ahuk catalogue options - airbus helicopters...ahuk-350-0003 - dual usb charging port (lhs and-or...

March 2021

HELICOPTERS

AHUK Catalogue Options

Airbus Helicopters is the world’s largest helicopter manufacturer and the company’s site at Oxford Airport is the UK

and Republic of Ireland’s civil helicopter hub for helicopters sales, customisation and support activities.

Helicopter customisation

Airbus Helicopters in the UK is committed to providing bespoke customisations and enhancements for the world’s most popular helicopters, in multiple sectors including air ambulance, police, private and business, passenger transport and military.

The AHUK Catalogue is aiming to share the most popular customisations available to our customers. We can also design and certify new options, under our Design Organisation Approval (UK.21J.0015) and our Production Organisation Approval (UK.21G.2063).

As an official Customer Centre, we have also been

recognised as an Authorised Design Organisation by

Airbus Helicopters Group.

Maintenance and Logistic centre

Additionally, the company is an approved Maintenance Repair Organisation (MRO), supported by a global supply chain supplying spare parts for the UK and Ireland region. We are committed to providing the highest level of service to ensure aircraft availability, safety and customer satisfaction.

Currently we are contracted to deliver maintenance services for the

most stringent of customers including the UK Police Air Service

(PAS), the UK Military Flying Training School (MFTS), and most of

the UK’s Air Ambulance services as well as highly demanding

private and corporate customers.

Training Services

Airbus Helicopters in the UK is an Approved Training

Organisation (GBR.ATO-0245), authorised to carry out

pilot training on Airbus Helicopters’ aircraft, whether as a

Type Rating or Recurrent Training.

We also provide Licensed Aircraft Engineer Type Ratings,

and we are authorised to conduct local Licensed Aircraft

Type Ratings on the H135 and H145, at Oxford.

Ultimately, Airbus Helicopters UK’s focus is to provide the highest level of completion, maintenance and training to

ensure customer’s safety.

Need information on our product range? Contact us at [email protected]

mailto:[email protected]

Light Single Engine

The H125 (previously named the AS350

B3e) outclasses all other single-engine

helicopters for performance, versatility,

low maintenance, and low acquisition

costs, while excelling in high and hot

and extreme environments. It is a

member of Airbus’ Ecureuil family,

which has accumulated more than 33

million flight hours worldwide.

The H125 is currently operated in the UK by the renowned Empire Test Pilot School as well as private customers.

From major tourist destinations to the

busy airspace over cities, the single-

engine H130 (previously known as the

EC130 T2) is in widespread use with

sightseeing services, charter operators

and emergency medical services,

among others.

The H130 is currently operated in the UK by private customers, for either bespoke interior definition or the latest

Aston Martin Edition

More information page 3


Light Twin Engines

Backed by experience and a long

heritage, over 1,350 twin engine H135s

have been delivered and are in service in

more than 60 countries. With more than

300 operators, these versatile aircraft

have flown 5 million hours.

The H135 is currently operated in the UK

for Police, Air Ambulance and training

operations.

The H135 is also well appreciated by worldwide by Private customers.

Designed to deliver excellent

performance throughout the flight

envelope, Airbus’ H145 is the

latest member of its 4-ton-class

twin-engine rotorcraft product

range – with designed-in mission

capability and flexibility,

especially in high and hot

operating conditions. Compact in

size, this helicopter’s small

footprint and large, flexible cabin

make it the aircraft of choice for a

variety of civil or military missions.

The H145 versatility allows the aircraft to be operated in the UK for Police, Air Ambulance Operation, Training, as

well as flown by Private customers.



AHUK-350-0001 - Instrument Panel iPad Mini Mount AHUK-350-0002 - iPad Mini Folding Mount (LHS and-or RHS) AHUK-350-0003 - Dual USB Charging Port (LHS and-or RHS) AHUK-350-0004 - Avidyne SkyTrax615 (TAS615A) Traffic Advisory System AHUK-350-0005 - Quick Release Stowage Pocket AHUK-350-0008 - Seat Back Stowage(s) AHUK-350-0009 - External Paint Scheme AHUK-350-0010 - VIP Trim Interior AHUK-350-0011 - Radar Altimeter Honeywell KRA405B AHUK-350-0012 - Fire Extinguisher Relocation AHUK-350-0014 - 2 Axis Autopilot with GPS coupling Genesys HeliSAS AHUK-350-0016 - Dual Colour LED Anti-Collision Light (HISL) RedBaron AHUK-350-0017 - Searchlight Trakka A800 AHUK-350-0019 - Wireless Connection Garmin Flight Stream 210 AHUK-350-0020 - Instrument panel PED Mount including power supply AHUK-350-0021 - GPS-NAV-COM Garmin GTN750H AHUK-350-0024 - Digital Clock Thommen CM20 AHUK-350-0025 - PowerFLARM Core Installation AHUK-350-0026 - NVG Swivelling Landing Light AHUK-350-0027 - Utility iPad Installation AHUK-350-0028 - External Grab Handles AHUK-350-0029 - Lean Instrument Panel AHUK-350-0030 - Garmin G500H TXi 10” Retrofit AHUK-350-0033 - Wi-Fi Enablement

3

AS350 / H125 Instrument panel iPad Mini Mount

Option Number:AHUK-350-0001 5 March 2021 This document is the property of Airbus Helicopters UK Ltd; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters UK Ltd and its contents shall not be disclosed.

Non-contractual pictures. Aircraft configuration might have an impact on the layout. Airbus Helicopters UK reserves the rights to make improvements, configuration and data changes at any time without notice.

The facts and figures contained in this document are expressed in good faith and do not constitute any contract with Airbus Helicopters UK.

Applicable Type Certification AS350B2 Development AS350B3 AHUK Minor Change H125 EASA STC

FAA STC

Description: Instrument panel iPad Mini Mount

Reference: AHUK-350-0001

The Instrument Panel iPad Mini Mount is a recessed stowage located in the LHS instrument panel.

