Engineer Engineering
Resume:
AREAS OF EXPERTISE
Concessions: Wings, Fuselage, Pax doors & Cargo door surroundings.
Quality checker: Electrical harness.
Team Management.
Onsite coordinator.
Modelling and Drafting: Cargo door surrounding, Brackets, Galleys.
Standard components.
Structural design modification
Configuration Management: Seating design, Galleys.
MULTIPLE PROJECT SKILLS
MODEL BASED DEFINITION of Nacelle-Reverse Thrust components.
CONCESSIONS – NCR, INCR, MRB activities, Signatory activities T100, T150, T200.
PASENGER SEAT DESIGN Configuration
INTERIOR - GALLEY G4B and G2 (Mortise and Tenon panel joints)
PART, ASSEMBLY drawings
ELECTRICAL HARNESS
CNC-Machined Parts/Sheet metal parts.
PROFESSIONAL EDUCATION
Bachelor’s in Mechanical Engineering
Omega institute of management and technology, New Delhi accredited with IEEE and KVQA – (Correspondence mode)
Diploma in Mechanical engineering
SNM Polytechnic Moodabidri (Bangalore University) – Regular mode.
CUSTOMER LOCATION EXPERIENCE:
ZODIAC Aerospace USA.
AIRBUS Broughton, UK.
BOEING, Bangalore, INDIA.
CONTACT DETAILS
NATARAJ S
Lead Design Engineer
PROFESSIONALSUMMARY:
Overall experience 14 years Aerospace industries, of which Aircraft Concession - 8 years, Manufacturing -1year, Interior and Electrical harness - 2 years and Landscape and Drip irrigation piping layout design.
Certified T200 signatory for passenger aircraft A380 wing and pylon concessions.
Implementing advance techniques and industry best practices on repair of Non-Conformance for system and components for A380, A350, SA, LR series aircrafts.
Concession design on Structural repair design of Wings and Pylon, Fuselage, Pax doors and surrounding parts, A320, A330, A350, A380 and its series.
Carrying out stack up analysis, interaction with various specialists like stress engineers, Aerodynamic specialist, Material engineer.
Experience on “Wings and Pylon” Life Cycle Engineering activities.
Model Based Design for Aircraft Engine - Nacelle components - Reverse Thrust for Airbus, Tail-cone detail parts and CARM parts for Boeing.
Electrical harness A350, A320 program Retrofit design routing clash analysis and different non-conformances checks along with UID and bracket installation decision.
Quality checks on Aircraft structural components water pipes, Flanges, Pallets and Headers, machining checks, sheet metal bending with die and mallet.
Interior galleys drawings and electrical harness bundle modification and detailing of drawing, EBOM and documents accordingly.
Catia -V5 hands-on experience 6.0 years- Sheet metal / Machined components- Assembly-Surface-Part workbench.
Aircraft interior Configuration management, product structure management and Engineering change management for passenger Seating design configuration.
KEY SKILLS:
Technical Skills:
Analyzing customer inputs and convey to the team.
Communicating with customers at onsite troubleshooting technical hurdles.
Software Proficiency: CATIA V5 R21, AutoCAD, SAP, DPDS, PRIMES, DVISE, ZAMIZ, SMARTEAM, VPM, PDM LINK SSCI, CATIA V5 ENNOVIA.
Soft skills:
Flexibility, Effective Communication, Accepting feedback, Creative thinking, work Ethic, Interpersonal Skills.
Work pressure neutralizing and Time management.
Managerial skills:
Excellent Verbal and communication, convey information clearly and effectively,
Decision making skills and problem solving abilities.
Motivate and Lead the team as and when required.
AWARDS:
Certified T200 signatory for A380 program Wings and Pylon concession project.
Airbus ID’s: A380 program “NG0ECAD” and A350: “NG4A7E4”
PROJECTS DETAILS
Project 1: MBD (Model based definition)
Client: Boeing India Pvt Ltd.
Software: CATIA V5 R21, Enovia V5.
