Mag. Nihad Ajdinovic

Specialize in the static and fatigue analyzes of the primary and secondary structure such as: Doors (Main Entry Door, Baggage, Emergency Exit Door, Main Landing Doors) and mechanisms. Sizing of the fuselage panels that include: major frames, longerons, skin-stringer panels. Analysis of the wing spars and wing to fuselage interface fittings. Carry out horizontal stabilizer sizing: composite spars and skin-stringer panels, metallic ribs and fittings. Support nacelle-redesign including composite cowl doors.

Carry out the structural sizing of the metallic and composite components part of the Wing to Body Fairing (WTBF) of Boeing 787-8/-9 airplane models. The structural sizing includes but not limited to static, fatigue and durability for the frames, intercostals, (MLGD) and composite panels. Review and approve Catia models for the release and production. Develop the analysis tool and organize training for the entire team. Document all analysis in support of the FAA certification for the WTBF section.