The mount includes a recessed housing assembly and a spring loaded cradle to ensure secure stowage and retention of the iPad Mini.

The spring loaded cradle means that fitment and removal of the iPad Mini is simple and quick.

Due to the recessed housing once the iPad Mini is fitted to the mount it provides a flush finish ensuring a visually stunning cockpit installation.

The modification requires a rework of the central panel.

Compatible with Universal iPad Mini

Key Benefits: Pre/Post Requisites & Effectivity: Secure quick fit/release system. Flush mount for great cockpit finish.

Instrumentation and lighting platemodifications are required.

Total Mass Kg

X Axis Moment m.kg

Y Axis Moment m.kg

Electrical Load (Max)

Aircraft Downtime

0.62 0.59 0.11 N/A 5 days Data based on configuration 1 without any option selected.

AS350 / H125 Instrument panel iPad Mini Mount




Configuration / Option Matrix:

Configuration In

stru

men

t Pa

nel

1 ●

Key: ● Required□ Option─ Not Applicable

Notes:

Configuration / Kit Matrix:

Configuration Kit Number Description 1 AHUK3502122-200-01 Instrument Panel iPad Mini Mount (Inc. Instrument panel mod).

Typical Installation time: - Airframe, structure 60 Hr- Avionic, Electric 15 Hr

Price On request Price(s) based on configuration 1 without any option selected.

AS350 / H125 iPad Mini Folding Mount (LHS and-or RHS)





FAA STC

Description: iPad Mini Folding Mount (LHS and-or RHS)


The Folding iPad Mini Mount is installed outboard of the instrument panel glare shield. The mount consists of a bracket assembly and spring loaded cradle.

The spring loaded cradle ensures secure stowage and retention of the iPad Mini. The spring loaded mechanism means fitment and removal of the iPad Mini is simple, quick and there is no need for tooling or locking keys.

The bracket assembly enables the user to “fold-out” the iPad and then retains it in position for viewing, access and touchscreen control. With an applied force, the bracket will “fold-in” and stows adjacent to the instrument panel glare shield enabling pilot and co-pilot unrestricted view out of the cockpit.

Compatible with Universal iPad Mini

Key Benefits: Pre/Post Requisites & Effectivity: Folds for unrestricted cockpit view Cost effective LHS and RHS Solution

None

Total Mass Kg

X Axis Moment m.kg

Y Axis Moment m.kg


Aircraft Downtime S/B & Kit

0.39 0.37 -0.23 N/A 2 days Available Data based on configuration 1 without any option selected.

AS350 / H125 iPad Mini Folding Mount (LHS and-or RHS)





Configuration C

opilo

t Gla

re

shie

ld fo

ldin

g m

ount

.

Pilo

t Gla

re

shie

ld fo

ldin

g m

ount

1 ● □ 2 □ ●


Notes:


Configuration Kit Number Description 1 AHUK3502122-205-05 Folding iPad Mini Mount (LHS) 2 AHUK3502122-205-06 Folding iPad Mini Mount (RHS)


Price: On request Price(s) based on configuration 1 without any option selected.

AS350 / H125 Dual USB Charging Port (LHS and-or RHS)




Applicable Type Certification AS350B2 Development AS350B3 AHUK Minor Change H125 EASA STC FAA STC Description: Dual USB Charging Port (LHS and-or RHS)

Reference: AHUK-350-0003 The Dual USB Charging Port converts the aircraft electrical input to a standard 5V power for any electronic product that charges using a USB connector. The two Universal Serial Bus-A (USB-A) ports can be mounted in a variety of locations throughout the aircraft cockpit and cabin. As a high power dedicated charging port the system can provide up to 2.1A of power to charge any USB device including the higher demand products. The Dual USB Charging Port can provide 2.1A of power to both ports simultaneously.

The unit features short circuit protection, over-current protection, low voltage shut-down and temperature monitoring making it ideal for any application. The Dual USB is linked to the master switch, for maximum convenience, and can also be mounted on the collective housing of the pilot.

Key Benefits: Pre/Post Requisites & Effectivity: Charge any USB electrical device. Lightweight, Small and versatile.

None

Total Mass Kg

X Axis Moment m.kg

Y Axis Moment m.kg


Aircraft Downtime S/B & Kit

0.09 0.09 0.05 0.85A 5 days Available Data based on configuration 1 without any option selected.

AS350 / H125 Dual USB Charging Port (LHS and-or RHS)





Configuration LH

S G

lare

sh

ield

(Glo

ve

Box)

Pilo

t Pow

er

Switc

h

RH

S G

lare

sh

ield

LHS

USB

–

Exte

nded

in

stru

men

t pa

nel

AHU

K co

ntro

l sw

itch

1 ● ● □ - -2 □ ● ● - -3 - - - ● ●


Notes:


Configuration Kit Number Description 1 AHUK3503106-101-04 Dual USB Charging Port (LHS Glare Shield / Glove Box) 2 AHUK3503106-101-05 Dual USB Charging Port (RHS Glare Shield) 2 AHUK3503188-205-01 Dual USB Charging Port (Extended instrument panel)

Typical Installation time: - Airframe, structure 7 Hrs- Avionic, Electric 15 Hrs


AS350 / H125 Avidyne SkyTrax615 (TAS615A) Traffic Advisory

System




Applicable Type Certification AS350B2 Development AS350B3 AHUK Minor Change H125 EASA STC FAA STC Description: Avidyne SkyTrax615 (TAS615A) Traffic Advisory System

Reference: AHUK-350-0004 The SkyTrax600 (TAS6XXA) Series Traffic Advisory System combines active with passive ADS-B traffic information to provide a hybrid solution for identifying potential collision threats. The SkyTrax600 Series system comprises of the following main components; a processor, a transponder coupler, a single blade antenna, a dual blade antenna and a display. The system is also installed with a “Mute” switch. The Traffic Advisory System can be interfaced to a multitude of different displays.

