.

EC 145
BK 117C-2


 .   

Air Ambulance

quick conversion
EMS Interior

 

innovative air medical interior 

   

 

Advantages

  • Ergonomic and versatile modular system - maximum safety and comfort for crew and patient; full configuration flexibility

  • Low weight design – more pay load or safety margin

  • Quick conversion  standard utility helicopter to the air ambulance / EMS role in less than 1 hour,
    ..........................no structural or interior modification required 

  • Superior handling – simple patient loading and unloading; reconfiguration or removal of equipment in minutes

  • Easy maintenance and cleaning – good accessibility; material contamination proof 

  • Taylor-made solutions for your specific mission requirements

  • Full EASA certification (STC)

Missions

  • Primary and secondary EMS
  • Search & Rescue
  • Disaster
Transport Capability / Crew
  • 1 patient or incubator, 2 patients disaster role

  • 2 to 4 medical crew depending on configuration

  • 2 flight crew 

Features

  • Integral medical floor (leak proof, blood dam)

  • Removeable locker systems with AFT loading ramp

  • 1 low profile intensive undercarriage stretcher
    for easy AFT patient loading and unloading

  • 1 foldable rescue stretcher for second patient (disaster role)

  •  Medical equipment carrier with

Supports for medical devices
(suction unit, ventilation, syringe pump, ECG monitor
)

Patient illumination

Medical Power Distribution Unit

  • Ceiling panel with supports for medical devices and LED cabin light

  • RH rail system with oxygen / air distribution and holder for foldable rescue stretcher

  • 2 to 4 adjustable medical crew seats (2 off swivelling)

  • Oxygen / Air station with drawers for medical material

Optional Features

  • Storage box for additional rescue equipment, vacuum mattress and survival kit
  • Cabinet AFT with drawers for medical materials
  • Storage box with holder for foldable rescue stretcher

Certification: EASA / JCAB Supplemental Type Certificate (STC)  No. EASA.R.S.00468 according to CS / JAR and FAR part 29