Heliproducts Industries Ltd can provide full installation and sales of STC optional equipment for the AS350 and AS355. Call for Pricing.
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
|
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
|
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”)
|
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
|
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
|
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
|
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
|
- 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
|
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
|
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
|
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
|
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
|
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
|
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
|
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
|
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 |