The SkyTrax615A (TAS615A) has an Active range of 17nm and ADS-B range of 30nm. The system can display a maximum of 30 targets. In addition, the SkyTrax620A (TAS620A) is also available, and has an Active range of 20nm and ADS-B range of 40nm. The system can display a maximum of 30 targets.

Displayed on: G500H/GTN/GNS depending of the aircraft configuration. The Traffic Advisory system provides three levels of alert, so pilots can monitor traffic before it ever becomes a threat. The modification includes the upper VHF antenna relocation.

Key Benefits: Pre/Post Requisites & Effectivity: Detection of potential collision threats. Lightweight Graphical overlay with many display options. ADS-B IN compatible

Transponder and Altitude Encoder required.

Total Mass Kg

X Axis Moment m.kg

Y Axis Moment m.kg


Aircraft Downtime

7.99 30.73 0.56 1.00A 7 days

Data based on configuration 1 without any option selected.

Display solutions most commonly used

AS350 / H125 Avidyne SkyTrax615 (TAS615A) Traffic Advisory

System





Configuration Av

idyn

e TA

S615

Avid

yne

TAS6

15A

GN

S D

ispl

ay

GTN

Dis

play

MH

D D

ispl

ay

G50

0H D

ispl

ay

Avid

yne

TAS6

20A

1 ─ ● ─ ● ─ ● ─2 ─ ─ ─ ● □ ● ● 3 ─ ● ─ ● □ ─ ─4 ● ─ ─ ● □ □ ─5 ● ─ ● ─ □ ─ ─


Notes: [1] AHUK installs an ADS-B IN compatible system. The ADS-B IN functionality is not installed.[2] Certification with the Garmin G500H TXi avionics suite is pending.


Configuration Kit Number Description 1 AHUK3503037-201-05 TAS615A - G500H and GTN650H 2 AHUK3503037-201-04 TAS620A - G500H and GTN650H 3 AHUK3503037-201-03 TAS615A - GTN650H 4 AHUK3503037-201-01 TAS615 - GTN650H 5 AHUK3502143-200-01 TAS615 - GNS430

Typical Installation time: - Airframe, structure - Hr- Avionic, Electric - Hr


AS350 / H125 Quick Release Stowage Pocket





FAA STC

Description: Quick Release Stowage Pocket


The Stowage Pocket is installed outboard adjacent to the Pilot seat. The Stowage can be used for maps, documents and/or any other small item.

The quick release system consists of a camloc quarter-turn fastener which enables the stowage pocket to be removed from the aircraft without tooling and retaining only stowage feet.

AHUK offers the replacement of the existing map stowage pocket inboard of the Co-pilot seat with a quick release solution.

Key Benefits: Pre/Post Requisites & Effectivity: Increased stowage inside the cabin. Quick release for removal without tooling.

Pilot’s stowage may require fire extinguisherrelocation.

Total Mass Kg

X Axis Moment m.kg

Y Axis Moment m.kg


Aircraft Downlink

1.35 2.29 0.84 N/A 3 days Data based on configuration 1 without any option selected.

AS350 / H125

Quick Release Stowage Pocket





Configuration Pi

lot S

tow

age

Pock

et

CoP

ilot

Stow

age

Pock

et

Rel

ocat

ion

of

Fire

Ex

tingu

ishe

r

1 ● ─ ●[1] / □[2] 2 □ ● ─

Key:

● Required □ Option ─ Not Applicable

Notes:

[1] If the aircraft fire extinguisher is located adjacent to the pilot seat then it must be relocated. [2] Relocation of the Fire Extinguisher is detailed in the AHUK Option AHUK-350-0012.


Configuration Kit Number Description 1 ECUK3502107-207-01 Pilot Stowage Pocket 2 ECUK3502107-207-02 Co-pilot Stowage Pocket

Typical Installation time: - Airframe, structure - Hr

- Avionic, Electric - Hr


AS350 / H125 Seat Back Stowage(s)




Applicable Type Certification AS350B2 Development AS350B3 AHUK Minor Change H125 EASA STC FAA STC Description: Seat Back Stowage(s)

Reference: AHUK-350-0008 The custom seat back stowage pocket can be installed to the rear of the Pilot and/or Co-pilot seat. The pocket is finished with specific material and colours to match the aircraft cabin interior. The stowage pocket has a zipped enclosure and additional slip pocket on the front.

The main stowage pocket is approximately 330mm (h) x 290mm (w) x 60mm (d) and is ideal for storing paperwork, documentation and other small devices.

Key Benefits: Pre/Post Requisites & Effectivity: Additional Storage. Different Finishes to suit aircraft interior.

None

Total Mass Kg

X Axis Moment m.kg

Y Axis Moment m.kg


Aircraft Downtime

Negligible Negligible Negligible N/A 1 day


AS350 / H125 Seat Back Stowage(s)





Configuration Pi

lot S

eat B

ack

Stow

age

Cop

ilot S

eat

Back

Sto

wag

e

1 □ □

Key:


Notes:


Configuration Kit Number Description 1 MHL3501236-508-01 Stowage Pocket

Typical Installation time: - Airframe, structure: - Hrs

- Avionics, Electrical: - Hrs


AS350 / H125 External Paint Scheme





FAA STC

Description: External Paint Scheme


Freedom is key! The customer is free to explore their creativity and develop the bespoke design and paint scheme of their dreams.

Airbus Helicopters UK are on hand to assist with the concept, design and completion every step of the way.

Key Benefits: Pre/Post Requisites & Effectivity: Customer defined None

Total Mass Kg

X Axis Moment m.kg

Y Axis Moment m.kg


Aircraft Downtime

Varies Negligible Negligible N/A 20 days Data based on configuration 1 without any option selected.

