2plus: 135 KTAS)
• Descent from 5,000 ft to SL with R/D of 1,000 fpm, mean 80 KIAS
• Landing at SL

Payload range diagram

Figure 4.3: Payload range diagram

Relevant flight data

PW206B3 engines Arrius 2B2plus engines
Calculated maximum range (without payload, with
trip fuel) 316 NM (585 km) 320 NM (593 km)
Corresponding flight time (incl. 2x climb / descent
phases) 2 h 25 min 2 h 24 min

30 135 T3H/P3H 18.ACH.01 E

4.2 Stylence®, 4 Passengers Solution Including one Cabinet and one

Multifunctional Box

4.2.1 Mission Parameter

• Flight Rules Single / Dual Pilot IFR Night

• Cat. A Yes
• Instrumentation Glass Cockpit
• NVG friendly No
• EASA OPS Yesa
a. Please refer to chapter 5.4

Figure 4.4: Stylence, 4 passengers solution including one cabinet and one multifunctional box

4.2.2 Mission Configuration

Baseline Aircraft

Qty Document Commercial Description kg lb

Reference Reference
Baseline Aircraft
1 00-10048-A E0000-001-00 H135 Baseline Aircraft 135 T3H/P3H 18.100.01 E 1,563.0 3,445.8
plus
1 00-10048-A E0000-003-01 Safran Helicopter Engines ARRIUS 2B2 turbine engines (2 0.0 0.0
engines)
1 00-10048-A E0000-003-02 Pratt & Whitney Canada PW206B3 turbine engines (2 engines) 0.0 0.0
Subtotal Weight: 1,563.0 3,445.8
1.5 % Weight margin: 23.4 51.7
Subtotal Weight (incl. margin): 1,586.4 3,497.5

Mission Package

Qty Document Commercial Description kg lb

135 T3H/P3H 18.ACH.01 E 31

Qty Document Commercial Description kg lb

Reference Reference
1 05-23009-B E7165-000-00 Engine compressor wash kit 2.0 4.4
1 05-30004-C E3310-001-00 Flashlight for copilot side 0.3 0.7
1 05-31146-A E2511-000-00 Tinted sun shades for cockpit windshield roof section 1.8 4.0
1 05-32014-A E3042-000-00 Windshield wiper system 4.9 10.8
1 05-33007-B E3113-000-00 Center console 1.4 3.1
1 05-34012-B E2570-000-00 Avionics compartment 4.6 10.1
1 05-37030-B E6700-000-20 Copilot flight controls, detachable parts 6.1 13.4
1 05-38025-B E3111-000-00 Instrument panel extension on copilot side 1.5 3.3
1 05-39021-A E2513-001-00 Map case in copilot door 0.4 0.9
1 05-39022-A E2514-000-00 Map cases on instrument panel glare shield 0.6 1.3
1 05-41013-B E2142-100-00 Bleed air heating system 6.4 14.1
1 05-61026-A E2433-100-00 Battery (40 Ah, 24 VDC) ULM (Saft) instead of standard battery 8.3 18.3
1 05-71003-B E6350-000-00 Rotor brake system 5.7 12.6
Specific Mission Equipment
1 06-45082-B E3343-200-10 Search & landing light, fixed provisions 1.2 2.6
1 06-45082-B E3343-200-20 Search & landing light, detachable parts 3.3 7.3
1 06-67081-A E2562-000-00 Emergency Locator Transmitter (ELT) 1.7 3.7
Interior Layout
1 07-86019-A E1150-000-00 Special interior paintingb 0.0 0.0
Avionics
1 08-00447-B E2300-120-00 Avionics Package DP IFR GC GTN 750 0.0 0.0
1 08-16164-C E2341-000-00 Digital Audio Control System (DACS), incl. ACP53 (Cobham), 5.8 12.8
pilot + copilot
1 08-22083-A E3451-000-00 Transponder GTX 335R (Garmin)c 2.4 5.3
1 08-25519-A E3455-000-00 Distance Measuring Equipment (DME) DME-4000 (Rockwell 2.6 5.7
Collins)
1 08-26063-A E3431-000-00 Marker beacon receiver MKR3300-1 (Becker) 1.2 2.6
1 08-43077-C E3463-001-00 GPS/NAV/COM GTN 750 (Garmin), copilotd 6.9 15.2
1 08-43077-C E3463-002-00 GPS/NAV/COM GTN 750 (Garmin), pilotd 8.2 18.1
1 08-65054-A E3161-001-00 Flight Display Subsystem (FDS), copilot 5.5 12.1
1 08-99005-B E0000-151-00 Avionics Package DP IFR GTN Series interconnection / wiring 23.5 51.8
1 08-21036-A E3441-000-00 Radar altimeter KRA 405B (Honeywell) 3.3 7.3
1 08-35068-B E3446-000-00 Helicopter Terrain Awareness and Warning System (H-TAWS) - 0.1 0.2
Helionixe
1 08-35069-B E3446-100-00 Synthetic Vision System (SVS) - Helionixe 0.0 0.0
1 08-53010-B E2213-000-00 Additional Attitude and Heading Reference System (AHRS) & 5.4 11.9
magnetometer
1 08-54004-B E3411-000-00 Copilot pitot static system 2.9 6.4
1 08-65068-B E3315-402-00 iPad Air holder, pilot 0.7 1.5
1 08-65068-B E2461-002-00 Electrical fixed provisions, 5 VDC, pilot 0.6 1.3
1 08-72007-A E2212-100-00 4-axis Automatic Flight Control System (AFCS) 17.6 38.8
1 08-81045-A E3139-000-00 Lightweight Aircraft Recording System (LARS) Alerts Vision 0.7 1.5
1000 (Appareo)

