Enise Sarikaya

• • Electrical wiring and system design for VIP aircraft (AIRBUS and BOEING).

• • Electrical wiring diagram preparation.

• • Electrical load and voltage drop analysis.

• • Electrical harness manufacturing and installation requirement design.

• • Electrical harness test documentation.

Achievement:

• • Contributing to the design and certification of VIP aircraft electrical systems on AIRBUS and BOEING platforms, ensuring compliance with aerospace standards.

• • Preparing detailed electrical wiring diagrams in accordance with aerospace and EWIS requirements.

• • Performing accurate electrical load and voltage drop analyses, supporting safe and reliable system operation.

• • Producing technical test and verification documentation.

• • Developed electrical wiring interconnection systems (EWIS) and prepared harness manufacturing and installation documentation.

• • Supporting project milestones through timely and high-quality delivery of technical documentation.

On behalf of AIRBUS System Engineer for ATA29&ATA32. Technical Assistant LIEBHERR Aerospace SAS ECS team System Design Engineer On behalf of AIRBUS 1YYS team Model Developer for ATA24. On behalf ofAIRBUS 1YYS team Model Specialist for ATA24/35/42. On behalf of AIRBUS Modeling Project Leader for ATA35/42 in A320 family and A350. On behalf of VOLOCOPTER Validation & Verification Engineer(DO-178C) for Avionics& Flight Control Achievement:

• • HLR and LLR traceability according to DO-178B and ARP4754

• • Model Developing and HILR testing for ATA21&ATA36

• • WIR (electrical wiring) Model Developing for ATA24 via SCADE tool.

• • Validation and Verification of the developed models using industrial programs.

• • VSIM-I platform model test for ATA24/35/42 in A320NEO, A330NEO,A340 and A350. is a simulation

• • VSIM-D platform model test for ATA29/32 in A320 family, A350 and A380.

• • Preparation of test procedure and test report.

• • System Design Engineer for ATA22/24/33.

• • Designed aircraft electrical equipment and systems, including APU interfaces, starter-generators, and battery systems.

• • Designed and developed architecture of aircraft electrical power systems (ATA 24), ensuring efficient power generation, conversion, and distribution across all aircraft systems.

• • Performed system-level design, integration, and validation of generators, TRUs, inverters, and battery systems.

• • Ensured compliance with airworthiness and safety standards during system design and integration.

• • Preparation of system requirement documents for ATA22/24/33/27 (SRD,SIRD,SDD,SWRD,AWSS, Technical Specification(TS),ICD).

• • Modeling and simulation of data from avionic equipment and actuators for Flight Control Computer in TAI ATAK, GÖKBEY, T70 helicopters.

• • Real-time testing of models developed for ATA22/27.