Team Leader
AXISCADES TECHNOLOGIES LIMITED
Total years of experience :13 years, 9 Months
Currently working on Aircrafts area:-
Single Aisle family (A318, A319, A320, A321-CEO and NEO)
- Central fuselage Section15
- Center wing box Section21
- Air inlet area- Nacelle component
Long range (A330-200, A330-300, A330-900 A330-200F CEO and NEO)
- Central fuselage Section15
- Center wing box Section21
- Air inlet area- Nacelle component
A350XWB
- Air inlet area- Nacelle component
A400M (Airbus Military aircraft)
- Center wing box
Area: Central fuselage -Section15, Center wing box-Section21 and Nose section
Type of work: Structural non-conformity/defect such as dent, impact, fastener oversize occurred on aircraft panel, frame, stringer and other parts, for that providing the static and fatigue justification after design repair solution is proposed or reworks solution performed in Plants Assembly line. (In AIRBUS PLANTS Saint-Nazaire, Nantes and Toulouse)
Tools used: ISAMI-Xpress (Static), ISAMI-Analyst (fatigue), Zamiz, MS Excel and word templates, Airbus documents and other related standard documents, Airbus standard drawings
Job title: Lead engineer
Duration: From 15-october-2010 (offshore Bangalore, INDIA)
From 2012 to 2014 (Onsite Toulouse-AIRBUS PLANT, FRANCE)
From 2014-2017 (offshore Bangalore, INDIA)
From 2017-2018 (Onsite Saint Nazaire-AIRBUS PLANT, FRANCE)
From 2018-till date (offshore Bangalore, INDIA)
Structural non-conformity/defect such as dent, impact, fastener oversize occurred on aircraft panel, frame, stringer and other parts, for that providing the static and fatigue justification after design repair solution is proposed or reworks solution performed in Plants Assembly line. (In AIRBUS PLANTS Saint-Nazaire, Nantes and Toulouse)