Heliproducts Industries Ltd can provide full installation and sales of STC optional equipment for the AS350 and AS355.

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EXTERNAL MARKINGS
Replaces all external markings (stickers) mandatory by OEM standards. The External Markings changes and replaces the Fuel Quantity and Approved fuels placard and adds two new placards, Fuel Anti-icing Additive, Fenestron gearbox oil level placards. It also eliminates some of the non required external placards which are not required by 14 CFR Part 27 airworthiness regulations. Examples of markings available:

Specifications
• Direct replacement of original OEM markings
• Provides maintenance information to ground personnel

EXTERNAL MARKINGS

Mass (kg) Negligible
Arm (m) Negligible
Approvals Canada, USA, Brazil
Part Number AHC/78R-E-34-01 (AS350C, D, D1), AHC/78R-E-34-01 (AS350B, B1, BA), AHC/78R-E-34-05 (AS350B2), AHC/78R-E-34-03 (AS350B3)
Retrofit Information TCCA# SH89-41

FAA# SH2973SW-D

ANAC Brazil# 1999S05-15 &16

SX-16 NIGHTSUN SEARCHLIGHT INSTALLATION

The Spectrolab SX-16 Nightsun® is a high-intensity (30-40 million candlepower) searchlight located at the junction with tailboom of the helicopter. The light and gimbal are mounted using a quick release assembly for fast, tool free installation and removal. This installation consists of:

  • SX-16 searchlight and mount
  • A gimbal assembly supporting the light
  • A junction box located on the shelf in the aft baggage compartment
  • A removable hand controller in the cockpit
  • Internal and external wiring, circuit breakers and connectors
  • Optional modified gimbal & Gen II control box for Spectrolink system

Specifications

  • Vertical: 0° up to 47° down
  • Horizontal: 30° right to 90° left
  • Beam width (focus): 4° to 20°
  • Lamp power output: 1600W/30 Million Cd
  • Voltage: 28 VDC

SX-16 NIGHTSUN SEARCHLIGHT

Mass (kg) 29.5 (64.62 lbs)
Arm (m) 15.16
Approvals USA
Part Number 350A82-1648-01

(INSTL, ENHANCED SX16 W/O SPECTROLINK)

350A82-1648-02

(INSTL, ENHANCED SX16 W/ SPECTROLINK)

Retrofit Information FAA# SH7011SW-D

EXTERNAL PA SPEAKER

The external public address (PA) system is designed for use on police or rescue missions, as well as for border patrol operations. This modification installs Power Sonix Inc. model PSAIR22 speaker provisions to support short-range broadcast capability. The PSAIR22 speaker assembly is mounted within the left hand intermediate chine panel and is oriented with the speaker bells directed outboard and downward. The basic aircraft’s lower intermediate cover and the demisting bleed air lines in the vicinity of the speakers are modified to accommodate the installation.

Specifications

  • The speakers allow the pilot or observer to make announcements through the PA system via the audio box
  • The system can also be used to broadcast other audio signatures, e.g. a siren
  • The PA system is activated by a switch marked ‘PA’ located on the audio panel
  • The siren is activated from the pilot’s cyclic switch
  • Nearly no impact on aircraft performance

EXTERNAL PA SPEAKER

Mass (kg) 9.07 (20.0 lb)
Arm (m) 2.15
Approvals USA
Part Number 350A73-1720-01
Retrofit Information FAA# SR09299RC-D

NORTHERN AIRBORNE TECHNOLOGY 250 WATT PUBLIC ADDRESS SYSTEM

This modification installs NAT speakers, amplifier and controller to support short-range broadcast capability. The speaker and amplifier assemblies are mounted within the left hand intermediate chine panel and the speaker assembly is oriented with the speaker bells directed outboard and downward. The PA system controller is (typically) mounted in the center pedestal area. The basic aircraft’s lower intermediate cover and the demisting bleed air lines in the vicinity of the speakers are modified to accommodate the installation.

Specifications

  • The 250W PA system is a multi-speaker package mounted externally on the lower left belly panel
  • The speakers allow the pilot or observer to make announcements through the PA system via the audio box
  • The system can also be used to broadcast other audio signatures, e.g. a siren
  • The best audio clarity in the PA mode is obtained by placing helicopter in a left hand orbit at approximately 500 ft AGL and at minimum power setting (65 kts)
  • The PA system is activated by a switch marked ‘PA’ located on the audio panel
  • The siren is activated from the pilot’s cyclic switch

NORTHERN AIRBORNE TECHNOLOGY 250 WATT PUBLIC ADDRESS SYSTEM

Mass (kg) 8.25 (18.19 lb)
Arm (m) 5.83
Approvals USA
Part Number 350A73-1724-01
Retrofit Information FAA# SR09301RC-D

SETTLING PROTECTORS

Settling Protectors help guard against sinking into snow and soft ground. The settling protectors are comprised of LH and RH pads which attach to the aft end of the landing gear skid tubes.