32 135 T3H/P3H 18.ACH.01 E

Qty Document Commercial Description kg lb

Reference Reference
Reference Equipment
General Equipment
1 05-02084-A E1111-300-00 Complex exterior painting instead of standard painting 2.7 6.0
1 05-31149-B E5611-300-00 Tinted front windshields 0.0 0.0
1 05-31149-B E5632-300-00 Tinted windows in cockpit doors 0.0 0.0
1 05-31149-B E5632-305-00 Tinted windows in cabin incl. sliding windows in sliding doors 1.2 2.6
1 05-42051-B E2111-000-00 Air Conditioning System (ACS) 49.7 109.6
1 05-85018-A E2841-000-00 Fuel management system (fuel flow meters) 1.0 2.2
Specific Mission Equipment
1 06-66025-B E3342-400-00 Boarding step illuminations 0.3 0.7
Interior Layout
1 07-30078-B E2581-100-00 Enhanced sound proofing kit 27.0 59.5
1 07-30079-A E2521-100-00 Separation wall for cabin / cargo compartment 4.4 9.7
1 07-60049-B E2513-005-00 Map cases in sliding doors 1.4 3.1
1 07-90036-B E2524-005-00 Retractable coat hooks in rear cabin (2 hooks) 0.1 0.2
Interior Layout - Stylence, 4 passengers
1 07-80056-C AAT-35200-220-2 Stylence®, 4 passengers, 1 cabinet, 1 multifunctional box, 0.0 0.0
package (AAT - STC), 2018f
1 07-81129-A AAT-35230-200-2 Stylence height adjustable pilot seat instead of standard pilot 3.1 6.8
seat
1 07-81129-A AAT-35230-201-2 Stylence height adjustable copilot seat instead of standard 3.1 6.8
copilot seat
1 07-81130-A AAT-35230-202-2 Stylence front passenger seats (2 seats) 24.8 54.7
1 07-81131-A AAT-35230-204-2 Stylence rear passenger seats (2 seats) 24.8 54.7
1 07-82022-A AAT-35220-201-2 Stylence armrest in rear window niches 0.3 0.7
1 07-83036-A AAT-35220-208-2 Stylence entrance rails 0.3 0.7
1 07-83037-A AAT-35210-201-2 Stylence carpet for cockpit 5.2 11.5
1 07-83037-A AAT-35210-202-2 Stylence carpet for cabin 3.3 7.3
1 07-83037-A AAT-35210-203-2 Stylence carpet for cargo compartment 4.2 9.3
1 07-83039-A AAT-35220-210-2 Stylence leather cuffs for flight controls 0.0 0.0
1 07-85056-B AAT-35240-202-2 Stylence rear cabinet with USB power socket 12.5 27.6
1 07-82023-A AAT-35240-203-2 Stylence multifunctional box 12.5 27.6
1 07-86035-A AAT-35260-200-2 Stylence Passenger Service Units (PSU) 0.3 0.7
1 07-86036-A AAT-35220-204-2 Stylence metal placards 0.0 0.0
2 07-81140-A E2512-000-90 Stylence pilot seat protective cover GSE GSE
4 07-81140-A E2522-000-90 Stylence passenger seat protective cover GSE GSE

135 T3H/P3H 18.ACH.01 E 33

Qty Document Commercial Description kg lb

Reference Reference
Avionics
1 08-16166-A E2340-000-00 Headset electrical power supply (28 VDC), fixed provisionsg 0.5 1.1
2 08-18079-B E2342-100-00 Headset adapter cable crew GLENAIR / LEMO ANR 0.2 0.4
4 08-18079-B E2342-105-00 Headset adapter cable pax GLENAIR / LEMO ANR 0.8 1.8
6 08-18080-B E2315-300-00 Headset A20 ANR LEMO (Bose), low impedance 1.8 4.0
1 08-43078-A E3464-000-00 Wireless connectivity Connext (Garmin) 0.3 0.7
Subtotal Weight: 331.4 730.6
3.0 % Weight margin: 9.9 21.8
Subtotal Weight (incl. margin): 341.3 752.4
Total Weight: 1,927.8 4,250.0
a. Customization of first aid kit content necessary to comply with EASA OPS requirements. Medications may have to be
removed for Export.
b. RAL 9006 suitable for Titanium color line.
c. incl. ADS-B out
d. SBAS RNP approach local service availability verification through your Airbus helicopter sales representative on request.
e. The database update service is provided under a dedicated service contract. Please contact your Airbus helicopter sales
representative for further information.
f. This STC is only EASA certified. Prices and leadtimes for national certifications are available on request. Standard color line
is Titanium. Other color lines are available on request.
g. Required for Active Noise Reduction (ANR).

34 135 T3H/P3H 18.ACH.01 E

4.2.3 Stylence, Color Lines

Qty Document Commercial Description kg lb

135 T3H/P3H 18.ACH.01 E 35

4.2.4 Mission Performance

Weight breakdown (with payload and fuel)
kg lb
Weight basis for Equipped empty weight Stylence 4 passengers, with
Payload Range multifunctional box (incl. engine oil, unusable fuel and 1,927 4,249
Diagram weight margin)
1 pilots (1 x 85 kg) 85 187
Payload 4 passengers (4 x 85 kg) 340 750
Reserve fuel: 20 min in 1,500 ft with 130 KIAS 67 148
Fuel Contingency fuel: 5% 23 51
Trip fuel 470 1,036
Mission takeoff weight (MTOW) 2,912 6,420

Payload range diagram

Figure 4.5: Stylence, 4 Passengers (box) Solution - payload range diagram

Relevant flight data

PW206B3 engines Arrius 2B2plus engines
Calculated maximum range (without payload, with
trip fuel) 316 NM (585 km) 320NM (593 km)
Corresponding flight time (incl. 2x climb / descent
phases) 2 h 25 min 2 h 24 min

36 135 T3H/P3H 18.ACH.01 E

4.3 Stylence®, 4 Passengers Solution Including two Cabinets

4.3.1 Mission Parameter

• Flight Rules Single / Dual Pilot IFR Night

• Cat. A Yes
• Instrumentation Glass Cockpit
• NVG friendly No
• EASA OPS Yesa
a. Please refer to chapter 5.4

Figure 4.6: Stylence, 4 passengers solution including two cabinets

4.3.2 Mission Configuration

Baseline Aircraft

Qty Document Commercial Description kg lb

Reference Reference
Baseline Aircraft
1 00-10048-A E0000-001-00 H135 Baseline Aircraft 135 T3H/P3H 18.100.01 E 1,563.0 3,445.8
plus
1 00-10048-A E0000-003-01 Safran Helicopter Engines ARRIUS 2B2 turbine engines (2 0.0 0.0
engines)
1 00-10048-A E0000-003-02 Pratt & Whitney Canada PW206B3 turbine engines (2 engines) 0.0 0.0
Subtotal Weight: 1,563.0 3,445.8
1.5 % Weight margin: 23.4 51.7
Subtotal Weight (incl. margin): 1,586.4 3,497.5