Company: Umlaut Pt Ltd
Duration: 15th July 2019 to 15th July 2020
Project 2: MBD
Client: Bombardier – Belfast, UK
Software: Catia V5- work bench includes Surfacing, Part, Assembly, FTA, PTC Wind-chill. Searching for similar condition or reference drawings or parts in Ennovia.
Company: TechMahindra
Duration: 8th Jan 2018 to 10th July 2019
Project 3: Electrical harness
Client: Airbus - Germany
Software: Catia V5 R21.
Project 4: Aircraft interiors – Passenger Seating configuration
Client: Bombardier
Software: Catia V5 R21, Enovia V5, BDI
Project 5: Aircraft Interiors - Chromate-free primer engineering documentation incorporation.
Client: Bombardier (5000 / 6000), Canada
Software: Catia V5 R21, Enovia V5
Project 6: Aircraft Interiors
Client: Zodiac Aerospace, USA
Software used: – Primes-A380, Sap r/3,
Ennovia V5 LCS, Smart team, VPM, PDM
Company: Axis Cades Engineering Technologies Ltd
Duration: 01st April 2014to 10 July 2017
Model Based Definition, design for all structural parts, Sheet metal, Metallic parts of Tailcone and Non-Tailcone parts for Boeing Aircraft.
Analyzing parts of different material and its machining process need to update attribute and part information for sheet metal, machined components and composite parts fulfilling Functional Tolerance and Annotations.
Creating Flat pattern for sheet metal parts manually with basic as per Airbus process and methods
Creating drawings, Selection of Layouts, Generating BOM.
Electric harness DMU Fuselage A380, Clash analysis with ATA 21, ATA 53, ATA 92, segregation with types of routings, Clash analysis, Brackets / Ramp requirement checks.
Checking and decision making for UID installations for all retrofit electrical routing design. Adhere to TDD SIDP, EWIS.
Engineering change management activities, Aircraft passenger seats layout drawing creations with different configuration.
Product Release management. SDD creations, RV creations, Part and drawing creations, SDD table creations.
This activity involves in changing the finish codes for aero-interior components (galley) as per the new Standards (BAPS -710-008) set by the bombardier and also incorporate the changes specified in respective modification summary.
Investigate any existing change documentation (Mod drawing, etc.) of affecting parts.
Create new dash number for existing part (“Dash roll”) incorporating existing change management.
Involved in Interior design and development projects such as BOEING XSB/TRS program interior mortise and Tenon panel design and detailing of G4B galleys and G2 galleys.
Detailing of final assembly drawings, sub assembly, part drawings, placard installation drawings, quality check of the deliverables and integration into smart team. Creating and updating of DCN’s drawings.
Project 7: Concession Repair - Aircraft fuselage and
Airbus Helicopters - Pax doors, A350
Client: Airbus, Germany.
Software used: Catia V5, MS word, Capturing.
Role: Project Execution, Activity scheduling, Quality check, client interfacing, Team co-ordination, documenting the executing guidelines and lessons learnt.
Project 8: Concession - Aircraft Wings and Pylon, A380, SA, LR
Client: Airbus, UK & Hyde Group, UK
Software used: Zamiz, Execogate, Device (dmu), AutoCAD
Role: Mentoring Engineers, Review and authorize
Concessions, Assist management activities. Creating process chart for different Non-conformances.
Company: Quest Global Engineering Pvt Ltd
Duration: 19th July 2010 - 31st Dec 2013
Company: Infosys Technologies
Duration: Nov 2007 to Oct 2009)
Detail Design of Secondary structure for XWB-A350-900 Sec13-14 and Sec16-18 for Upper shell, Lower shell, and Paxdoor surrounds for each package following aspects were covered.
Creating manufacturing drawing for brackets installation,
Checking the interface points validation while modifying solution for Bracket Assembly for Electrical & Mechanical systems.
Creating CFRP thermoplastic clips frame and composite parts as per Airbus standards.
Checking of clash between brackets & Primary structure. Material and fastener selection for composite and brackets (loaded & unloaded). Generating Bill of Material and Implementing required DQN and IPCN.
Trimming and detailing of packing material on clashing with surrounding part.
Creating new repaired part and manufacturing drawing, for inner module, edge member, Stabilo, stringers, brackets & primary structure installation.