Benefits

  • Maintains tail rotor ground clearance
  • Easy installation and removal
  • Lightweight
  • Competitively priced

AS350/H125

AS355

AS350 B, BA, B1, B2, B3

AS355 F, F1, F2, N, NP

SETTLING PROTECTORS

Mass (kg) 4.08 (9.0 lb)
Arm (m) 4.04
Approvals Canada, USA, Mexico
Material UHMW Polyethylene
Part Number 120-500214-01
Retrofit Information TCCA# SH01-22

FAA# SR01351NY

DGAC Mexico# IA-296-2015

Notes:

  • Available for the complete AS350 series and AS355 E, F/F1 and F2 models (USA)
  • Available for the complete AS350 series and AS355 E, F/F1/F2, N, NP (Canada, Mexico)

LEFT HAND (LH) LITTER

The LH Litter allows for transportation of an injured person on a portable litter. The litter is secured to the LH cabin floor, with the LH forward seat removed and the LH aft seats in the stowed position.

Benefits

  • Fixed and detachable provisions can be sold separately
  • Fleet interchangeable detachable provisions
  • Quick mission changes possible
  • Single seats can be stored in the side baggage compartment for remote area usage
  • If Airbus Helicopters’ cargo pods are installed, removed single seat can be stored in one of the pods

Notes:

  • Also available as a RH litter (with a different P/N)

for an aircraft equipped in LH pilot configuration

  • AS355 information available upon request
  • Check with Airbus Helicopters for compatibility with your aircraft

AS350/H125

AS355

AS350 BA, B1, B2

AS355

LEFT HAND (LH) LITTER

Mass (kg) 0.51 (1.12 lb) Fixed Provisions

12.8 (28.2 lb) Detachable Provisions

-10.6 (23.4 lb) Removed Items, LH Seat

2.67 (5.9 lb) Total

Arm (m) 0.98 (Fixed Provisions)

1.54 (Detachable Provisions)

1.61 (Removed Items, LH Seat)

1.15 (Total)

Approvals Canada, USA, Brazil, EASA, Mexico
Part Number 350-200034-01 (Fixed)

350-200034-03 (Detachable)

Retrofit Information TCCA# SH94-29

FAA# SR00407NY, SR00406NY

ANAC# 1999S08-14, 1999S08-15, 1999S08-16

EASA# 10038250DGAC Mexico# IA-299-2015

AIRFRAME HOURMETER

The airframe hourmeter monitors and displays elapsed airborne time of the aircraft. This collective-activated hourmeter allows the operator to accurately record aircraft hours

Benefits

  • Indicates operating time in hours and tenths,
  • Has a running indicator
  • Activated upon take-off
  • Improved maintenance efficiency
  • Functions as a back-up to VEMD for flight hour recording purposes

AS350/H125

AS350 B, BA, B1, B2, B3

AIRFRAME HOURMETER

Mass (kg) Negligible
Arm (m) Negligible
Approvals Canada, USA, Brazil
Part Number 350A82-1631-01

350A82-1631-05 post AMS 07-3274

350A82-1631-07 post AMS 07-3435/3436

350A82-1631-09 post AMS 07-3478

Please contact your Airbus Helicopters representative

Retrofit Information TCCA# SH90-56

FAA# SH4016SW-D

ANAC Brazil# 1999S05-17&18

G500H GLASS COCKPIT INSTALLATION

Replaces analog instruments and installs G500H EFIS with options for single or dual transponder, radar altimeter and traffic system. AMS 07-4654 is the installation of the new avionics radio line (GTN650, GNC255A, GMA350H and GTX33H)

Benefits

  • Dual 6.5” flight displays that are easy to read
  • See clearly in dark VFR night, DVE or inadvertent IMC with HSVT™
  • Helicopter Terrain Awareness Warning System (HTAWS) support
  • Weather, traffic, and charting all in your primary field of view
  • Video input for FLIR or other camera display
  • Enhanced avionics and cockpit flexibility
  • Increased safety

Notes:

  • Standby Instruments are to be purchased separately, not included in the kit

AS350/H125

AS350 B2, B3

G500H GLASS COCKPIT INSTALLATION

Mass (kg) 7.25 kg (16 lbs)
Arm (m) 17.23
Approvals Canada, USA
Part Number 350A82-1643-01 G500H with LH PFD

350A82-1643-02 G500H with RH PFD

post AMS 07-4654

350A82-1643-09 G500H with LH PFD

350A82-1643-10 G500H with RH PFD

Retrofit Information TCCA, FAA# SR09501RC

ESI-2000 ELECTRONIC STANDBY INDICATOR (TRILOGY) INSTALLATION

Replaces analog instruments and installs G500H EFIS with options for single or dual transponder, radar altimeter and traffic system. AMS 07-4654 is the installation of the new avionics radio line (GTN650, GNC255A, GMA350H and GTX33H)

Benefits

  • Combines attitude, altitude, airspeed, slip/skid and optional heading data into a single digital display
  • Logically grouped flight data eliminates multiple instruments, making the transition to standby easier
  • Internal battery (ESI-2000 model) provides flight data for a minimum of one hour after power loss
  • Single instrument reduces weight and scan times vs. reading multiple instruments
  • Solid-state design offers increased reliability compared to electro-mechanical instruments

ESI-2000 ELECTRONIC STANDBY INDICATOR (TRILOGY) INSTALLATION

Mass (kg) 1.01 kg (2.22 lb)
Arm (m) 1.2
Approvals Canada, USA
Part Number 350A82-1645-01
Retrofit Information TCCA, FAA# SR09500RC-D

  • Trilogy™ Electronic Standby Instrument (ESI) is required as per TCCA STC
  • Check with Airbus Helicopters for compatibility with your aircraft

TRAFFIC ADVISORY SYSTEM (TAS) 615 INSTALLATION

Avidyne’s TAS615 system detects and actively interrogates other aircraft transponders within range, displays the sur- rounding traffic on a host of compatible display systems, and provides audible and visual alerts in the event of a poten- tial traffic conflict. The system also provides real-time traffic monitoring and advisories, it is not radar-coverage limited, and operates independent of ground-based systems.