AS350 / H125 External Paint Scheme





Configuration 3

Col

our P

aint

Sc

hem

e

1 ●

Key:


Notes:


Configuration Kit Number Description 1 Bespoke External Paint Scheme (Three Colour Non-Metallic)

Typical Installation time: - Airframe, structure: N/A

- Avionics, Electrical: N/A

Price: On request

Price(s) based on configuration 1 without any option selected.

AS350 / H125

VIP Trim Interior




Applicable Type Certification AS350B2 Development AS350B3 AHUK Minor Change H125 EASA STC FAA STC Description: VIP Trim Interior

Reference: AHUK-350-0010 Freedom is key! The customer is free to explore their creativity and develop the bespoke design and cabin interior of their dreams. The VIP interior trim includes: Refurbish in leather 5 or 6 place seating,

including the armrests (only for 5 seats). Install carpet with bound edges, sewn in heel

pads, and drugget for the rear seating position Carpet in the rear baggage bay compartments Interior door and baggage door painted 2 seat back stowage on the crew seats Door interior panel and luggage bay painted

AHUK are on hand to assist with the concept, design and completion every step of the way.

Cover lining panels in leather/ultra-leather: - Cockpit and passenger doors trim panels - Cockpit overhead trim panel - Rear trim panel/Bulkhead - Cabin overhead trim panel - Instrument panel covered in mirage plus

New placards with a metallic brush finishing

The customer is free to choose the leather colours, stitching pattern and stitching colour.

Key Benefits: Pre/Post Requisites & Effectivity: Customer defined 3 places instead of 4 places transformation kit

Total Mass Kg

X Axis Moment m.kg

Y Axis Moment m.kg


Aircraft Downtime

Varies Varies Varies N/A 7 days


Lining panels covers in leather/ultra-leather

Bespoke pattern on backrest

Twin stich on the outer line

Carpet with bound edges

AS350 / H125

VIP Trim Interior





Configuration St

anda

rd V

.I.P

Inte

rior T

rim

1 ●

Key:


Notes:

[1] The placards needs to meet the contrast regulation criteria.


Configuration Kit Number Description 1 Bespoke V.I.P. Interior Trim




AS350 / H125 Radar Altimeter Honeywell KRA405B

Option Number:AHUK-350-0011 21 March 2021

This document is the property of Airbus Helicopters UK Ltd; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters UK Ltd and its contents shall not be disclosed.



Applicable Type Certification AS350B2 Development AS350B3 AHUK Minor Change H125 EASA STC FAA STC Description: Radar Altimeter Honeywell KRA405B

Reference: AHUK-350-0011 The KRA405B Radar Altimeter system provides the pilot with accurate AGL (altitude above ground level) information up to 2000ft. The Radar Altimeter is available with the KNI416 expanded scale indicator for helicopter installations. The KRA405B determines the altitude above ground by transmitting a signal to the ground then processing the reflected signal. The KRA405B system has the capability of alerting the pilot when a predetermined altitude (decision height) is reached

The system comprises of a KRA405B transceiver, a KNI416 indicator, two antennas and a CM2000 Configuration module The Transceiver has both analogue and ARINC 429 outputs for increased interface capabilities including TAS, EGPWS, Autopilot etc. The Configuration module allows for pre-selected height trips values to be set for any operational requirements

Key Benefits: Pre/Post Requisites & Effectivity: Accurate AGL up to 2000ft. Selectable Decision Height. Three configurable pre-selected altitude

trips.

None

Total Mass Kg

X Axis Moment m.kg

Y Axis Moment m.kg


Aircraft Downtime

2.88 5.85 0.79 1.7A 7 days


AS350 / H125 Radar Altimeter Honeywell KRA405B

Option Number:AHUK-350-0011 22 March 2021

This document is the property of Airbus Helicopters UK Ltd; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters UK Ltd and its contents shall not be disclosed.




Configuration KN

I416

In

dica

tor

1 ● 2 ●

Key:


Notes:


Configuration Kit Number Description 1 MHL350912-200-02 Installation of Rad/Alt System (H125 non-G500H) 2 MHL350912-200-01 Installation of Rad/Alt System (AS350B3)




AS350 / H125 Fire Extinguisher Relocation




Applicable Type Certification AS350B2 Development AS350B3 AHUK Minor Change H125 EASA STC FAA STC Description: Fire Extinguisher Relocation

Reference: AHUK-350-0012 This option relocates the existing cabin fire extinguisher from the cabin floor outboard of the pilot’s seat to the inboard back upright of the co-pilot seat.

This relocation still ensures the pilot has easy and unrestricted access to the fire extinguisher whilst creating space on the cabin floor for additional stowage.

Key Benefits: Pre/Post Requisites & Effectivity: Clear cabin floor area allowing for additional

stowage None

Total Mass Kg

X Axis Moment m.kg

Y Axis Moment m.kg


Aircraft Downtime SB & Kit

N/A N/A N/A N/A 1 day On request

AS350 / H125 Fire Extinguisher Relocation





Configuration Fi

re

Extin

guis

her

Rel

ocat

ion

1 ●

Key:


Notes:


Configuration Kit Number Description

1 ECUK3502107-204-01 Fire Extinguisher Relocation




AS350 / H125 2 Axis Autopilot with GPS coupling Genesys HeliSAS




Applicable Type Certification AS350B2 Development AS350B3 AHUK Minor Change H125 EASA STC FAA STC Description: 2 Axis Autopilot with GPS coupling Genesys HeliSAS

Reference: AHUK-350-0014 The HeliSAS Autopilot and Stability Augmentation System dramatically improves safety and reduces workload for the pilot. HeliSAS ensures precise control during all modes of flight, regardless of wind conditions or shifts in weight. In situations like whiteouts or brownouts where a pilot may lose visual reference, the HeliSAS is invaluable in maintaining a safe and stable attitude. If the helicopter is inadvertently flown to an extreme attitude, releasing the cyclic when HeliSAS is engaged will automatically return the helicopter to a neutral attitude.

