SECURITY & DEFENSE

AVIATION

SPECIAL MISSION AIRCRAFT

YEAR

2017 - TODAY

LOCATION

HAMBURG / KIEL 

MÖNCHENGLADBACH,

GERMANY

CUSTOMER

QinetiQ GmbH

QinetiQ Ltd.

PROJECT

PILATUS PC-12/47E

PILATUS PC-12/47

PILATUS PC-9 / PC-9B

DIAMOND DA62

Pilatus PC-12/47E

Marine Patrol Aircraft (MPA). Aircraft  equipped with a powerful radar, avionics, optronics, live video downlink options and  operator consoles for maritime patrol missions.

  • Radome design and installation at the lower fuselage of the aircraft
  • Major and minor structure modification for the installation of the radar sensor and radome
  • Installation of the PrecISR 1000 HENSOLDT airborne surveillance radar
  • Installation of antennas, tactical broadband data links, EO/IR Camera Systems (WESCAM MX15) and sensors
  • Relocation of antennas (e.g. radar altimeter), systems inside the fuselage (e.g. underfloor heating system) and other devices to provide the required space envelope for the planed system integration
  • Installation of specific hardware for the operation of the airborne surveillance radar (e.g. iNAT - RLG Based Navigation, Surveying & Control System)
  • Installation of specific hardware for mission operation e.g. AMU-Audio Management Unit as termination point for all relevant aircraft system interfaces, radios, audio control panels (ACP) and headsets
  • Components and systems for use inside the mission cabin of the MPA Aircraft (e.g, mission rack’s, operator consoles, patch panel)
  • Systems modification for adaptation to the cabin layout LOPA (e.g., Oxygen System)
  • All modifications were developed in accordance with EASA Part 21J standards, ensuring seamless certification and airworthiness compliance. 
Pilatus PC-12/47

Flying TestBed (FTB) for experimental equipment installations and applications. Establishment and realization of a Flying Testbed (FTB) based on a Pilatus PC12/47 for the concept development and testing of key technologies in the aviation sector of security and defense.

  • Execution of major and minor structural modifications for the installation of radar sensors, radoms,camera systems and special mission equipment
  • Installation of the HENSOLDT MFRFS Airborne Surveillance Radar Prototype for test campaigns and advanced product development.
  • Radome design and installation at the lower fuselage of the aircraft
  • Installation of antennas, tactical broadband data links, EO/IR Camera Systems (WESCAM MX15) and sensors
  • Relocation of antennas (e.g. radar altimeter), systems inside the fuselage  and other devices to provide the required space envelope for the planed system integration
  • Installation of specific hardware for the operation of the airborne surveillance radar (e.g. iNAT - RLG Based Navigation, Surveying & Control System)
  • Installation of specific hardware for mission operation e.g. AMU-Audio Management Unit as termination point for all relevant aircraft system interfaces, radios, audio control panels (ACP) and headsets
  • Components and systems for use inside the mission cabin of the Flying TestBed (e.g, mission rack’s, power converter rack’s, operator consoles, patch panel)
  • Installation and customisation of the ADMI Special Mission Interior for the Pilatus PC-12
  • Systems modification for adaptation to the cabin layout LOPA
  • All modifications were developed in accordance with EASA Part 21J standards, ensuring seamless certification and airworthiness compliance
Pilatus PC-9 & PC-9B 

Special Mission Aircraft for Aerial Targeting Services & Close Air Support

  • Minor Structural Modifications – targeted design changes such as bracket installations, antenna mounts, and equipment supports to improve functionality with minimal impact to the airframe
  • MX-10 Underwing EO/IR Sensor Pylon with Data Link – Mechanical design, structural integration, and installation to support enhanced surveillance and reconnaissance capabilities 
  • MX-10 EO/IR Sensor Aircraft Integration – Cockpit control and display installation with full support for avionics, flight testing and certification to ensure seamless system operation.
  • Cockpit Modifications – design and integration of multi-function displays, sensor displays, hand controllers and radios to enhance the operator interface and mission effectiveness.
  • Antenna and Sensor Installation – Expert integration of systems such as GPS, data link antennas, and other mission-critical equipment to enhance connectivity and navigation capabilities.
  • All modifications were developed in accordance with EASA Part 21J standards, ensuring seamless certification and airworthiness compliance. 
DIAMOND DA62

Multi-Purpose Platform (MPP) / Maritime Surveillance Aircraft

  • Downlink System integration DATA LINK
  • Installation of different devices inside and outside the fuselage for the transmitting and receiving of video and sensor data between different airborne platforms and ground stations, paired with an external RF front-end
  • Design and development of a customized component rack for secure installation within the baggage compartment of the Diamond DA62, ensuring optimal space utilization, structural integrity, and ease of access for system devices.
  • Installation of transmitting and receiving antennas for the data link system on the fuselage
Pilatus PC-9B Aerial Targeting Services & Close Air Support

YEAR

2013- 2017

LOCATION

HAMBURG / KIEL 

EUSKIRCHEN,

GERMANY

CUSTOMER

E.I.S AIRCRAFT GmbH

PROJECT

PILATUS PC-9B

  • Minor Structural Modifications – targeted design changes such as bracket installations, antenna mounts, and equipment supports to improve functionality with minimal impact to the airframe
  • MX-10 Underwing EO/IR Sensor Pylon with Data Link – Mechanical design, structural integration, and installation to support enhanced surveillance and reconnaissance capabilities 
  • MX-10 EO/IR Sensor Aircraft Integration – Cockpit control and display installation with full support for avionics, flight testing and certification to ensure seamless system operation.
  • NASAT Integration – Mechanical provisions for datalink terminals, display units and peripheral devices to enable robust communication capabilities.
  • IFF Combat Identification System – Comprehensive system installation for command and control platforms, ensuring secure identification and enhanced operational awareness.
  • Cockpit Modifications – Design and integration of multi-function displays, sensor displays, hand controllers and radios to enhance the operator interface and mission effectiveness.
  • SSCA System for simulated chemical attacks: mechanical development / support for production, flight testing and certification
  • Antenna and Sensor Installation – Expert integration of systems such as GPS, data link antennas, and other mission-critical equipment to enhance connectivity and navigation capabilities.
  • All modifications were developed in accordance with EASA Part 21J standards, ensuring seamless certification and airworthiness compliance. 
Logo

© 2025 Copyright E-CADO Engineering. All rights reserved.

Wir benötigen Ihre Zustimmung zum Laden der Übersetzungen

Wir nutzen einen Drittanbieter-Service, um den Inhalt der Website zu übersetzen, der möglicherweise Daten über Ihre Aktivitäten sammelt. Bitte überprüfen Sie die Details in der Datenschutzerklärung und akzeptieren Sie den Dienst, um die Übersetzungen zu sehen.