Benefits

  • Three levels of alert – Other Traffic (OT), Proximity Alert (PA) and Traffic Alert (TA)
  • Provide a full 30-second decision time at a closure rate of up to 1200 knots
  • Added safety in all flight conditions
  • Provides real time traffic information

TRAFFIC ADVISORY SYSTEM (TAS) 615 INSTALLATION

Mass (kg) 4.98 kg (10.98 lb)
Arm (m) 12.08
Approvals USA
Part Number 350A82-1649-01 (W/ Analog Controls),

350A82-1649-02 (W/ G500H)

Retrofit Information FAA# SR09312RC-D

Notes:

  • Altitude information provided by the TAS615 is advisory only and is not to be used for dispatching purposes. It does not relieve the pilot in command of this responsibility

BMS VIDEO DOWNLINK SYSTEM INSTALLATION

The Airborne Downlink system is a single box solution containing everything needed for high-quality, reliable transmission. This includes the video encoder, modulator, up-converter and high-power amplifier. It also includes a dependable low cost antenna mounted on the cabin roof and employs an omnidirectional antenna that provides 360° of azimuth coverage. The new Cockpit Downlink Control Panel is designed to give the aircraft operator full control of any BMS digital microwave system.

Features

This installation consists of:

  • A signal power amplifier mounted in the right baggage compartment
  • Primary aerial control panel mounted in the console
  • Omni antenna mounted on the right skid
  • Dedicated GPS antenna mounted on the cabin roof

Benefits

  • Low delay time
  • Digital signal resistant to multipath degradation

BMS VIDEO DOWNLINK SYSTEM INSTALLATION

Mass (kg) 3.73 kg (8.25 lb)
Arm (m) 10.98
Approvals USA
Part Number 350A82-1647-03
Retrofit Information FAA# SR09311RC-D

Notes:

  • Operation of the BMS downlink system DLC50 Control Panel is restricted to a crewmember that is not manipulating the flight controls.

MULTI-BLOC CENTER CONSOLE INSTALLATION

This modification replaces the original center console with one which is slightly taller, allowing for the installation of deeper avionics units. The switches and annunciators from the original center console are transferred to the new console

Benefits

  • Allows for the installation of Garmin GTN750 displays

MULTI-BLOC CENTER CONSOLE INSTALLATION

Mass (kg) Negligible
Arm (m) Negliigible
Approvals USA
Part Number 350A73-2023-01
Retrofit Information FAA# SR09504RC

AS355

AS350B, BA, B1, B2, B3, D AS355 NP

CABLE CUTTER INSTALLATION

The Cable Cutter Installation offers a measure of protection against impacting horizontally strung cables. The cable- cutters are installed on the lower and upper canopy. This installation is highly recommended by Airbus Helicopters for the improved safety of passengers and crew.

Benefits

  • Protection against cable strike
  • Improved safety for pilot and passengers
  • No additional maintenance
  • Lightweight installation

AS355

AS350B, BA, B1, B2, B3, D AS355 E, F, F1, F2, N, NP

CABLE CUTTER INSTALLATION

Mass (kg) 6.64 (14.6 lb)
Arm (m) 0.93
Approvals Canada, USA, Brazil, Mexico
Part Number 350-252004
Retrofit Information TCCA# SH12-52

FAA# SR03279NY (only AS350) ANAC # 2013S10-12 (only AS350)

DGAC Mexico # IA-267/2014 (only AS350)

Notes:

  • Kit compatible only with airframe post factory modi- fications OP 1946 and OP 1947

DUAL CARGO MIRRORS

The Cargo Mirrors positions two mirrors directly outside the Pilot’s chin window for improved visibility when per- forming cargo hook operations. The mirrors can be installed on the left hand side, right hand side or both sides of the aircraft.

Benefits

  • Eases maneuverability
  • Lightweight

AS350/H125

AS355

DUAL CARGO MIRRORS

Mass (kg) 1.72 (3.8 lb) per side
Arm (m) 0.28
Approvals Canada, USA, LBA (Germany), EASA countries, Brazil, Mexico
Part Number 350-200264-03-RH

350-200254-03-LH

Retrofit Information TCCA# SH96-61

FAA# SR00457NY LBA# RC 1019

EASA# 10042575

ANAC# 2013S10-13

DGAC Mexico# IA-223/2013

Notes:

  • The mirror is available as a replacement item P/N 350-200254.10
  • Approved configurations: Canada: LH and/or RH USA: LH or RH

ELECTRICAL CONTROLLER FOR 50AMP/LONGLINE RELEASE/CAROUSEL SYSTEMS

Universal external 50Amp power supply designed to control longline remote hook release or carousel. It is a self contained unit with cyclic release and arm function.