Mission Package

Qty Document Commercial Description kg lb

135 T3H/P3H 18.ACH.01 E 37

Qty Document Commercial Description kg lb

38 135 T3H/P3H 18.ACH.01 E

Qty Document Commercial Description kg lb

Reference Reference
Reference Equipment
General Equipment
1 05-02084-A E1111-300-00 Complex exterior painting instead of standard painting 2.7 6,0
1 05-31149-B E5611-300-00 Tinted front windshields 0.0 0.0
1 05-31149-B E5632-300-00 Tinted windows in cockpit doors 0.0 0.0
1 05-31149-B E5632-305-00 Tinted windows in cabin incl. sliding windows in sliding doors 1.2 2.6
1 05-42051-B E2111-000-00 Air Conditioning System (ACS) 49.7 109.6
1 05-85018-A E2841-000-00 Fuel management system (fuel flow meters) 1.0 2.2
Specific Mission Equipment
1 06-66025-B E3342-400-00 Boarding step illuminations 0.3 0.7
Interior Layout
1 07-30078-B E2581-100-00 Enhanced sound proofing kit 27.0 59.5
1 07-30079-A E2521-100-00 Separation wall for cabin / cargo compartment 4.4 9.7
1 07-60049-B E2513-005-00 Map cases in sliding doors 1.4 3.1
1 07-90036-B E2524-005-00 Retractable coat hooks in rear cabin (2 hooks) 0.1 0.2
Interior Layout - Stylence, 4 passengers
1 07-80056-C AAT-35200-210-2 Stylence®, 4 passengers and 2 cabinets, package (AAT - STC), 0.0 0.0
2018,f
1 07-81129-A AAT-35230-200-2 Stylence height adjustable pilot seat instead of standard pilot 3.1 6.8
seat
1 07-81129-A AAT-35230-201-2 Stylence height adjustable copilot seat instead of standard 3.1 6.8
copilot seat
1 07-81130-A AAT-35230-202-2 Stylence front passenger seats (2 seats) 24.8 54.7
1 07-81131-A AAT-35230-204-2 Stylence rear passenger seats (2 seats) 24.8 54.7
1 07-82022-A AAT-35220-201-2 Stylence armrest in rear window niches 0.3 0.7
1 07-83036-A AAT-35220-208-2 Stylence entrance rails 0.3 0.7
1 07-83037-A AAT-35210-201-2 Stylence carpet for cockpit 5.2 11.5
1 07-83037-A AAT-35210-202-2 Stylence carpet for cabin 3.3 7.3
1 07-83037-A AAT-35210-203-2 Stylence carpet for cargo compartment 4.2 9.3
1 07-83039-A AAT-35220-210-2 Stylence leather cuffs for flight controls 0.0 0.0
1 07-85056-B AAT-35240-202-2 Stylence rear cabinet with USB power socket 12.5 27.6
1 07-85057-A AAT-35240-201-2 Stylence front cabinet 21.7 47.8
1 07-86035-A AAT-35260-200-2 Stylence Passenger Service Units (PSU) 0.3 0.7
1 07-86036-A AAT-35220-204-2 Stylence metal placards 0.0 0.0
2 07-81140-A E2512-000-90 Stylence pilot seat protective cover GSE GSE
4 07-81140-A E2522-000-90 Stylence passenger seat protective cover GSE GSE

135 T3H/P3H 18.ACH.01 E 39

Qty Document Commercial Description kg lb

Reference Reference
Avionics
1 08-16166-A E2340-000-00 Headset electrical power supply (28 VDC), fixed provisionsg 0.5 1.1
2 08-18079-B E2342-100-00 Headset adapter cable crew GLENAIR / LEMO ANR 0.2 0.4
4 08-18079-B E2342-105-00 Headset adapter cable pax GLENAIR / LEMO ANR 0.8 1.8
6 08-18080-B E2315-300-00 Headset A20 ANR LEMO (Bose), low impedance 1.8 4.0
1 08-43078-A E3464-000-00 Wireless connectivity Connext (Garmin) 0.3 0.7
Subtotal Weight: 340.6 750.9
3.0 % Weight margin: 10.2 22.5
Subtotal Weight (incl. margin): 350.8 773.4
Total Weight: 1,937.3 4,271.0
a. Customization of first aid kit content necessary to comply with EASA OPS requirements. Medications may have to be
removed for Export.
b. RAL 9006 suitable for Titanium color line.
c. incl. ADS-B out
d. SBAS RNP approach local service availability verification through your Airbus helicopter sales representative on request.
e. The database update service is provided under a dedicated service contract. Please contact your Airbus helicopter sales
representative for further information.
f. This STC is only EASA certified. Prices and leadtimes for national certifications are available on request. Standard color line
is Titanium. Other color lines are available on request.
g. Required for Active Noise Reduction (ANR).

40 135 T3H/P3H 18.ACH.01 E

4.3.3 Stylence, Color Lines

Qty Document Commercial Description kg lb

135 T3H/P3H 18.ACH.01 E 41

4.3.4 Mission Performance

Weight breakdown (with payload and fuel)
kg lb
Weight basis for Equipped empty weight Stylence 4 passengers, with 2
Payload Range cabinets (incl. engine oil, unusable fuel and weight margin) 1,937 4,271
Diagram 1 pilots (1 x 85 kg) 85 187
Payload 4 passengers (4 x 85 kg) 340 750
Reserve fuel: 20 min in 1,500 ft with 130 KIAS 67 148
Fuel Contingency fuel: 5% 23 51
Trip fuel 470 1,036
Mission takeoff weight (MTOW) 2,922 6,442

Payload range diagram

Figure 4.7: Stylence, 4 Passengers (Cabinet) Solution - payload range diagram

Relevant flight data

PW206B3 engines Arrius 2B2plus engines
Calculated maximum range (without payload, with
trip fuel) 315 NM (583 km) 319 NM (591 km)
Corresponding flight time (incl. 2x climb / descent
phases) 2 h 24 min 2 h 24 min

42 135 T3H/P3H 18.ACH.01 E

5 Further Equipment Information

5.1 General Available Equipment

The following list presents the General Available Equipment which may be added to customize the
mission configurations or to build specific configurations. For further mission adaptation specific
equipment is also available on request. Any modification and/or complement of the proposed mission
configuration shall be done with the assistance of an Airbus Helicopters helicopter sales representative
to avoid incompatibilities between various optional equipment items.

Abbreviation Availability
G General Available Equipment for the mission configuration

