Sebastien Adam

System Engineer at Pilatus Aircraft Ltd
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Contact Information
us****@****om
(386) 825-5501
Location
Beckenried, Nidwalden, Switzerland, CH

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Experience

    • Switzerland
    • Aviation and Aerospace Component Manufacturing
    • 700 & Above Employee
    • System Engineer
      • Feb 2016 - Present

    • Germany
    • Industrial Machinery Manufacturing
    • 400 - 500 Employee
    • Production test engineeer
      • Jul 2008 - Jan 2016

      Design of flight control computer production testsWriting of the embedded test software specifications and C-language code for the following systems :Airbus A320 Slat/Flap Control Computer (SFCC)Airbus A350 Slat/Flap Control Computer (SFCC)Airbus A350 Common Remote Data Concentrator (CRDC)Airbus A350 Flight Control Unit (FCU)Writing the specification and the C-language code of the embedded communication protocol (MICBAC) used during production test for data exchange between the test bench and the system under test.Writing of the embedded test software specifications and C-language code for a test bench component. (Ethernet interfaced load simulation board).

    • France
    • IT Services and IT Consulting
    • 700 & Above Employee
    • System Engineer
      • Feb 2008 - Jun 2008

      Working under LINUXSRSA Validation Procedures writingValidation of the system prototype in the Mont de Marsan French Air Force BaseInterface between CS and customer Working under LINUXSRSA Validation Procedures writingValidation of the system prototype in the Mont de Marsan French Air Force BaseInterface between CS and customer

    • France
    • Aviation and Aerospace Component Manufacturing
    • 700 & Above Employee
    • System Engineer
      • Mar 2007 - Jan 2008

      Integration of the core system of the Rafale aircraft: the Modular Digital Process Unit (MDPU)Suppliers are followed up for the Problem Report solving activityRetrofits managementSupport to the users. Integration of the core system of the Rafale aircraft: the Modular Digital Process Unit (MDPU)Suppliers are followed up for the Problem Report solving activityRetrofits managementSupport to the users.

    • Engineering and design engineer
      • Jul 2006 - Jan 2007

      Organzation and constitution of the electric folder for a military vehicle (Car electricity, industrial electrics, automats, GSM, GPS)Writing of documents for the maintenance in operational condition of the electric installationContribution to improvements of the electric design of the vehicle. Organzation and constitution of the electric folder for a military vehicle (Car electricity, industrial electrics, automats, GSM, GPS)Writing of documents for the maintenance in operational condition of the electric installationContribution to improvements of the electric design of the vehicle.

    • Lab Test System Engineer
      • 2006 - 2006

      2 months for the Acceptance Test Procedure (ATP) design and integration for the British Aerospace (BAES) Flight Control Computer (FCC) of the Aer Macchi M346. It includes the design of a MIL-STD-1553 bus analyzer, an ARINC-429 bus analyzer and LVDT – RVDT (position sensors of the aircraft control surfaces) simulation tools.2 months for the transfer of the previous procedure for the Italian FCC and its integration. 2 months for the Acceptance Test Procedure (ATP) design and integration for the British Aerospace (BAES) Flight Control Computer (FCC) of the Aer Macchi M346. It includes the design of a MIL-STD-1553 bus analyzer, an ARINC-429 bus analyzer and LVDT – RVDT (position sensors of the aircraft control surfaces) simulation tools.2 months for the transfer of the previous procedure for the Italian FCC and its integration.

    • Lab Test System Engineer
      • 2002 - 2006

      Test of the training aircraft AerMacchi M346 Flight Control System (FCS)Design of the integration procedures of the Flight Control Computer (FCC) equipment interface with the following equipment :- Cockpit Control Panels : pilot interface with the Flight Control System (FCS)- FCS 1553 data bus : FCC interface with the FCS sensors- Avionics 1553 data bus : FCS interface with other aircraft equipment- 1553 end to end : data transfer from one bus to the other- Power-Up Built In Test (PUBIT)For each of the previous topic, the following process has been applied :- Design of the automatic test software with National Instruments Labview 7.1- Integration on the Equipment Test System (ETS)- Problems reporting, interface with customer and supplierTest requirements and procedures are managed with Telelogic DOORS 6.0

    • System Engineer
      • Jan 2001 - Jun 2002

      Writing of the specifications of the generation and transmission chains of a Multi Function RADAR (MFR).Design of the power supply card of the pre-amplifier of the MFR.Defense confidential projectWriting of the specifications of the equipments of the generation-reception chain of the RADAR signal.2 months to design and draw the electric diagrams of the power supply card of the MFR transmitter pre-amplifier until the release of the card prototype. Writing of the specifications of the generation and transmission chains of a Multi Function RADAR (MFR).Design of the power supply card of the pre-amplifier of the MFR.Defense confidential projectWriting of the specifications of the equipments of the generation-reception chain of the RADAR signal.2 months to design and draw the electric diagrams of the power supply card of the MFR transmitter pre-amplifier until the release of the card prototype.

Education

  • Ecole supérieure d'Ingénieurs en Génie électrique
    Diplôme d'ingénieur - Master degree, Graduate school of electrical engineering, Specialization in Electronics, Telecom, Microwaves
    1997 - 2000

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