Compatible with following equipment (not supplied in kit):

  • Bambi bucket (incl. USFS modification)
  • Carousel system
  • Geophysics survey equipment
  • Drip torch

Benefits

  • Self contained controller
  • Cyclic activation – increase safety
  • Separate ARM functions (exclusive)

Technical Information

AS350/H125

AS350 B2, B3

ELECTRICAL CONTROLLER FOR 50AMP/LONGLINE RELEASE/CAROUSEL SYSTEMS

Mass (kg) 6.38 kg (14 lb)
Arm (m) 2.75
Approvals Canada, USA, EASA, Brazil, Mexico
Part Number 350-900564
Retrofit Information TCCA# SH14-10

FAA# SR03526NY EASA# 10051182

ANAC# 2014S11-18

DGAC Mexico# IA-295/2014

Notes:

  • Kit supplied with loose mating connector to be wired by installer/operator

CARGO PODS (“SQUIRREL CHEEKS”)

The Cargo Pods increase the volume of both the left hand (LH) and right hand (RH) cargo compartments. They can be installed individually or in pairs.

The composite material pod has a hinged door which opens widely for easy access to the storage area and is held open by a gas strut. The door fastens securely for flight with three positive latches.

The installation also includes a door open warning annunciator. The upper portion of the cargo pod surface includes an excellent standing area for maintenance activities. The fuel filler and EPU access are unaffected.

The cargo pods are ideal for utility missions, tourism and corporate passenger transport

Benefits

  • Increases the cargo load capacity by 70% over the standard AS350 cargo compartment
  • Increases cargo volume capacity by 90% over the standard AS350 cargo compartment
  • Eases access
  • Platform for maintenance
  • Aerodynamic design
  • Dual or single installation
  • Battery relocation option: Cargo Pod volume on RH

side is 0.43 cubic meters and can carry 195kg

  • Cargo Pod volume on LH side is 0.43 cubic meters

and can carry 195kg

AS355

AS350 B, BA, B1, B2, B3, D AS355 E, F, F1, F2, NP

CARGO PODS (“SQUIRREL CHEEKS”)

Mass (kg) 32 (70.5 lb) both sides installed
Arm (m) 3.53
Approvals Canada, USA, EASA
Material Fiberglass, Prepreg Layup

Durable Aluminum Floor Cover

Part Number 350-200814-824 (AS350)

355-200814-824 (AS355)

Incompatibility Not compatible with sliding doors

Not compatible with AS350 equipped with AFS air conditioning system with condenser located in the RH cargo compartment

L/H compatible with aircraft before modification

07-4606 only

Operational

Limitations

HIGE, HOGE charts and climb performance are af- fected, refer to FMS (Flight Manual Supplement)
Retrofit Information TCCA# SH97-15 (AS350), SH97-60 (AS355) FAA# SR00699NY, SR00795NY (E, F, F1, F2) EASA.IM.R.S.01031

FORWARD OPENING REAR CARGO DOOR

The Forward Opening Rear Cargo Door replaces the existing door. The dual-hinged side mounted door improves access for loading and unloading of the rear cargo compartment.

Benefits

  • Facilitates maintenance by allowing easy access
  • Facilitates loading and unloading
  • Equipped with a gas strut to keep door in open position

AS355

AS350 B, BA, B1, B2, B3, D, D1

AS355 E, F, F1, F2, NP

FORWARD OPENING REAR CARGO DOOR

Mass (kg) 0.63 (1.39 lb)
Arm (m) 2.91
Approvals Canada, USA, EASA, Brazil, Mexico
Material Fiberglass, Prepreg Layup
Part Number 350-201014
Retrofit Information TCCA# SH97-34

FAA# SR00676NY, SR00678NY EASA# IM.R.S.01321

DGAC Mexico# IA-239/2013

ANAC# 1999S08-03, 1999S08-04, 1999S08-05

AIRFRAME FUEL FILTER

The Airframe Fuel Filter removes foreign particles from the fuel, including ice particles which allows sub zero operation without the use of anti-ice fuel additives.

Benefits

  • Removes foreign particles from fuel
  • Allows helicopter to operate at below freezing temperatures without anti-ice additives
  • Impending bypass indicator in cockpit

AS350

AS350 B, BA, B1, B2

AIRFRAME FUEL FILTER

Mass (kg) 2.37 (5.2 lb)
Arm (m) 3.46
Approvals Canada, USA, Germany, Brazil, Mexico
Part Number 350-600004
Retrofit Information TCCA# SH94-31

FAA# SR00379NY LBA# RC1020

ANAC# 2013S07-05

DGAC Mexico# IA-225/2013

Notes:

  • Container must be emptied manually
  • Fuel additives are required for operation below 0°C

when ferry tanks are used

AIRFRAME FUEL FILTER

The Airframe Fuel Filter removes foreign particles from the fuel, including ice particles which allows sub zero operation without the use of anti-ice fuel additives.

Benefits

  • Removes foreign particles from fuel
  • Allows helicopter to operate at below freezing temperatures without anti-ice additives
  • Impending bypass indicator in cockpit
  • There is a limitation of Jet A only for the H125

(AS350 B3) with Arriel 2D Engine installed

  • Container must be emptied manually

H125

AS350 B3, B3e

Mass (kg) 3.35 (7.4 lb)
Arm (m) 3.50
Approvals Canada, USA, Brazil, Mexico
Part Number 350-600024
Operational

Limitations

Max Altitude JET A 21000 ft. (B3) Max Altitude JET A 15000 ft. (B3e)

Max Altitude JET B 15000 ft. (B3), Replacement fuels prohibited (B3e).