Document Commercial Description kg lb

Stylence
Reference Reference

Yacht Interface Available Equipment*

*For EASA OPS compliance please refer to chapter 5.4
05-12010-A E7110-300-00 Maintenance step on cabin roof, LH 0,7 1.5 G
05-25037-C E7162-000-00 Inlet Barrier Filter (IBF) system 19.1 42.1 G
05-26020-A E1241-100-00 Corrosion protection for high corrosive environment 3.2 7.1 G
05-92019-A E6611-000-00 Main rotor blade folding, basic kit 1.5 3.3 G
05-92019-A E6611-100-10 Main rotor blade folding, fixed provisions for ground handling kit 0.8 1.8 G
05-92019-A E6611-100-90 Main rotor blade folding, ground handling kit GSE GSE G
05-93017-A E1021-000-10 Lashing points for wind speeds up to 40 kts, fixed provisions 1.6 3.5 G
05-93017-A E1021-000-20 Lashing points for wind speeds up to 40 kts, detachable parts 0.8 1.8 G
06-46012-A E3344-100-00 White strobe lights 1.3 2.9 G
a
06-61036-B E3215-100-10 Emergency floats, fixed provisions 9.5 20.9 G
06-61036-B E3215-000-20 Emergency floats, detachable parts 63.4 139.8 G
06-67080-A E2562-400-00 Automatic Deployable Emergency Locator Transmitter (ADELT) 10.3 22.7 G
08-12101-A E2312-000-00 Tactical radio VHF-FM NPX138N (Cobham)b 2.5 5.5 G
General Equipment
05-02084-A E1111-100-00 Enhanced exterior painting instead of standard painting 2.0 4.4
05-02085-B E6211-000-00 High visibility paint for main rotor blades 0.0 0.0 G
05-02086-A E1111-900-00 Surface protective coating (Airglaze) 0.5 1.1 G
05-02087-B E6211-100-00 Main rotor blade erosion protection paint 0.1 0.2 G
05-12011-B E2516-000-00 Boarding grips for cockpit 0.1 0.2 G
05-21036-C E8541-000-10 Cable cutter system, fixed provisions 3.1 6.8 G
05-21036-C E8541-000-20 Cable cutter system, detachable parts 8.1 17.9 G
05-31147-A E5632-005-00 Sliding windows in sliding doors 1.2 2.6
05-31148-A E5633-001-00 Window in clam-shell door LH 0.3 0.7
05-31148-A E5633-002-00 Window in clam-shell door RH 0.3 0.7
05-31150-A E2524-000-10 IFR training screens, fixed provisions 0.1 0.2 G
05-31150-A E2524-000-20 IFR training screens, detachable parts 1.2 2.6 G
05-31152-A E5632-100-00 Ram air deflectors for sliding windows in cockpit doors 0.6 1.3 G
05-31152-A E5632-105-00 Ram air deflectors for sliding windows in sliding doors 0.4 0.9
05-37031-B E6700-101-00 Pedal cover for copilot flight controls -4.8 -10.6 G

135 T3H/P3H 18.ACH.01 E 43

Document Commercial Description kg lb

Stylence
Reference Reference

05-39023-A E3315-102-00 Illuminated chart holder, pilot 0.9 2.0 G

05-39023-A E3315-101-00 Illuminated chart holder, copilot 0.8 1.8 G
05-44014-B E2122-100-00 Ventilation enhancement for cockpit 1.0 2.2
05-62029-A E2420-000-00 Alternating Current (AC) systemc 1.5 3.3
05-67040-B E2460-000-00 Power sockets (2x 28 VDC, 20 A) at center console 1.1 2.4
05-81054-A E2818-000-10 Internal long range fuel tank system, fixed provisions 2.0 4.4 G
05-81054-A E2818-000-20 Internal long range fuel tank system, detachable parts 35.9 79.1 G
05-93018-A E1021-100-10 Lashing points for ship landings, fixed provisions 2.1 4.6
05-93018-A E1021-100-20 Lashing points for ship landings, detachable parts 0.3 0.7
05-95005-A E1320-200-00 Long term cover kit for helicopter GSE GSE G
05-95006-A E1320-300-00 Main rotor head cover GSE GSE
05-97006-B E6201-100-00 Accelerometers for track and balance system (Chadwick 0.0 0.0 G
Helmuth)
05-97007-B E6201-200-10 Optical tracker FasTrak 11800-3 (Chadwick Helmuth), fixed 0.1 0.2 G
provisions
05-97007-B E6201-200-20 Optical tracker FasTrak 11800-3 (Chadwick Helmuth), 0.6 1.3 G
detachable parts
Specific Mission Equipment
06-11044-A E3274-000-10 Settling protectors, fixed provisions 0.1 0.2 G
06-11044-A E3274-000-20 Settling protectors, detachable parts 8.1 17.9 G
06-11045-B E3272-000-10 Snow skids, fixed provisions 0.9 2.0
06-11045-B E3272-000-20 Snow skids, detachable parts 18.3 40.3
06-12028-A E3210-100-00 Medium height landing gear instead of standard landing gear 5.2 11.5
06-12029-A E3213-100-00 Extended skid protection 3.4 7.5 G
06-21042-D E8510-001-10 External hoist LH, fixed provisions 13.1 28.9
06-21042-D E8510-001-20 External hoist LH, detachable parts 2.6 5.7
06-21042-D E8510-002-10 External hoist RH, fixed provisions 13.8 30.4
06-21042-D E8510-002-20 External hoist RH, detachable parts 2.5 5.5
06-21042-D E8510-100-31 External hoist (without hook and damper kit), 90 m, vendor 62.4 137.6
partsd
06-21042-D E8510-000-31 External hoist (without hook and damper kit), 50 m, vendor 56.2 123.9
partsd
06-21042-D E8510-300-30 External hoist, small hook damper kit & D-LOK hook, vendor 2.3 5.1
parts
06-21042-D E8510-300-31 External hoist, small hook damper kit & slide lock hook, vendor 2.3 5.1
parts
06-26028-A E8512-002-10 Cargo hook mirrors RH, fixed provisions 0.5 1.1
06-26028-A E8512-002-20 Cargo hook mirrors RH, detachable partse 4.0 8.8
06-26028-A E8512-002-90 Cover for cargo hook mirrors RH 0.4 0.9
06-26029-A E3181-000-10 External multi-purpose camera on tail boom, fixed provisions 2.0 4.4 G
06-26029-A E3181-000-20 External multi-purpose camera on tail boom, detachable parts 0.6 1.3 G
06-26029-A E3181-100-10 External rear-view camera on landing gear, fixed provisions 1.5 3.3 G
06-26029-A E3181-100-20 External rear-view camera on landing gear, detachable parts 1.4 3.1 G
06-27049-D E8511-000-10 Single cargo hook system, fixed provisions 5.2 11.5
06-27049-D E8511-000-20 Single cargo hook system, detachable parts 25.9 57.1
06-27049-D E8511-500-10 Dual cargo hook system, fixed provisions 6.6 14.6