While the pilot may override the HeliSAS at any time with manual cyclic inputs, the attitude stabilisation and force feel features enhance handling characteristics to mitigate inadvertent cyclic control inputs that could result in dangerous attitudes.

Key Benefits: Pre/Post Requisites & Effectivity: Lightweight. Improved safety and decreased workload.

If autopilot heading hold is desired, a heading system (e.g. DG with heading bug) must be installed and active.

Total Mass Kg

X Axis Moment m.kg

Y Axis Moment m.kg


Aircraft Downtime

13.94 10.35 0.47 2.15A 15 days


AS350 / H125 2 Axis Autopilot with GPS coupling Genesys HeliSAS





Configuration G

500H

Com

pass

Sy

stem

Cob

ham

AD

AHR

S

GN

S/G

TN

Inte

rface

1 ● ─ ─ ● 2 ─ ● ● ●

Key:


Notes:

[1] AHUK Pre-Requisite for Standard Mechanical Instrumentation is for the installation of Compass System (AHUK-350-0013) and Cobham ADAHRS.

[2] The installation of the system requires to be performed by a Genesys approved centre. [3] Certification with the Garmin G500H TXi avionics suite is pending.


Configuration Kit Number Description 1 AHUK/3503035-201-03 HeliSAS 2 Axis AP (G500H - AHF) 2 AHUK/3503035-201-02 HeliSAS 2 Axis AP (Standard Mechanical Instrumentation)




AS350 / H125 Dual Colour LED Anti-Collision Light (HISL) RedBaron




Applicable Type Certification AS350B2 Development AS350B3 AHUK Minor Change H125 EASA STC FAA STC Description: Dual Colour LED Anti-Collision Light (HISL) RedBaron

Reference: AHUK-350-0016 The dual-colour HISL LED red and white anti-collision light incorporates some of the brightest LEDs available in the world today. The HISL chromaticity and intensity is compliant to all international aviation and safety standards.

The lightweight standalone HISL does not require an external power supply and is capable of a voltage input range between 18 and 36 volts. AH complete the installation of the HISL with an ON/OFF and RED/WHITE switched annunciator.

Key Benefits: Pre/Post Requisites & Effectivity: Lightweight. Cost Effective. No additional power supply.

Removal of existing Anti-Collision Light. Modification of the upper fin cap assembly

Total Mass Kg

X Axis Moment m.kg

Y Axis Moment m.kg


Aircraft Downtime

0.02 0.63 Negligible -0.8 A 7 days


AS350 / H125 Dual Colour LED Anti-Collision Light (HISL) RedBaron





Configuration H

ISL

- Dua

l C

olou

r LED

An

ti-C

ollis

ion

Ligh

t1 ●


Notes:


Configuration Kit Number Description 1 AHUK-350-3141-01 HISL - Dual Colour LED Anti-Collision Light

Typical Installation time: - Airframe, structure: - Hrs- Avionics, Electrical: - Hrs


AS350 / H125 Searchlight Trakka A800




Applicable Type Certification AS350B2 Development AS350B3 AHUK Minor Change H125 EASA STC FAA STC Description: Searchlight Trakka A800

Reference: AHUK-350-0017 The Trakka A800 Searchlight delivers a high-powered, uniform beam of light that eliminates black holes and fading and ensures optimum clarity and cover for all types of tracking and surveillance. The Searchlight is installed under the belly of the aircraft. Control of the Trakka is via the Grip Hand Controller and the Control Panel that are installed on the centre console.

The Trakka A800 searchlight includes the industries only in-flight, multi-filter solution allowing the operator to change through a maximum of six filters. Different filter options ensure enhanced performance whatever the conditions and subject matter, including NVIS.

Key Benefits: Pre/Post Requisites & Effectivity: Flywheel Filter Selection. NVG Compatible.

- None

Total Mass Kg

X Axis Moment m.kg

Y Axis Moment m.kg


Aircraft Downtime

25.12 +115.61 +3.17 43 A 15 days


Power Conditioning Interface Unit Trakka Searchlight A800

Pilot/Copilot Control Panel Grip Hand Controller

-99° Elevation ± 184° Azimuth

AS350 / H125 Searchlight Trakka A800





Configuration Tr

akka

A80

0

Grip

Han

d C

ontro

ller

Pilo

t and

Cop

ilot

Con

trol U

nit

Pilo

t Cyc

lic

Con

trol

1 ● ● ● ●

Key:


Notes:

Lamp Power: 800 Watts Luminance at 1km: 15.8 lux (maximum) Effective Beam Angle: 3.9° to 13.3° Azimuth rotation: ± 184° (non-continuous) Elevation rotation: 0° to -99° Speed Limitation: 140 knots in operation Configuration: Single pilot configuration Fixed parts: Electronic connector and associated wirings Removable parts: Trakka Gimbal and A-Frame, PCIU, Control Panel, Hand Controller STC Reference: 10068727


Configuration Kit Number Description 1 AHUK/3503185-101-01 Installation of Trakka Searchlight A800

Typical Installation time: - Airframe, structure N/A

- Avionic, Electric N/A

Price On request


AS350 / H125 Wireless Connection Garmin Flight Stream 210





FAA STC

Description: Wireless Connection Garmin Flight Stream 210


The Flight Stream 210 is a Garmin feature which allows a wireless connectivity within the aircraft between your iPad/PED device and the Garmin GTN650/GTN750 via Bluetooth.

This option allows you to prepare your flight plan and waypoints in facilities and then upload it in your GTN suite.

This option is recommended with: An iPad holder USB Charging supply GTN750 option

Key Benefits: Pre/Post Requisites & Effectivity: Comfortable flight preparation Saving time to prepare flight plan Get airborne quickly

Installation of GTN650 or GTN750

Total Mass Kg

X Axis Moment m.kg

Y Axis Moment m.kg


Aircraft Downtime

0.12 0.12 -0.04 0.06 A 2 days Data based on configuration 1 without any option selected.