Max OAT JET B ISA +30°C to 43°C (B3)

Retrofit Information TCCA# SH02-42

FAA# SR01632NY (only B3) DGAC Mexico# IA-231/2013

ANAC# 2013S10-14 (only B3)

Supplied by Airbus Helicopters Canada .

Retrofit can be performed at customer’s facility

CARGO TIE DOWN RINGS IN AFT CABIN FLOOR

The Six heavy-duty cargo tie-down ring system consists of reinforced attachment points on the aircraft’s cabin floor. This system allows heavy objects to be secured in the cabin, and can also be used for rappelling from the helicopter, without preventing the later re-installation of rear seats. The system’s flexibility makes it extremely popular with utility and parapublic operators.

Benefits

  • Enhanced safety through the secure transportation of loads and equipment inside the helicopter
  • Allows internal or external loads to be safely secured
  • Enhanced aircraft mission versatility
  • Each tie down point is rated to restrain 62.5 lb of cargo for internal loads and 250 lb for external loads
  • The tie-down fittings can be mounted on the four floor attachment rails which are fitted as standard

AS350/H125

All models

CARGO TIE DOWN RINGS IN AFT CABIN FLOOR

Mass (kg) Negligible
Arm (m) Negligible
Approvals USA
Part Number 350A82-1094-02
Retrofit Information FAA# SH7693SW-D

AIRCRAFT FLOOR COVER

The Aircraft Floor Cover is a durable utility vinyl floor mat made to help protect the entire cabin floor. Available in black, grey and blue.

Benefits

  • Protects the cabin floor
  • Provides enhanced comfort through insulation
  • Long-lasting
  • Reinforced with minimal shrinkage
  • Wear-resistant
  • Custom fit

AS350/H125

AS355

All models

AIRCRAFT FLOOR COVER

Mass (kg) 11.3 (25.0 lb)
Arm (m) 1.4
Approvals Canada, USA, EASA, Mexico, Brazil
Part Number 350-701814-01 (Grey)

350-701814-02 (Blue)

350-701814-03 (Black)

Retrofit Information TCCA# SH12-28

FAA# SR03572N EASA# 10056823

DGAC Mexico# IA-355/2016

ANAC Brazil# 2016S09-07

AIRCRAFT SEAT COVER

The Aircraft Seat Covers are made with highly wear-resistant aircraft fabric or leather. Approved fabric is available in two patterns and three colors (black, grey and blue). Approved leather is available in two colors (grey and blue). The covers can easily fit onto the existing seat foams. Replacement foams can be ordered separately to provide a replacement cushion.

Benefits

  • Enhanced comfort and design
  • Easy to install
  • Made with flame resistant materials, approved by Transport Canada

AIRCRAFT SEAT COVER

Mass (kg) 1.0 – 1.5 (2.2 lb – 3.3 lb) depending on material
Arm (m) Varies depending on configuration
Approvals Canada, USA, EASA, Mexico, Brazil
Part Number 350-701904-01, 03 or 08

Front Seat Cover

350-701044-02 or 06

Rear Seat Cover (Bottom)

350-701044-04 or 05

Rear Seat Cover (Back)

Retrofit Information TCCA# SH12-28

FAA# SR03572N EASA# 10056823

DGAC Mexico# IA-355/2016

ANAC Brazil# 2016S09-07

BACK SEAT DOCUMENT HOLDERS

The Back Seat Document Holders provide discreet leather pockets mounted on the rear of the energy absorbing seats. Due to its elastic design the document holders are not bulky, however can easily accommodate larger documents, such as Flight Manuals, or store up to approx. 3.2 kg.

Available in a highly robust leather, dyed black, grey or blue to match the approved leather seat covers.

Benefits

  • Provides space for stowing documents and small personal items for pilots and crew
  • Light weight and compact
  • Elastic design prevents holder contents from moving during flight, thus enhancing safety
  • Easy to install

BACK SEAT DOCUMENT HOLDERS

Mass (kg) 1.0 (2.2 lb)
Arm (m) 1.62
Approvals Canada, USA, EASA, Mexico, Brazil
Part Number 350-701074 (Installation kit)

350-701084-01 (Black document holder)

350-701084-41 (Blue document holder)

350-701084-42 (Grey document holder)

Retrofit Information TCCA# SH12-28

FAA# SR03572N EASA# 10056823

DGAC Mexico# IA-355/2016

ANAC Brazil# 2016S09-07

  • Only available on energy absorbing seats

UTILITY VINYL SEAT COVERS

The Utility Seat Covers are made with a highly wear-resistant aircraft vinyl. The covers can easily fit onto the existing

OEM seat foams. Using covers with additional OEM foams can provide replacement cushions.

