List of modifications

Helicopters / Airbus / AS365N/N2/N3/EC155B1

MAP037 – Chelton Direction Finder (935-series) Installation
MAP039 – Centre Console Reconfiguration
MAP042 – 3rd ICS Jack
MAP043 – Flight Data Management – Quick Access Recorder Installation
MAP047 / MAP065 – Fire Extinguisher Relocation in Cabin
MAP051 – Helicopter Emergency Egress Lighting (HEEL) System Installation
MAP052 – Cockpit Voice Recorder Replacement
MAP061/MAP085 – HF removal
MAP062 – Skytrac ISAT-200 SATCOM Installation
MAP073-MAP079, Flight Manual Supplements - Translations
MAP079 – HR Smith ADELT CPI Installation
MAP080 – Replacement of KXP 756 transponder with Garmin GTX330 Mode-S Transponder
MAP083/MAP086/MAP152/MAP153 – Replacement of VHF radios with 8.33kHz capable radio systems, Fleet standardisation
MAP084 – Axnes PNG installation
MAP100 – FLIR 2000 integration on AS365N2
MAP105 – TAS installation
MAP108 – Passenger intercom extension
MAP148 – Partial Air Conditioner removal
MAP150 – Shock Mounts Replacement RNAV ARINC Tray
MAP155 – External Paint Livery
MAP156 - USB Power outlets in instrument panel
MAP158 - Flightcell DZMx installaiton
MAP159 - COBHAM (NAT) NPX-138 VHF FM Installation
MAP162 - Jupiter Avionics Headset Expander Installation
MAP163 – 28VDC power outlet change in cabin
MAP165 - ICS Channel switching
MAP170 - Tail fin cover modification for a VHF FM antenna

MAP105 – TAS installation

The modification covers the complete installation and aircraft integration of an Avidyne TAS-620A system in combination with a Bendix King KMD-550 Multi Function Display (MFD).

The installation is comprised of the following main LRUs:

  • TAS-620 Processor
  • Antenna couplers (2 off)
  • Top and bottom external antennas
  • Display Unit (DU) in the instrument panel in the cockpit

The Traffic Advisory System (TAS) has the functionality to:

  • Actively Interrogates threat aircraft transponders for reply
  • Not dependent on “third party interrogation”
  • Provides “real-time” collision alerts
  • Meets FAA TSO C-147 specifications
  • Provides up to a 30-second warning at up to 1200 knot closure – (same as TCAS I)
  • 360° coverage for intruder around the aircraft

The modification includes (customer documents):

  • Mechanical installation drawings
  • Mechanical manufacturing drawings (for e.g. brackets and adapter plates required)
  • Wiring diagrams
  • Engineering orders
  • Test plans
  • Instruction for Continued Airworthiness
  • Flight Manual Supplement

To request development and/or EASA approval of a modification or repair, please contact us.

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EASA Design Organisation approval

Certified design

MAP 21 achieved an EASA Part 21 Subpart J Design Organisation Approval in 2007, EASA.21J.326, which enables us to approve modifications to the aviation industry as a delegated EASA authority.