AS350 / H125 Wireless Connection Garmin Flight Stream 210





Configuration In

stal

latio

n of

fli

ght S

tream

21

0

1 ●

Key:


Notes:

[1] Certification with the Garmin G500H TXi avionics suite is pending.


Configuration Kit Number Description 1 AHUK3503134-201-01 Installation of Flight Stream 210




AS350 / H125 Instrument panel PED Mount including power supply




Applicable Type Certification AS350B2 Development AS350B3 AHUK Minor Change H125 EASA STC FAA STC Description: Instrument panel PED Mount including power supply

Reference: AHUK-350-0020 The Instrument Panel Portable Electronic Device (PED) Mount is a recessed stowage located in the LHS instrument panel. The mount includes a recessed housing assembly and a spring loaded cradle to ensure secure stowage and retention of a PED. The modification includes a dedicated USB power supply which is located behind the assembly. The assembly is equipped with a mechanism allowing to tilt the screen toward the pilot. Compatible with iPad Air 9.7” or iPad Pro 11”

The spring loaded cradle means that fitment and removal of the PED is simple, quick and without. Due to the recessed housing once the PED is fitted to the mount it provides a flush finish ensuring a visually stunning cockpit installation. AHUK install a master power switch to enable the pilot to have final control over the aircraft electrical consumption. This switch also acts as an indicator to inform the crew that the PED USB port is live and ready for connection to a compatible device.

Key Benefits: Pre/Post Requisites & Effectivity: Secure quick fit/release system. Flush mount for great cockpit finish.

Instrumentation and lighting plate modifications are required.

Total Mass Kg

X Axis Moment m.kg

Y Axis Moment m.kg


Aircraft Downtime

3.87 3.59 -0.93 1.25 5 days


AS350 / H125 Instrument panel PED Mount including power supply





Configuration PE

D M

ount

9.7

”

PED

Mou

nt 1

1”

USB

Pow

er

Supp

ly

1 ● - ● 2 - ● ●

Key:


Notes:

[1] Maximum PED Details 9.7”: Weight 500g; Size 240x169.5x7.5mm (h,w,d). Power Consumption: 5V DC, 1.2 A

[2] Maximum PED Details 11”: Weight 470g; Size 250x180.5x6mm (h,w,d). Power Consumption: 5V DC, 3 A


Configuration Kit Number Description 1 AHUK3503152-201-01 Installation of LH Instrument Panel iPad 9.7” 2 AHUK3503152-202-01 Installation of LH Instrument Panel iPad 11”



Price: On Request


AS350 / H125 GPS-NAV-COM Garmin GTN750H




Applicable Type Certification AS350B2 Development AS350B3 AHUK Minor Change H125 EASA STC FAA STC Description: GPS-NAV-COM Garmin GTN750H

Reference: AHUK-350-0021 The GTN750H is a fully integrated GPS/NAV/COM solution. The 6.9" touchscreen controls and large display give you an access to high-resolution terrain mapping, graphical flight planning, geo-referenced charting, traffic display, multiple weather options, connectivity, advanced navigation, which ease the interface Pilot/Aircraft.

The modification includes the installation of the:

Multi-Bloc Centre Console Garmin GMA35 (or GMA35c) to replace the

GNC 255A and GMA 350H.

Key Benefits: Pre/Post Requisites & Effectivity: Increased screen display compared to the

GTN650 Multi-Bloc Centre Console

Total Mass Kg

X Axis Moment m.kg

Y Axis Moment m.kg


Aircraft Downtime

2.9 3.17 -0.09 2.74A 20 Days


AS350 / H125 GPS-NAV-COM Garmin GTN750H





Configuration G

TN75

0H

GM

A 35

Mul

tiblo

c C

entre

C

onso

le

GM

A 35

c

1 ● ● ● ─ 2 ● ─ ● ●

Key:


Notes:

[1] Certification with the Garmin G500H TXi avionics suite is pending.


Configuration Kit Number Description 1 AHUK/ 3503162-201-01 Garmin GTN750H as NAVCOM2 and Garmin GMA35 as ICS 2 AHUK/ 3503162-201-02 Garmin GTN750H as NAVCOM2 and Garmin GMA35c as ICS



Price On request


AS350 / H125 Digital Clock Thommen CM20




Applicable Type Certification AS350B2 Development AS350B3 AHUK Minor Change H125 EASA STC FAA STC Description: Digital Clock Thommen CM20

Reference: AHUK-350-0024 The CM20 is a 2‘’ Clock Swiss Made precision, multifunctional chronometer. The CM20 is designed according to the latest civil and military avionics standards. It has a Solid state Liquid Crystal Display (LCD) technology which provides a continuous readout using negative image for excellent visibility during all operating conditions. This digital clock is the perfect complement to a glasscockpit instrument Panel.

It features a three line display with light digits on dark background. It supports the simultaneous indication of a combination of clock- and timer-function reading. The time base is supplied by a dedicated internal power reserve to provide the timekeeping function even when the aircraft power is removed. The CM20 replaces the original TCH analogue clock.

