Nithish Kumar Mohan Email & Phone Number

Germany

• Responsible for providing technical oversight and guidance throughout the project lifecycle.• Responsible for managing team dynamics, delegating tasks, and fostering a collaborative work environment to ensure the successful execution of projects.• Providing technical expertise and guidance to resolve complex technical challenges, make design decisions, and ensure the integrity and performance of aerospace systems and components.• Identifying opportunities for process optimisation, implementing best practices.• Responsible for planning, validating and providing forecast for Input received.• Responsible for Quality deliverables and ensuring 100% OTD & FTR.• Delegation for final check and responsible for final deliverables.

Hamburg, Hamburg, Germany

1. Analyse inputs with MP, FIN Referencial, APS-NG, design improvements and IUID‘s to create prepa document for design solution.2. Creation of product structure for 928 & 929.3. 3D creation with Implementation of MP, design improvements and IUID‘s as per input preparation.4. Creation of checklist, change report and 3DXML preparation.5. Creation of FULL3D drawing set.

Hamburg, Germany

DQN CREATION, ELECTRICAL DESIGN SYSTEM INTEGRATION- A320 FAMILY AIRCRAFT.1. Study/Analyse NC’s (Non-Conformities) created by ME. Checks (TRS, DQN, VKMS, MFB, and IDV) from production areas, system installation and customization in the MCA and FAL. Propose the solution for identified non-conformity and discuss it with DO/ME. Perform Task 100 Signature.2. Creation of the necessary documents, e.g. Design Query Notes (DQNs) for ATA-92 (-928, -924 and -923), to implement the solution on the aircraft, Identification of manufacturing problems and comparison of 3D-models in the DMU as well as the valid installation documents (including the MOD process).3. Check complaint reports (NCRB) for completeness and priority, determine the MCA and FAL impact on new modifications, complaints are processed in the engineering / MAP with regard to Detailed development of technical solutions for series implementation, including Quality, deadlines, and costs from the target/actual comparison of the aircraft including Ensuring the implementation of changes on the part of the construction.LEGACY PREPARATION-ELECTRICAL DESIGN SYSTEM INTEGRATION- A320 FAMILY AIRCRAFT.1. Creating simple PRE/POST solution for NC's created for Single Aisle all standard (ST01-ST09) aircrafts.2. Analysing the possibilities of Harness installation as per NC.3. Proposing new solution for issue exist in aircraft.4. Alignment meeting with CVE and ME for the approval of LEGACY POST creation document.5. Creation of LEGACY PRE/POST document and uploading it into the tool.

Hamburg, Germany

1. Input analysis for 150% FP - Topology, ADF solution, corouting & CZ connection, 3D Morphology/variability change.2. Co-ordinating with AIB for Prepa alignment meeting for clarification and open points with ME/DO/CI responsibles.3. Creation of product structure with part zone concept with STD & OPT PZ’s for ATA929, considering Lower-Level Product structure Fundamentals of SA.4. Creation of product structure with part zone concept with STD & OPT PZ’s for ATA928 considering CI Split, PZ borders, Section split.5. Conversion of bundle from single VB Method to merged VB method.6. Calculation of diameter of bundle for 150% FP considering wire provisions for FIN to FIN concept.7. Design creation of ATA929 & ATA928 Considering all the AIB design rule and SIDP92A002D.8. Open point creation for the deviation against SIDP92A002D design rules.9. Co-ordinating with the team for the quality deliverables and clarifying technical topics for 100% quality deliverables.10. Checklist preparation for the AIB handover.

Hamburg, Germany

1. Preparation of ADF solutions by analysing all ST08 HOV‘s for Input preparation of ST09.2. Quality checker for Topology creation, coordinating customer with proposals for creation of 150% FP design.3. Analysis for removal of corouting and CZ connection.4. 3D Morphology / variability analysis to minimise the variants and to make one common STD solution for ST09.

Germany

DQN CREATION, ELECTRICAL DESIGN SYSTEM INTEGRATION- A320 FAMILY AIRCRAFT.1. Study/Analyse NC’s (Non-Conformities) created by ME. Checks (TRS, DQN, VKMS, MFB, and IDV) from production areas, system installation and customization in the MCA and FAL. Propose the solution for identified non-conformity and discuss it with DO/ME. Perform Task 100 Signature.2. Creation of the necessary documents, e.g. Design Query Notes (DQNs) for ATA-92 (-928, -924 and -923), to implement the solution on the aircraft, Identification of manufacturing problems and comparison of 3D-models in the DMU as well as the valid installation documents (including the MOD process).3. Check complaint reports (NCRB) for completeness and priority, determine the MCA and FAL impact on new modifications, complaints are processed in the engineering / MAP with regard to Detailed development of technical solutions for series implementation, including Quality, deadlines, and costs from the target/actual comparison of the aircraft including Ensuring the implementation of changes on the part of the construction.

Bengaluru, Karnataka, India

Analysing the 2D inputs.➢ Creation of 3D model of Rail components.➢ Assembly and detailed drawing creation.➢ Cross checking assembly with Environment.➢ Performing detailed check of parts and assemblies.➢ Responsible for delivering the packages.

Bengaluru, Karnataka, India

1. Implementation of TRS, DQN and RDR as per IMADE.2. Implementation of all FINs in DS as per Electrical Referential.3. Update of Backshell orientation as per Electrical referential.4. Implementation of Markers, sleeves as per SIDP rules.5. Check of continuity between PZ’s and clash free design with 928 DS.6. Upload and check in Circe and Tresti for the maturity of FIN implementation in 929 DS7. Validation of 929 DS and update of Delivery note with PZ’s and its iterations for the Manufacturing Engineering.8. Performing MCB of 929 PZ’s to know the length impact in the Aircraft to analyze any impact in the Aircraft for the changes made after installation.9. Design quality check for harness and validating.

Bangalore

1. Implementation of TRS, DQN and RDR as per IMADE.2. Implementation of all FINs in DS as per Electrical Referential.3. Update of Backshell orientation as per Electrical referential.4. Implementation of Markers, sleeves as per SIDP rules.5. Check of continuity between PZ’s and clash free design with 928 DS.6. Upload and check in Circe and Tresti for the maturity of FIN implementation in 929 DS7. Validation of 929 DS and update of Delivery note with PZ’s and its iterations for the Manufacturing Engineering.8. Performing MCB of 929 PZ’s to know the length impact in the Aircraft to analyze any impact in the Aircraft for the changes made after installation.9. Design quality check for harness and validating.

Bangalore

Intern at Engine division, HAL.