To represent MRB activities in aerospace production or pre-production environment utilize independent single signature authority for disposition non-conformances of aircraft structural components, systems, functional tests and Wiring /electrical installations under rapid paced production schedules.
Deputed to on-site (Broughton-UK) for a product familiarization during which I have gained knowledge on different build stages of wing manufacturing and assembly line shop floor and process.
Internal / External Defect analysis, technical discussion to reduce the defects. Re-solving customer queries / issues service bulletins and mod bulletins.
Ensure compliance with applicable of Airbus Means and Methods, ABD, CS-25, RSDP, SIDP, TDD for the appropriate.
Airbus wing component includes Skins, Stringers, Front and Rear Spar, Wing box ribs, leading edge assembly and Trailing edge assembly.
Prepare/Review design and stress solution for aircraft wing component concessions structures only.
Optimize the design solution selected based on balance of cost, quality and performance also by following application standards and working procedures and manufacturing feasibility.
Project 9: Part Modification and Drafting
Company: Unit Force Technologies
Duration: Sep 2006 to March 2007
Project 10: Landscape & Drip irrigation and fountain systems.
Client: HP Pvt Ltd, Tulips garden park –1.
Shivrame Gowda terrace garden.
Durga saffron, Parivar petals apartment.
Sundaram Claytons Vengadamahi Estate.
Hari Priya apartment, Deesha technology park.
Software used: AutoCAD, MS Office.
Role: Site survey, Design the measured layout, Client input requirement study, Layout plan
Generating drawing, prepare quotation,
schedule meeting, Negotiation project Budget.
Re-design, execution, site supervision when required.
Company: Professional Irrigation Company
Duration: 16th Feb 2010- July 2010 /
March 2007-Oct 2007
Project 11: Airbus –Traverse beam Assembly,
Lower Hinge Arm Assembly,
Die Design for Elliptical Pallets & Headers
Client: Hindustan Aeronautic Limited, Bangalore.
Gigani Casting Industry, jigani Bangalore.
Software used: Catia V5,
Role: Quality control engineer.
Company: Venkateshwara Engineering Works
Duration: July 2005 to Sept 2006
Personal Details:
Skype ID: natarajshetty20
LinkedIn ID: https://www.linkedin.com/in/nataraj-shetty=b9958638
Facebook ID: adjlz3@r.postjobfree.com
LANGUAGE KNOWN:
DOB:
Passport No:
Passport Date of issue:
USA VISA:
The Scope of work in this project includes, modification of main components of gear box viz. main shaft, idler shaft, lay shaft, gear wheels and gear case housing were modeled from 2-D drawings. Assembly build, clearance and interference checks were also done. Worked on projects for conversion of 2D to 3D
The Scope of work in this project includes, end-to-end solution provider for Landscaping and water management systems. The main distributors of JAIN IRRIGATION COMPANY
Layout plan proposals, and 3-D virtual design schemes using AutoCAD.
Sprinkler Layout – Piping Layout designing, Optimization of pipe lengths for a given Farm house/Landscape configuration.
Creation of BOM, Quotation, Client interfacing, Executing the project, design version/revision control & approval activities in conjunction with the Client.
Assistance to field deployment team.
The Scope of work in this project includes, drafting support on main components of Airbus traverse beam, Jaguar, lower hinge arm assembly, die design for pallets and header model from 2-D drawings, Assembly build and clearance and interference checks were also done. GD&T requirements to be fulfilled.
Drilling, Filing, de-burring, spot-facing, surface finishing, maintaining bins for raw materials.
Part modeling, assembly and drafting with GD&T was done to develop the product by using CMM- Prototype Method.
English, Hindi, Kannada, Tulu, Telugu.
20th Apr 1983
J8445488
29/8/2011.Date of Expiry: 28/8/2021.
H8689191 Issue Date: 11 Jul 2014 Expiry Date: 09 Jul 2024, VISA TYPE: B1/B2
DECLARATION:
I hereby declare that all of above information is correct to the best of knowledge.
Date: /12/ 2020
Place: Bangalore NATARAJ.S
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