44 135 T3H/P3H 18.ACH.01 E

Document Commercial Description kg lb

Stylence
Reference Reference

06-27049-D E8511-500-20 Dual cargo hook system, detachable parts 29.6 65.3
06-27049-D E8511-800-10 Cargo hook weighing system, fixed provisions 0.2 0.4
06-27049-D E8511-800-20 Cargo hook weighing system, detachable parts 0.2 0.4
06-45082-B E3343-300-10 2nd Search & landing light, fixed provisions 1.7 3.7
06-45082-B E3343-300-20 2nd Search & landing light, detachable parts 3.1 6.8
06-45082-B E3343-900-00 Search & landing light, IR mode 0.1 0.2
06-62034-A E2565-001-10 External Life Raft System (ELRS) LH, fixed provisions 0.8 1.8
06-62034-A E2565-001-20 External Life Raft System (ELRS) LH, detachable partsf 37.1 81.8
06-62034-A E2565-002-10 External Life Raft System (ELRS) RH, fixed provisions 0.8 1.8
06-62034-A E2565-002-20 External Life Raft System (ELRS) RH, detachable partsf 37.1 81.8
06-62034-A E2562-600-00 Survival emergency locator transmitter ELT(S) 0.9 2.0
06-65016-B E2625-100-00 2nd portable fire extinguisher 2.8 6.2 G
06-66027-B E3323-000-00 Illuminated signs "NO SMOKING / FASTEN SEAT BELT" 0.7 1.5 G
06-71011-B E2521-500-10 Separation curtain for cockpit / cabin, fixed provisions 0.3 0.7
06-71011-B E2521-500-20 Separation curtain for cockpit / cabin, detachable parts 0.3 0.7
Interior Layout
07-40037-C E2532-000-00 Sealed cabin floor 0.3 0.7
07-50082-B E5231-000-00 One-hand latching system for clam-shell doors 1.4 3.1 G
07-50083-A E5231-100-00 Extended opening fasteners for clam-shell doors 0.1 0.2 G
07-50084-A E5213-001-00 Sliding door fastener, intermediate and max. position, LH 1.2 2.6
07-50084-A E5213-002-00 Sliding door fastener, intermediate and max. position, RH 1.2 2.6
07-50085-B E5212-000-00 Jettisonable cockpit doors 0.9 2.0 G
07-50086-B E5212-100-00 Spoiler position for cockpit doors 1.0 2.2
07-50089-A E5211-200-00 Securing device for complete opening of cockpit doors 1.1 2.4
07-60050-B E2550-000-00 Variable tie-down net 3.3 7.3 G
Avionics
08-10026-B E2311-000-10 HF system HF-9000 (Rockwell Collins), fixed provisionsg 7.2 15.9 G
08-10026-B E2311-000-20 HF system HF-9000 (Rockwell Collins), detachable partsg 19.3 42.5 G
08-12102-B E2317-000-00 Tactical radio, fixed provisions, incl. antenna, power supply & 2.0 4.4
intercom interfaceb
08-15568-B E2315-400-00 LTE phone, fixed provisions, incl. antenna, power supply (28 1.0 2.2 G
VDC) & intercom interfaceh
08-15570-B E2315-000-00 Iridium satellite transceiver GSR 56 (Garmin) 4.3 9.5 G
08-18078-A E2315-100-00 Headset H 10-76 (David Clark), low impedance 0.6 1.3
08-18078-A E2315-200-00 Headset H 10-56 (David Clark), high impedance 0.6 1.3
08-18079-B E2342-000-00 Headset adapter cable crew GLENAIR / U92 0.1 0.2
08-18079-B E2342-005-00 Headset adapter cable pax GLENAIR / U92 0.2 0.4
08-24038-A E3452-100-00 Automatic Direction Finder (ADF), control unit CDF552 1.0 2.2
(Cobham)
08-24038-A E3452-000-00 Automatic Direction Finder (ADF), receiver DF-431B (Cobham) 11.0 24.3
08-31070-A E3443-200-00 Color weather radar RDR 2000 (Honeywell), radar radome 3.2 7.1
08-31070-A E3443-000-10 Color weather radar RDR 2000 (Honeywell), fixed provisions 0.8 1.8
08-31070-A E3443-010-30 Color weather radar RDR 2000 incl. control unit CP466 6.7 14.8
(Honeywell), vendor parts
08-31071-B E3443-300-00 Search and rescue weather radar RDR-1600 (Telephonics), 5.3 11.7
radar radome

135 T3H/P3H 18.ACH.01 E 45

Document Commercial Description kg lb

Stylence
Reference Reference

08-31071-B E3443-100-10 Search and rescue weather radar RDR-1600 (Telephonics), 1.7 3.7
fixed provisions
08-31071-B E3443-100-20 Search and rescue weather radar RDR-1600 (Telephonics), 12.9 28.4
detachable parts
08-35070-B E2327-000-10 Traffic Advisory System TAS620A (Avidyne), fixed provisions 3.0 6.6 G
08-35070-B E2327-000-20 Traffic Advisory System TAS620A (Avidyne), detachable parts 3.4 7.5 G
08-46068-B E3168-000-00 Moving map EuroNav 7 – RN7 (EuroAvionics), basic versioni 6.3 13.9
08-46068-B E3168-100-00 Moving map EuroNav 7 – RN7 (EuroAvionics), Iridium satcom 1.4 3.1
module
08-46068-B E3168-400-00 Moving map EuroNav 7 – RN7 (EuroAvionics), GSM / UMTS 0.5 1.1
module
08-46068-B E3168-300-00 Moving map EuroNav 7 – RN7 (EuroAvionics), FLARM module 0.6 1.3
08-46068-B E3168-600-00 Moving map EuroNav 7 – RN7 (EuroAvionics), weather radar 0.0 0.0
interface
08-46070-A E3169-000-00 Moving map - Helionixj 0.0 0.0 G
08-65068-B E2461-001-00 Electrical fixed provisions, 5 VDC, copilot 0.6 1.3
08-65068-B E3315-302-00 iPad mini holder, pilot 0.6 1.3
08-65068-B E3315-301-00 iPad mini holder, copilot 0.6 1.3
08-65068-B E3315-401-00 iPad Air holder, copilot 0.7 1.5
08-81046-C E3132-000-10 Cockpit Voice and Flight Data Recorder (CVFDR), fixed 3.3 7.3 G
provisions
08-81046-C E3132-000-20 Cockpit Voice and Flight Data Recorder (CVFDR), detachable 4.7 10.4 G
partsk
08-83047-A E3171-000-10 Health Monitoring System (HMS), fixed provisions 3.1 6.8
08-83047-A E3171-000-20 Health Monitoring System (HMS), detachable parts 2.7 6.0
08-83048-A E3171-200-00 Professional Ground Station (PGS) Vision Systeml GSE GSE G
m
08-83049-A E3171-100-00 Helicopter Flight Data Monitoring (HFDM) GSE GSE G
a. incl. auto-activation.
b. Onboard HF/tact. radio transm. can influence radio nav systems (MKR, VOR, ILS, ADF) and com systems (VHF/other tact.
radio). Depending on NAA cert. requirements, such systems must either be turned off during IFR approaches/departures or
deactivated.
c. 50 VA
d. Hoist operation & maintenance training included. Details are provided in the respective documentation.
e. Mirror detachable parts have to be removed for CAT A VTOL takeoff and landings.
f. Operator to equip ELT(S) meeting ICAO Annex 10 requirements to comply with EASA OPS.
g. Onboard HF/tact. radio transm. can influence radio nav systems (MKR, VOR, ILS, ADF) and com systems (VHF/other tact.
radio). Depending on NAA cert. requirements, such systems must either be turned off during IFR approaches/departures or
deactivated. Export clearance needs to be clarified by Airbus helicopters sales representative.
h. Without integration and EASA certification of LTE phone.
i. incl. 512 GB flashdisk and Global Map Package
j. The database update service is provided under a dedicated service contract. Please contact your Airbus helicopter sales
representative for further information.
k. Ground station not included.
l. Recommended 1 per customer base if CVFDR is selected.
m. Instead of PGS Vision System