Benefits

  • Highly resistant to dirt and harsh environments
  • Easy to install
  • Made with flame resistant materials

UTILITY VINYL SEAT COVERS

Mass (kg) 1.35 (3.0 lb)
Arm (m) 1.62
Approvals Canada, USA, EASA, Mexico, Brazil
Part Number · 350-701044-01

Front seat cover (Pilot or Co-pilot))

· 350-701044-02 or 03

Rear seat cover (Back)

· 350-701044-06

Rear seat cover (Bottom)

· 350-701044-07

Rear 2 place seat cover (Back & Bottom)

Retrofit Information TCCA# SH12-28

FAA# SR03572N EASA# 10056823

DGAC Mexico# IA-355/2016

ANAC Brazil# 2016S09-07

Notes:

  • Available in black vinyl only

Airbus Helicopters reserves the right to make 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 offer or contract with Airbus Helicopters.

BATTERY RELOCATION KIT

The Battery Relocation Kit provides provisions to install a high capacity lead acid or nickel cadmium battery in the tail boom removing the standard aircraft battery located in the right hand (RH) cargo compartment. It reduces the need for aft aircraft ballast and increases the usable space in the RH cargo compartment. The battery is mounted on a removable tray in the left hand (LH) side of the tail boom. The battery relocation kit is ideal for balancing aircraft equipped with heavily loaded instrument panels.

Benefits

  • Increases RH cargo capacity
  • Reduces the need for tail boom ballast
  • The battery can be quickly disconnected and can be removed while wearing winter gloves

Notes:

  • Kit does not include battery
  • Compatible with NI-CAD (2376-1) or Lead Acid

(RG-390E) battery

  • Finished in primer: must be painted after installation.

AS350/H125

AS355

AS350 B, BA, B1, B2, B3, D, D1

AS355 E, F, F1, F2

BATTERY RELOCATION KIT

Mass (kg) 27.1 (59.7 lb) remove std battery, add lead acid battery

24.0 (52.9 lb) remove std battery, add NiCad battery

Arm (m) 9.49 (remove std battery, add lead acid battery)

9.49 (remove std battery, add NiCad battery)

Approvals Canada, USA, EASA, Brazil, Mexico
Part Number 350-700324 (AS350)

355-700324 (AS355)

Retrofit Information TCCA# SH96-31

FAA# SR00422NY (AS350), SR00800NY (AS355) EASA# 10016747 (or EASA.IM.R.S.01073)

ANAC# 9703-02 (AS350), #2002S06-01 (AS350 B)

ANAC# 2002S06-02 (AS355 F1, F2) DGAC Mexico# IA-266/2014

7 PLACE INTERIOR

The 7 Place Interior consists of a composite-structure 2 Place Forward Passenger Seat on the right-hand side of the cockpit as well as, the Left-hand Pilot Installation. The seat is installed on fixed rails on the cabin floor and is removable by use of quick-release fasteners. A four point seatbelt and shoulder harness is provided for each front occupant of the seating arrangement.

The pilot-in-command position is moved from the right to the left side, along with all associated flight controls and other cockpit controls and instrumentation. Provisions for optional dual pilot controls are included in this installation.

Battery Relocation is highly recommended for the 7 Place Interior.

Benefits

  • Increased passenger capacity
  • Increased visibility of load during cargo sling operations
  • Improved cabin space for additional options

Notes:

  • Requires the installation of the Left-hand Pilot

(I.A.W. TCCA SH96-32).

  • The dual bench rails are compatible with the extend- ed EA seat rails
  • Seat covers are not included and are to be provided and certified by the installer
  • The front bench seat is the same width as the rear

bench seats (16”).

Optional Equipment

Technical Information

AS350/H125

AS350 BA, B2, B3

7 PLACE INTERIOR

Mass (kg) 12.25 (27.0 lb) 2 Place Forward Passenger Seat

See SH96-31 (Battery Relocation) See SH96-32 (Left-hand Pilot)

Arm (m) 1.57 (2 Place Forward Passenger Seat)

See SH96-31 (Battery Relocation) See SH96-32 (Left-hand Pilot)

Approvals Canada, USA, EASA, Brazil, Mexico
Part Number 350-200624 (2 Place Forward Passenger Seat)

350-700324 / 355-700324 (Battery Relocation)

Contact your Airbus Helicopters Representative for Left- hand Pilot part numbers (based on specific I panel

requirements).

Operational

Limitations

Two place seat detachable provisions are not compatible with dual controls.

Minimum crew consists of one pilot in the left hand seat.

Retrofit Information TCCA SH96-39 (2 Place Forward Passenger Seat) EASA.IM.R.S.01022 (2 Place Forward Passenger Seat) FAA SR00430NY (2 Place Forward Passenger Seat) ANAC# 9703-04 (2 Place Forward Passenger Seat) DGAC Mexico# IA-230/2013

See SH96-31 (Battery Relocation) See SH96-32 (Left-hand Pilot)

Order Information

LEFT-HAND PILOT CONFIGURATION

The pilot-in-command position is moved from the right to the left hand side, along with all associated flight controls and additional cockpit controls and instrumentation. The Instrument Panel is available in three different sizes including; tour, standard and extended.