Key Benefits: Pre/Post Requisites & Effectivity: Three line display improve the readability

compared to an analogue clock

- None

Total Mass Kg

X Axis Moment m.kg

Y Axis Moment m.kg


Aircraft Downtime

-0.02 Negligible Negligible 0.3 A 2 days


AS350 / H125 Digital Clock Thommen CM20





Configuration C

M 2

0 D

igita

l Th

omm

en C

lock

AH In

c. C

entre

co

nsol

e

GTN

750H

AH

UK-

350-

0021

ESI 2

000

AHU

K-35

0-00

22

G50

0H

Cen

tralis

atio

n

1 ● ● □ □ □

Key:


Notes:

1. Configuration 1 has been installed on the AH Inc. centre console required for the GTN750H installation (AHUK-350-0021) and the ESI 2000 (AHUK-350-0022)


Configuration Kit Number Description 1 AHUK/3503161-201-02 Installation of CM20 Digital Clock (AH Inc Centre Console)



Price On request


AS350 / H125 PowerFLARM Core Installation




Applicable Type Certification AS350B2 Development AS350B3 AHUK Minor Change H125 EASA STC FAA STC Description: PowerFLARM Core Installation

Reference: AHUK-350-0025 The PowerFLARM Core Traffic Awareness System is used mainly by light aircraft, gliders and sky divers. AHUK’s installation is covering the ADS-B IN option, which significantly reduces the risk of air-collision with gliders. The system is fitted with dual antenna system fitted on the outside of the aircraft, and the CORE module install in the avionic bay.

The installation includes a switch on the centre console to mute the alarms. Display options:

Displayed on an iPad or compatible device via Wi-Fi relay installed in the cabin

Displayed on an Air Traffic Display which requires the relocation of the ELT push button. Wi-Fi option is included

The Wi-Fi relay is located in the back of the cabin, allowing any compatible device to display the information. 3 Different AHUK solutions to display information:

Foldable iPad Mini (AHUK-350-0002) Integrated iPad (AHUK-350-0020/0027)

PED mount not included in this option

Key Benefits: Pre/Post Requisites & Effectivity: Reduce collision Range coverage: Up to 10km Receiver option

- None

Total Mass Kg

X Axis Moment m.kg

Y Axis Moment m.kg


Aircraft Downtime

1.3 0.3 3.9 0.4 A 7 days


AS350 / H125 PowerFLARM Core Installation





Configuration Po

wer

FLAR

M

Cor

e

Air T

raffi

c D

ispl

ay

(ATD

57)

ELT

push

Bu

tton

Rel

ocat

ion

iPad

or i

Pad

min

i ins

talla

tion

Wi-F

i Rel

ay

1 ● ● ● □ ● 2 ● ─ ─ □ ●

Key:


Notes:

1. This equipment is not TSO certified, therefore the information communicated by the system are indicative. The system cannot replace an approved Traffic Advisory System.

2. Airbus Helicopters does not provide the software for the embedded PED. 3. PowerFLARM with Wi-Fi Relay only is not yet certified.


Configuration Kit Number Description

1 AHUK/3503192-201-01 Installation of PowerFLARM Core on Air Traffic Display with Wi-Fi Relay 2 Awaiting certification Installation of PowerFLARM with Wi-Fi Relay Only



Price On request


AS350 / H125 NVG Swivelling Landing Light





FAA STC

Description: NVG Swivelling Landing Light


Landing Light (swivelling in elevation and azimuth) enhances safety when approaching the ground and during helicopter manoeuvres on the ground.

AHUK is offering a NVIS compliant version of the landing light with an integrated dual mode light:

400W White 200W Infra-Red

The modification reuses the existing installation and replaces the light mount and light to be NVIS compatible.

The switch located on the Collective allows switching on and off the landing light while the joystick allows controlling the orientation of the light. A dedicated indicator is installed on the instrument panel to inform the pilots.

Key Benefits: Pre/Post Requisites & Effectivity: NVIS compatibility 06-42005-00-CI LH landing light (swivelling

in elevation and azimuth)

Total Mass Kg

X Axis Moment m.kg

Y Axis Moment m.kg


Aircraft Downtime

0.85 1.68 0.31 15.5 A 5 days Data based on configuration 1 without any option selected.

AS350 / H125 NVG Swivelling Landing Light





Configuration N

VIS

Swiv

ellin

g La

ndin

g Li

ght

1 ●


Notes: 1. The modification is certified under a minor change as NVIS compatible. The NVIS certification is

under the buyer responsibility.


Configuration Kit Number Description 1 AHUK/3503196-201-01 NVIS swivelling Landing Light Retrofit



AS350 / H125 Utility iPad Installation





FAA STC

Description: Utility iPad Installation


The iPad Mount is installed on the LHS of the instrument panel. The mount consists of a bracket assembly, a spring loaded cradle, and includes a USB power supply.

The spring loaded cradle ensures secure stowage and retention of the iPad. Its mechanism ensures fitment and removal of the iPad is simple, quick and there is no need for tooling or locking keys.

The bracket assembly enables the user to orientate the iPad toward the pilot, as well as rotating it up or down.

The installation is fitted with a switch located on the centre console allowing managing the power supply.

Compatible with iPad Generation 4 & 5

Key Benefits: Pre/Post Requisites & Effectivity: Secure quick fit/release system. Adjustable to pilot’s need Supplied with a USB power supply

- None

Total Mass Kg

X Axis Moment m.kg

Y Axis Moment m.kg


Aircraft Downtime

1.88 1.75 -0.46 0.85 A 7 days Data based on configuration 1 without any option selected.

Up to 30° extension

± 15° inclination

AS350 / H125 Utility iPad Installation





Configuration PE

D M

ount

In

stal

latio

n

USB

Pow

er

supp

ly

Exte

nded

In

stru

men

t Pa

nel

1 ● ● ●

Key:


Notes:

1. iPad not included in the option 2. Certified with the extended instrument panel. A new certification would be required with the standard

instrument panel


Configuration Kit Number Description 1 AHUK/3503189-101-01 Introduction of PED mount with USB power supply (Extended)



Price On request


AS350 / H125 External Grab Handles





FAA STC

Description: External Grab Handles


The external grab handles are installed on both LHS and RHS of the aircraft on the cabin roof. This installation enables special deployment missions such as parachuting missions or special operations.

The grab handles are installed symmetricaly about the longitudinal axis of the aircraft. The handles are covered with anti slip tape which enhances grip for the user.