46 135 T3H/P3H 18.ACH.01 E

5.2 Avionics Layout

Single / Dual Pilot IFR with dual GTN 750 (Garmin)

1. GPS / NAV / COM GTN 750

(Garmin), pilot
2. Audio Control Panel ACP53
(Cobham), pilot
3. Cockpit Control Panel (CCP)
4. Data Transfer Device (DTD)
5. Audio Control Panel ACP53
(Cobham), copilot
6. GPS / NAV / COM GTN 750
(Garmin), copilot
7. Flight Display Subsystem
(FDS, copilot

Figure 5.1: Single / Dual Pilot IFR GTN 750 (Garmin)

Qty Document Commercial Description kg lb

Reference Reference
1 08-00447-A E2300-120-00 Avionics Package DP IFR GC GTN 750 0.0 0.0
1 08-16164-C E2341-000-00 Digital Audio Control System (DACS), incl. ACP53 (Cobham), 5.8 12.8
pilot + copilot
1 08-22083-A E3451-000-00 Transponder GTX 335R (Garmin)a 2.4 5.3
1 08-25519-A E3455-000-00 Distance Measuring Equipment (DME) DME-4000 2.6 5.7
(Rockwell Collins)
1 08-26063-A E3431-000-00 Marker beacon receiver MKR3300-1 (Becker) 1.2 2.6
b
1 08-43077-C E3463-001-00 GPS/NAV/COM GTN 750 (Garmin), copilot 6.9 15.2
1 08-43077-C E3463-002-00 GPS/NAV/COM GTN 750 (Garmin), pilotb 8.2 18.1
1 08-65054-A E3161-001-00 Flight Display Subsystem (FDS), copilot 5.5 12.1
1 08-99005-B E0000-151-00 Avionics Package DP IFR GTN Series interconnection / wiring 23.5 51.8
a. incl. ADS-B out.
b. SBAS RNP approach local service availability verification through your Airbus helicopter sales representative on request.

135 T3H/P3H 18.ACH.01 E 47

Single Pilot IFR with dual GTN 750 (Garmin)

1. GPS / NAV / COM GTN 750

Figure 5.2: Single Pilot IFR GTN 750 (Garmin)

Qty Document Commercial Description kg lb

Reference Reference
1 08-00452-A E2300-122-00 Avionics Package SP IFR GC GTN 750 0.0 0.0
1 08-16164-C E2341-000-00 Digital Audio Control System (DACS), incl. ACP53 (Cobham), 5.8 12.8
pilot + copilot
1 08-22083-A E3451-000-00 Transponder GTX 335R (Garmin)a 2.4 5.3
1 08-25519-A E3455-000-00 Distance Measuring Equipment (DME) DME-4000 (Rockwell 2.6 5.7
Collins)
1 08-26063-A E3431-000-00 Marker beacon receiver MKR3300-1 (Becker) 1.2 2.6
1 08-43077-C E3463-001-00 GPS/NAV/COM GTN 750 (Garmin), copilotb 6.9 15.2
1 08-43077-C E3463-002-00 GPS/NAV/COM GTN 750 (Garmin), pilotb 8.2 18.1
1 08-99005-B E0000-152-00 Avionics Package SP IFR GTN Series interconnection / wiring 23.5 51.8
a. incl. ADS-B out.
b. SBAS RNP approach local service availability verification through Airbus Helicopters on request.

48 135 T3H/P3H 18.ACH.01 E

5.3 Antenna Layout

1. ELT antenna 6. FM Antenna 11. ATC antenna

2. VOR / ILS antenna 7. IRIDIUM antenna 12. Marker antenna
3. VHF / AM 2 antenna 8. TETRA antenna 13. DME antenna
4. GPS 2 antenna 9. Radar altimeter antenna 14. VHF-AM 1 antenna
5. GPS 1 antenna 10. ADF antenna

Figure 5.3: Typical IFR antenna layout

135 T3H/P3H 18.ACH.01 E 49

5.4 Disclaimers

EASA-OPS
Please note that some recommended mission configurations include equipment requested by EASA-
OPS. They do not cover oxygen equipment and the entire equipment required for extended over water
or offshore operations. The operator shall contact his national authority for the approval of the planned
aircraft mission configuration.

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.

50 135 T3H/P3H 18.ACH.01 E

6 Main Performance

The performance figures shown hereafter are guaranteed minimum performance data (minimum
specification engine power). Only the fuel consumption, range and endurance values and figures refer
to an ACH135 equipped with minimum specified new production engines.
Unless otherwise specified, the values and figures refer to a clean helicopter configuration at Sea Level
(SL), in International Standard Atmosphere (ISA) and zero wind condition.

6.1 Performance Summary Tables

All Engine Operative (AEO) - Altitude, Rate of Climb

Pratt & Whitney Canada PW206B3, standard air intake

kg 2,720 2,835 2,910 2,980

lb 5,997 6,250 6,415 6,570
Hover ceiling IGE (4 ft AGL), TOPa
• ISA m 4,816 4,465 4,237 4,039
ft 15,800 14,650 13,900 13,250
• ISA + 20°C m 4,084 3,719 3,490 3,277
ft 13,400 12,200 11,450 10,750
Hover ceiling OGE, TOPa
• ISA m 4,084 3,429 2,896 2,195
ft 13,400 11,250 9,500 7,200
• ISA +20°C m 3,261 2,880 2,484 1,844
ft 10,700 9,450 8,150 6,050
Service ceiling, MCP (climb reserve 200 ft/min)a
• ISA m 5,410 5,121 4,938 4,770
ft 17,750 16,800 16,200 15,650
• ISA +20°C m 4,541 4,267 4,100 3,962
ft 14,900 14,000 13,450 13,000
Rate of climb, TOP, VY = 65 KIASa m/s 9.5 8.8 8.3 7.9
ft/min 1,870 1,730 1,640 1,560
a. Preliminary performance data.

135 T3H/P3H 18.ACH.01 E 51

All Engine Operative (AEO) - Speed, Fuel Consumption, Range

Pratt & Whitney Canada PW206B3, standard air intake

kg 2,720 2,835 2,910 2,980

lb 5,997 6,250 6,415 6,570
Maximum speed (VNE)a, at IAS km/h 259 259 259 259
kts 140 140 140 140
Fast cruise speed (VH)a, at TAS km/h 257 255 253 252
kts 139 138 137 136
Fuel consumption at fast cruise speeda kg/h 229 229 229 229
lb/h 505 505 505 505
Best range speed (VBR)a, at IAS km/h 248 248 246 246
kts 134 134 133 133
Fuel consumption at best range speeda kg/h 220 221 222 223
lb/h 485 487 489 492
Fuel consumption at 65 KIASa kg/h 156 159 161 163
lb/h 344 351 355 359
Maximum range at best range speed (no reserve)a
• Standard fuel tank (560.4 kg) km 646 641 637 633
NM 349 346 344 342
• Standard and long range fuel tank (730.6 kg) km 846 841 837 832
NM 457 454 452 449
Maximum endurance at 65 KIAS (no reserve)a
• Standard fuel tank (560.4 kg) h:min 3:46 3:42 3:39 3:36
• Standard and long range fuel tank (730.6 kg) h:min 4:58 4:53 4:49 4:46
a. Preliminary performance data

