Munich, Bavaria, Germany
- lead certification process for Electrical System. - lead certification process and lead development activities for HIRF/ Lightning/ EMC - provide support to aircraft systems design and certification, for both electrical and electromagnetic aspect.
- Accountable for the powertrain design and certification. - Drive and coordinate the design and certification effort for the E3 aspects of the aircraft. - Lead cross functional system activities for E3 and Powertrain integration. - Provide guidance on strategic decisions for all aircraft systems.
-Manage a team of 5 engineers for the PC-24 data concentrator. I plan the validation and verification of requirements and coordinate the software integration effort from software team to flight testing. The role involves the management of problem reports with JIRA and drive the team to solve problems and improve system requirements (DOORS). -Responsible for the PC-24 electrical system, flaps system integration and software testing. -EMC, HIRF and Lightning Expert for all Pilatus aircrafts, which includes safety analysis, certification documentation, rig building and planning. -Responsible for the PC-24 electrical system management.
-Responsible for the PC-24 electrical system continuous development and fleet support. -EMC HIRF and Lightning expert for all Pilatus aircrafts. Which includes safety analysis, certification documentation, rig building and planning. -Accomplish certification of the PC-24 electrical system and the Electromagnetic and Lightning certification. -Provide support to electromechanical system design. -Responsible for the development of electrical and system requirements in DOORS.
-Lead the PC-24 electrical system requirement management (DOORS) and its aircraft integration. -Responsible of the design, liaison with supplier, testing and qualification of the secondary power distribution. -Drive certification activities ( SOI) with certification authorities EASA and FAA for level A "function critical" systems. -Provide support to electromechanical system design and coordinate information across engineering teams.
-conception and design of hardware for RIU (aircraft data concentrator) -build electric test bench to save company >50000£ of external development cost. -conduct PCB design and hardware certification test for Gulfstream G650 RIU. -write test procedures and synthesis of certification items for DO-160G testing. -leading design of new Electrical Landing Gear actuator and coordinating with Nottingham University research department for the development of the integrated FPGA to DO-254 standards. -solution finding for Military Units such as HAWK and V22 RIUs.
-fault finding on A320 electrical systems. -build simulation on Flowmaster of A400M in-flight refueling probe. -wrote concept report for usage on A350 of new generation CAN bus.