Benefits

  • Increased visibility of load during cargo sling operations
  • Improved cabin space for additional options
  • Allows for the use of dual controls

Notes:

  • Relocating the aircraft battery to the tailboom

(Battery Relocation Kit) is highly recommended

  • The space remaining in the center of the cockpit

floor after the engine control quadrant is moved to the left allows for a 7 Place Interior Configuration

  • Left-hand Pilot lighting modification and configuration to be addressed by installer
  • Lighting solution included for aircraft with multi-bloc console

Optional Equipment

Technical Information

AS350/H125

AS350 BA, B2, B3

LEFT-HAND PILOT CONFIGURATION

Mass (kg) 2.14 (4.7 lb)
Arm (m) 1.13
Approvals Canada, USA, EASA, Brazil
Part Number Contact your Airbus Helicopters Representative for part numbers (based on specific I-Panel requirements).
Operational

Limitations

Dual controls are prohibited if 7 Place Interior is installed in accordance with (TCCA) SH96-39.

Minimum crew consists of one pilot in the left hand seat.

Retrofit Information TCCA# SH96-32

EASA# 10016725

FAA# SR00429NY ANAC # 9703-03

HIGH VISIBILITY DOORS

The High Visibility Doors provide pilots and passengers with an increased viewing field through the extra large windows. The fully composite doorframe replaces the standard door(s) and can be installed individually or in any combination, including all four doors.

The high visibility doors are ideal for law enforcement, tourism and utility missions.

Benefits

  • Increases visibility for pilots and passengers
  • Increases passenger comfort
  • No change to operational limitations
  • Same safety features as a standard door (latching, locking and emergency egress)
  • No obstruction for camera, video equipment or goggles

Notes:

  • Finished in primer: must be painted after installation.

Technical Information

AS350/H125

AS355

AS350 B, BA, B1, B2, B3

AS355 N, NP

HIGH VISIBILITY DOORS

Mass (kg) 11.9 (26.2 lb) Forward LH door

11.9 (26.2 lb) Forward RH door

5.80 (12.8 lb) Rear LH door

5.80 (12.8 lb) Rear RH door

Arm (m) 1.62 (Forward LH door)

1.62 (Forward RH door)

2.43 (Rear LH door)

2.43 (Rear RH door)

Approvals Canada, USA, EASA
Material Fiberglass, Prepreg Frame and Acrylic Window
Part Number 350-202014-03 – LH Forward

350-202014-04 – RH Forward

350-202014-05 – LH Rear

350-202014-06 – RH Rear

Color Availability Gloss Beige Gloss Grey Black
Incompatibility Not compatible with sliding doors
Retrofit Information TCCA# SH00-1, SH15-7 (N, NP) FAA# SR01107NY (only AS350) EASA.IM.R.S.01195 (only AS350)

Product Description

AS350/H125

AS350 B, BA, B1, B2, B3

FORWARD SHORT HIGH-VISIBILITY DOORS

The short version of the high visibility door is compatible with the sliding door and provides a full height continuous window option for aircraft equipped with rear sliding doors. The doors can be installed on one or both sides of the aircraft.

Benefits

  • Increases visibility for pilots and passengers
  • No visual interference with binoculars or goggles
  • Increases passenger comfort
  • No performance restriction
  • Same safety features as a standard door (latching, locking and emergency egress)

Notes:

  • Finished in primer: must be painted after installation
  • For use with sliding rear doors only (not compatible with rear hinged doors).

Technical Information

AS350/H125

AS350 B, BA, B1, B2, B3, D, D1

FORWARD SHORT HIGH-VISIBILITY DOORS

Mass (kg) 8.0 (17.6 lb) Forward LH door

8.0 (17.6 lb) Forward RH door

Arm (m) 1.56 (Forward LH door)

1.56 (Forward RH door)

Approvals Canada, USA, EASA, Brazil, Mexico
Material Prepreg Fiberglass frame construction
Part Number 350-202414-01 – LH Clear Windows

350-202414-02 – RH Clear Windows

350-202414-03 – LH Tinted Windows

350-202414-04 – RH Tinted Windows

Retrofit Information TCCA# SH05-18

FAA# SR02141NY EASA# IM.R.S.01221

DGAC Mexico# IA-335/2015

ANAC# 2015S10-07

AS355

AS350 B, BA, B1, B2, B3

AS355 N, NP

ENLARGED VERTICAL REFERENCE WINDOW

The enlarged vertical reference window is the largest vertical reference window available on the market for AS350/355 aircraft. For long lining operations the larger window permits you to see loads closer to the aircraft allowing for opera- tions with shorter lines, resulting in enhanced operating versatility and safety. Increases visibility for long lining.

Benefits

  • AHCA extended forward composite belly panel totally incorporates the window.
  • The drop down of the belly panels for maintenance access is unaffected, no screws, only the original quick release latches.
  • Intermediate composite belly panels includes relocation of landing light.
  • Customer can keep the original panels.
  • AHCA offers the largest floor window on the market.

Belly panel window size is 0.23 square meters

(2.50 square feet).

AS355

AS350 B, BA, B1, B2, B3

AS355 N, NP

ENLARGED VERTICAL REFERENCE WINDOW

Mass (kg) 2.8 (6.2 lb)
Arm (m) 1.71
Approvals Canada, USA
Material Acrylic windows (belly and floor); aluminum sheet metal floor reinforcement; composite (rework of belly panels)
Part Number 350-201154
Retrofit Information TCCA# SH06-12

FAA# SR03771NY

Notes:

  • Rework of floor and composite belly panels required
  • Not compatible with the RH Sliding Door

Airbus Helicopters reserves the right to make 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 offer or contract with Airbus Helicopters.