All Engine Operative (AEO) - Speed, Fuel Consumption, Range at 5,000 ft

Pratt & Whitney Canada PW206B3, standard air intake

kg 2,720 2,835 2,910 2,980

lb 5,997 6,250 6,415 6,570
Fast cruise speed (VH)a, at TAS km/h 263 259 256 254
kts 142 140 138 137
Fuel consumption at fast cruise speeda kg/h 219 219 219 219
lb/h 483 483 483 483
Best range speed (VBR)a, at IAS km/h 222 222 224 224
kts 120 120 121 121
Fuel consumption at best range speeda kg/h 194 198 203 205
lb/h 428 437 448 452

52 135 T3H/P3H 18.ACH.01 E

kg 2,720 2,835 2,910 2,980

lb 5,997 6,250 6,415 6,570
Fuel consumption at 65 KIASa kg/h 144 147 150 153
lb/h 317 324 331 337
Maximum range at best range speed (no reserve)a
• Standard fuel tank (560.4 kg) km 719 707 700 691
NM 388 382 378 373
• Standard and long range fuel tank (730.6 kg) km 946 932 920 913
NM 511 503 497 493
Maximum endurance at 65 KIAS (no reserve)a
• Standard fuel tank (560.4 kg) h:min 4:07 4:01 3:57 3:54
• Standard and long range fuel tank (730.6 kg) h:min 5:26 5:19 5:15 5:10
a. Preliminary performance data

One Engine Inoperative (OEI) - Altitude, Rate of Climb

Pratt & Whitney Canada PW206B3, standard air intake

kg 2,720 2,835 2,910 2,980

lb 5,997 6,250 6,415 6,570
Service ceiling, MCP (climb reserve 100 ft/min)a
• ISA m 3,930 3,570 3,440 3,200
ft 12,900 11,700 11,300 10,500
• ISA +20°C m 3,140 2,740 2,620 2,190
ft 10,300 9,000 8,600 7,200
• Rate of climb, MCP, VY = 65 KIASa m/s 2.8 2.3 2.1 1.8
ft/min 560 460 410 350
a. Preliminary performance data

One Engine Inoperative (OEI) - Maximum Gross Mass

Pratt & Whitney Canada PW206B3, standard air intake

ISA ISA +20°C

Hover OGE, 30 s power (NR 100%)a kg 2725 2,665

lb 6008 5,875
Hover OGE, 2 min power (NR 102%)a kg 2,710 2,555
lb 5,975 5,633
Hover OGE, 2 min power, 10 kts headwind (NR 102%)a kg 2,755 2,600
lb 6,074 5,732
Hover IGE (4 ft AGL), 2 min power (NR 102%)a kg 2,965 2,810
lb 6,537 6,195
Category A - VTOL, surface level and elevateda kg 2,980 2,950
lb 6,570 6,504
Category A - VTOL, short fielda kg 2,980 2,950
lb 6,570 6,504
a. Preliminary performance data.

135 T3H/P3H 18.ACH.01 E 53

All Engine Operative (AEO) - Altitude, Rate of Climb

Pratt & Whitney Canada PW206B3, Inlet Barrier Filter (IBF)

kg 2,720 2,835 2,910 2,980

lb 5,997 6,250 6,415 6,570
Hover ceiling IGE (4 ft AGL), TOPa
• ISA m 4,724 4,343 4,115 3,901
ft 15,500 14,250 13,500 12,800
• ISA + 20°C m 3,932 3,551 3,322 3,109
ft 12,900 11,650 10,900 10,200
Hover ceiling OGE, TOPa
• ISA m 3,993 3,429 2,880 2,195
ft 13,100 11,250 9,450 7,200
• ISA +20°C m 3,139 2,743 2,454 1,829
ft 10,300 9,000 8,050 6,000
Service ceiling, MCP (climb reserve 200 ft/min)a
• ISA m 5,335 5,045 4,845 4,680
ft 17,500 16,550 15,900 15,350
• ISA +20°C m 4,420 4,145 3,995 3,780
ft 14,500 13,600 13,100 12,400
Rate of climb, TOP, VY = 65 KIASa m/s 9.5 8.8 8.3 7.9
ft/min 1,870 1,730 1,640 1,560
a. Preliminary performance data.

All Engine Operative (AEO) - Speed, Fuel Consumption, Range

Pratt & Whitney Canada PW206B3, Inlet Barrier Filter (IBF)

kg 2,720 2,835 2,910 2,980

54 135 T3H/P3H 18.ACH.01 E

kg 2,720 2,835 2,910 2,980

lb 5,997 6,250 6,415 6,570
Fuel consumption at 65 KIASa kg/h 159 162 164 166
lb/h 350 357 362 367
Maximum range at best range speed (no reserve)a
• Standard fuel tank (560.4 kg) km 643 637 632 626
NM 347 344 341 338
• Standard and long range fuel tank (730.6 kg) km 839 833 828 824
NM 453 450 447 445
Maximum endurance at 65 KIAS (no reserve)a
• Standard fuel tank (560.4 kg) h:min 3:44 3:40 3:37 3:34
• Standard and long range fuel tank (730.6 kg) h:min 4:56 4:50 4:47 4:43
a. Preliminary performance data

All Engine Operative (AEO) - Speed, Fuel Consumption, Range at 5,000 ft

Pratt & Whitney Canada PW206B3, Inlet Barrier Filter (IBF)

kg 2,720 2,835 2,910 2,980

lb 5,997 6,250 6,415 6,570
Fast cruise speed (VH)a, at TAS km/h 263 259 256 254
kts 142 140 138 137
Fuel consumption at fast cruise speeda kg/h 221 221 221 221
lb/h 487 487 487 487
Best range speed (VBR)a, at IAS km/h 222 222 224 224
kts 120 120 121 121
Fuel consumption at best range speeda kg/h 196 200 205 207
lb/h 432 441 452 456
Fuel consumption at 65 KIASa kg/h 145 149 152 154
lb/h 320 328 335 340
Maximum range at best range speed (no reserve)a
• Standard fuel tank (560.4 kg km 711 700 693 685
NM 384 378 374 370
• Standard and long range fuel tank (730.6 kg) km 937 922 913 904
NM 506 498 493 488
Maximum endurance at 65 KIAS (no reserve)a
• Standard fuel tank (560.4 kg) h:min 4:04 3:59 3:55 3:52
• Standard and long range fuel tank (730.6 kg) h:min 5:23 5:16 5:12 5:07
a. Preliminary performance data

135 T3H/P3H 18.ACH.01 E 55

One Engine Inoperative (OEI) - Altitude, Rate of Climb

Pratt & Whitney Canada PW206B3, Inlet Barrier Filter (IBF)

kg 2,720 2,835 2,910 2,980

lb 5,997 6,250 6,415 6,570
Service ceiling, MCP (climb reserve 100 ft/min)a
• ISA m 3,750 3,320 3,080 2,960
ft 12,300 10,900 10,100 9,700
• ISA +20°C m 2,870 2,380 2,040 1,740
ft 9,400 7,800 6,700 5,700
• Rate of climb, MCP, VY = 65 KIASa m/s 2.8 2.3 2.1 1.8
ft/min 560 460 410 350
a. Preliminary performance data.