Key Benefits: Pre/Post Requisites & Effectivity: More flexibility for special missions Enhanced friction and grip

Interference check with other roleequipment or antennas on aircraft cabinroof.

Total Mass Kg

X Axis Moment m.kg

Y Axis Moment m.kg


Aircraft Downtime

1.4 +3.3 0 0 5 days Data based on configuration 1 without any option selected.

AS350 / H125 External Grab Handles





Configuration Ex

tern

al G

rab

Han

dle

Inst

alla

tion

1 ●


Notes:


Configuration Kit Number Description 1 AHUK/3503198-202-01 Introduction of external grab handles

Typical Installation time: - Airframe, structure - 40 Hr- Avionic, Electric - 0 Hr


AS350 / H125 Lean Instrument Panel




Applicable Type Certification AS350B2 Development AS350B3 AHUK Minor Change H125 EASA STC FAA STC Description: Lean Instrument Panel

Reference: AHUK-350-0029 The Lean Instrument Panel (LIP) for H125 is designed for unparalleled and unrestricted visibility during single-pilot VFR operations, without sacrificing on form or functionality. It is offered both as an option for new helicopters or as a retrofit to a H125. The Lean Instrument panel consists of:

Replacing the standard GDU620 with the GU700P, also known as G500H TXi 7” Replacing the standard mechanical stand-by instruments with the ESI-500 Installing 2 x dual USB on the sides of the glare shield

The resulting space-saving allows the panel to be shortened by over 0.3m, as well as saving up to 3.8kg. This option provides a significantly improved visibility and awareness for the pilot, especially looking ahead or to the front-left of the aircraft. Figure 1: LIP Size Comparison to Standard Panel

Relocated ELT Switch VEMD Central Warning

Panel

Garmin GDU 700P 7” Portrait Display

Relocated Clock

L3 ESI-500 Electronic Standby Instrument

Garmin GTN 650H

NR Gauge

Lighting Panel





The Garmin GDU 700P certified as the Primary Flight Display (PFD), offers the latest avionics technology from Garmin. This new touchscreen PFD maintain the level of integration standard of the H125 standard with Garmin products such as the GTN series or the Flight Stream option Additionally, the display can show the readout from the Thales AHV16 Radio Altimeter when installed. The 7” display provides the same PFD functionality as its 10.6” full-sized counterpart but in a much smaller package, enabling more than 0.1m to be eliminated on the pilot’s side of the panel.

The ESI-500 by L3 is a 3.5” electronic standby instrument, which displays:

Indicated Air Speed (IAS) pressure altitude vertical speed, attitude, and slip/skid,

The ESI-500 has an in-built Li-Ion battery on hot-standby, rated for at least one hour of use, to take over without interrupting the data stream.

Figure 4: Example Lean Instrument Panel

Figure 3: L3 ESI-500

Figure 2 - GDU 700P 7" Portrait PFD





The LIP comes as standard with dual USB (Types A and C) sockets on both the Left and Right of the Glare Shield. Optional iPad mounts can be fitted to each side of the instrument panel, to allow more display space. The Pilot-side mount (Right hand) is suitable to fit either a 9.7” iPad device, or a smaller iPad Mini device. The far-side mount (Left hand) is designed to accept a 10.5” iPad Pro device, in addition to the two aforementioned. Both mounts fold flush to the sides of the glare shield for take-off and landing, or for other critical mission stages. Additional options can be fitted on request, either under the ESI-500 or on the centre console.

Key Benefits: Pre/Post Requisites & Effectivity:

Glass panel instruments including Garmin GDU 700P

Weight saving over stock panel of between 2.1Kg & 3.8Kg

327mm reduction in width from stock panel Increased pilot FOV and awareness Designed with future NVG certification in

mind

- None

Total Mass Kg

X Axis Moment

m.kg Y Axis Moment

m.kg Electrical

Load (Max) Aircraft

Downtime

-2.100 to baseline

-2.247 to baseline

-0.431 to baseline Varies 4 weeks


RHS Mount for 9.7” iPad or iPad Mini LHS Mount accepts up

to 10.5” iPad Pro

Figure 5: PED mounts on the LIP






Configuration

Lean

Inst

rum

ent

Pane

l Ins

talla

tion,

w

ith L

H a

nd R

H

USB

pow

er

sock

ets

LH (<

10.5

”) PE

D

Mou

nt

RH

(<9.

7”)

PED

M

ount

Thal

es A

HV1

6 R

adio

Alti

met

er

Synt

hetic

Vis

ion

Syst

em

1 ● ● ● ● □2 ● ● ─ ● □3 ● ─ ● ● □4 ● ─ ─ ● □5 ● ● ● ─ □6 ● ● ─ ─ □7 ● ─ ● ─ □8 ● ─ ─ ─ □

Key: ● Installed□ Option─ Not Installed

Notes:


Configuration Kit Number Description 1 AHUK/3503244-101-01 LIP Installation – LH/RH PED mount / AHV16 RADALT 2 AHUK/3503244-101-02 LIP Installation – LH PED Mount/AHV16 RADALT 3 AHUK/3503244-101-03 LIP Installation – RH PED mount/AHV16 RADALT 4 AHUK/3503244-101-04 LIP Installation – AHV16 RADALT 5 AHUK/3503244-101-05 LIP Installation – LH/RH PED Mount 6 AHUK/3503244-101-06 LIP Installation – LH PED Mount 7 AHUK/3503244-101-07 LIP Installation – RH PED Mount 8 AHUK/3503244-101-08 LIP Installation only

Typical Installation time: - Airframe, structure N/A- Avionic, Electric N/A


AS350 / H125 Garmin G500H TXi 10” Retrofit


Non-contractual pictures. Aircraft configuration might have an impact on the layout. Airbus Helicopters UK reserves the rights to make improvements, configuration and data chang

ahuk catalogue options - airbus helicopters...ahuk-350-0003 - dual usb charging port (lhs and-or...

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