Product Description

AS350/H125

All models

COWLING MAINTENANCE STEPS

The Cowling Maintenance Steps improve access to the main rotor head for routine maintenance and inspection. Large enough for winter boots, the steps are located on both sides of the aircraft.

Benefits

  • Improved access to the main rotor head for maintenance and inspection

Technical Information

AS350/H125

All models

COWLING MAINTENANCE STEPS

Mass (kg) Negligible
Arm (m) N/A
Approvals Canada, USA, Mexico
Part Number 350-200094

350-200104

Retrofit Information TCCA# SH97-36

FAA# SR00653NY

DGAC Mexico# IA-300/2015

RAIL STEPS

The Rail Steps installation introduces an elevated step to each side of the landing gear, providing easier entry and exit for crew and passengers. It also provides maintenance staff with improved access to the transmission deck for daily checks and maintenance

Benefits

  • Provides easier entry and exit for crew and passengers
  • Provides easier access to transmission deck for maintenance

RAIL STEPS

Mass (kg) 7.7 (17.0 lb) with LH & RH installed
Arm (m) 2.06
Approvals Canada, USA
Material Aluminum Alloy
Part Number 350-500194 – LH

350-500204 – RH

Retrofit Information TCCA# SH98-44

FAA# SR00906NY (AS350)

REAR MAINTENANCE STEPS

The Rear Maintenance Steps improve access to the engine and transmission decks for routine maintenance and inspec- tion. They are mounted on the landing gear aft cross tube and include an anti-slip surface.

Benefits

  • Large contact surface with anti-slip finish for safety
  • Improved access to engine and transmission
  • Kit includes both left and right step assembly

REAR MAINTENANCE STEPS

Mass (kg) 2.2 (4.9 lb) LH & RH installed
Arm (m) 4.22 (LH & RH installed)
Approvals Canada, USA, EASA, Mexico, Brazil
Material Aluminum Alloy
Part Number 350-500604 (LH and RH)

350-500614 (LH only)

350-500624 (RH only)

Retrofit Information TCCA# SH98-43

FAA# SR00916NY EASA# 10057054

DGAC Mexico# IA-301/2015

ANAC# 2015S09-03

Product Description

AS350/H125

AS350 B, BA, B1, B2, B3, D

BELLY-MOUNTED ANTI-COLLISION LIGHT

The Belly Mounted Strobe Light enhances collision avoidance by making your aircraft more visible to others, thereby improving flight safety. Installation of the anti-collision strobe light on the belly of the aircraft is done just aft of the rear landing gear cross tube.

Benefits

  • Enhanced collision avoidance
  • Offers increased positional awareness for nearby traffic
  • Note: for the LED version, choice of Red or Red/White light

Notes:

  • Light must be turned off during night take-offs and landings.
  • To avoid optical illusions and vertigo turn strobe lights off upon entering clouds, fog or haze.

Technical Information

AS350/H125

AS350 B, BA, B1, B2, B3, D

BELLY-MOUNTED ANTI-COLLISION LIGHT

Mass (kg) 0.82 (1.8 lb)
Arm (m) 4.34
Approvals Canada, USA, EASA, Brazil, Mexico
Part Number 350-900624-01 – no RADALT installed

350-900624-02 – with RADALT installed

350A82-1576-11 (LED)

Retrofit Information TCCA# SH96-114

FAA# SR00645NY LBA# RC1004

ANAC# 1999S08-06 (AS350 BA, B1, B2)

ANAC# 1999S08-07 (AS350 B) DGAC Mexico# IA-186/2012

LED

TCCA# SH93-32

FAA# SH4343SW-D

Product Description

AS350/H125

AS355

AS350 D,, B, BA, B1, B2, B3

AS355 E, F, F1, F2, N, NP

BLADE TIE-DOWN KIT

The Blade Tie-Down Kit prevents the blades from flapping in windy conditions while the helicopter is parked on the ground.

Benefits

  • Prevents blade movement and main rotor head damage
  • Easy and efficient one-person installation, no additional equipment required
  • Compact and light ground support equipment for on-board storage

Technical Information

AS350/H125

AS355

AS350 D, B, BA, B1, B2, B3

AS355 E, F, F1, F2, N, NP

BLADE TIE-DOWN KIT

Mass (kg) 0.14 (0.3 lb) fixed provision
Arm (m) 1.48
Approvals Canada, USA, EASA, Brazil, Mexico
Part Number 350-700414 (complete kit)

350-700424 (fixed provisions)

130-700474-01 (detachable kit)

Retrofit Information TCCA# SH96-126

FAA# SR00539NY (355), SR00540NY (350) EASA# 10043426

ANAC# 1999S08-11, 1999S08-10,

1999S08-12 (355)

DGAC Mexico# IA-265/2014

Notes:

  • For winds up to 40 knots.

Airbus Helicopters reserves the right to make 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 offer or contract with Airbus Helicopters.

ADDITIONAL AS350/355 OPTIONS

DESCRIPTION APPROVALS PART NUMBER

Side Latch Kit LH TCCA#SH97-35

FAA# SR00657NY

350-201214

Side Latch Kit RH

TCCA#SH97-35

FAA# SR00657NY

350-201224

Firewall Reinforcement

TCCA# SH96-115

FAA# SR00579NY

350-601014-02

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