One Engine Inoperative (OEI) - Maximum Gross Mass

Pratt & Whitney Canada PW206B3, Inlet Barrier Filter (IBF)

ISA ISA +20°C

Hover OGE, 30 s power (NR 100%)a kg 2725 2,660

lb 6008 5,864
Hover OGE, 2 min power (NR 102%)a kg 2,710 2,515
lb 5,975 5,545
Hover OGE, 2 min power, 10 kts headwind (NR 102%)a kg 2,755 2,560
lb 6,074 5,644
Hover IGE (4 ft AGL), 2 min power (NR 102%)a kg 2,965 2,760
lb 6,537 6,085
Category A - VTOL, surface level and elevateda kg 2,980 2,950
lb 6,570 6,504
Category A - VTOL, short fielda kg 2,980 2,950
lb 6,570 6,504
a. Preliminary performance data.

56 135 T3H/P3H 18.ACH.01 E

All Engine Operative (AEO) - Altitude, Rate of Climb

Safran Helicopter Engines Arrius 2B2plus, standard air intake

kg 2,720 2,835 2,910 2,980

lb 5,997 6,250 6,415 6,570
Hover ceiling IGE (4 ft AGL), TOP
• ISA m 4,880 4,495 4,265 4,025
ft 16,000 14,750 14,000 13,200
• ISA + 20°C m 4,025 3,595 3,352 3,065
ft 13,200 11,800 11,000 10,050
Hover ceiling OGE, TOP
• ISA m 4,085 3,385 2,865 2,195
ft 13,400 11,100 9,400 7,200
• ISA +20°C m 3,048 2,575 2,315 1,830
ft 10,000 8,450 7,600 6,000
Service ceiling, MCP (climb reserve 200 ft/min)
• ISA m 5,625 5,335 5,150 4,985
ft 18,450 17,500 16,900 16,350
• ISA +20°C m 4,755 4,450 4,300 4,145
ft 15,600 14,600 14,100 13,600
Rate of climb, TOP, VY = 65 KIAS m/s 9.5 8.8 8.3 7.9
ft/min 1,870 1,730 1,640 1,560

All Engine Operative (AEO) - Speed, Fuel Consumption, Range

Safran Helicopter Engines Arrius 2B2plus, standard air intake

kg 2,720 2,835 2,910 2,980

lb 5,997 6,250 6,415 6,570
Maximum speed (VNE), at IAS km/h 259 259 259 259
kts 140 140 140 140
Fast cruise speed (VH), at TAS km/h 257 255 253 252
kts 139 138 137 136
Fuel consumption at fast cruise speed kg/h 230 230 230 230
lb/h 507 507 507 507
Best range speed (VBR), at IAS km/h 250 250 250 250
kts 135 135 135 135
Fuel consumption at best range speed kg/h 223 225 227 228
lb/h 492 495 500 503
Fuel consumption at 65 KIAS kg/h 165 168 170 172
lb/h 363 370 374 378
Maximum range at best range speed (no reserve)
• Standard fuel tank (560.4 kg) km 625 621 617 614
NM 337 335 333 332
• Standard and long range fuel tank (730.6 kg) km 823 817 813 810
NM 444 441 439 437
Maximum endurance at 65 KIAS (no reserve)
• Standard fuel tank (560.4 kg) h:min 3:28 3:24 3:22 3:20
• Standard and long range fuel tank (730.6 kg) h:min 4:36 4:31 4:28 4:26

135 T3H/P3H 18.ACH.01 E 57

All Engine Operative (AEO) - Speed, Fuel Consumption, Range at 5,000 ft

Safran Helicopter Engines Arrius 2B2plus, standard air intake

kg 2,720 2,835 2,910 2,980

lb 5,997 6,250 6,415 6,570
Fast cruise speed (VH), at IAS km/h 263 259 256 252
kts 142 140 138 137
Fuel consumption at fast cruise speed kg/h 226 226 226 226
lb/h 498 498 498 498
Best range speed (VBR), at TAS km/h 230 230 230 230
kts 124 124 124 124
Fuel consumption at best range speed kg/h 196 199 202 204
lb/h 432 439 445 450
Fuel consumption at 65 KIAS kg/h 148 151 153 155
lb/h 326 333 337 342
Maximum range at best range speed (no reserve)
• Standard fuel tank (560.4 kg) km 732 722 715 709
NM 395 390 386 383
• Standard and long range fuel tank (730.6 kg) km 961 950 941 933
NM 519 513 508 504
Maximum endurance at 65 KIAS (no reserve)
• Standard fuel tank (560.4 kg) h:min 3:59 3:54 3:51 3:48
• Standard and long range fuel tank (730.6 kg) h:min 5:14 5:09 5:03 5:02

58 135 T3H/P3H 18.ACH.01 E

One Engine Inoperative (OEI) - Altitude, Rate of Climb

Safran Helicopter Engines Arrius 2B2plus, standard air intake

kg 2,720 2,835 2,910 2,980

lb 5,997 6,250 6,415 6,570
Service ceiling, MCP (climb reserve 100 ft/min)
• ISA m 4,025 3,640 3,415 3,200
ft 13,200 11,950 11,200 10,500
• ISA +20°C m 3,260 2,790 2,470 2,150
ft 10,700 9,150 8,100 7,050
Rate of climb, MCP, VY = 65 KIAS m/s 2.8 2.3 2.0 1.8
ft/min 560 460 400 350

One Engine Inoperative (OEI) - Maximum Gross Mass

Safran Helicopter Engines Arrius 2B2plus, standard air intake

ISA ISA +20°C

Hover OGE, 30 s power (NR 100%) kg 2725 2,665

lb 6008 5,875
Hover OGE, 2 min power (NR 102%) kg 2,710 2,545
lb 5,975 5,611
Hover OGE, 2 min power, 10 kts headwind (NR 102%) kg 2,750 2,600
lb 6,063 5,732
Hover IGE (4 ft AGL), 2 min power (NR 102%) kg 2,965 2,800
lb 6,537 6,173
Category A - VTOL, surface level and elevated kg 2,980 2,950
lb 6,570 6,504
Category A - VTOL, short field kg 2,980 2,950
lb 6,570 6,504