Ingegnere aeronautico

Support of the production:
(MRR/MRB) on  GE-90, GEnx-1B, GEnx-2B, PW2037,
TRENT-900, 146SAM146 and V2500 ADTs program Avio

Stress lead analyst on Boeing 787-8 program.
Static analysis of part of the horizontal stabilizer
The parts are in metallic
The analysis have been performed hand calculation (BDM) with tools Boeing and fem detail analysis

Stress lead analyst on C27J program.
Static analysis of system parts.
The parts are in metallic
The analysis have been performed hand calculation (Niu,Roak and Bruhn) and fem detail analysis.

Stress lead analyst on Meltem program.
Static analysis of system parts sec.11, 15 and sec.18.
The parts are in metallic
The analysis have been performed hand calculation (Niu,Roak
and Bruhn) and fem detail analysis

Activity of concession on A380 AIRBUS program.
The analysis static and fatigue have been performed on all
parts of the fuselage with aribus tools.

Stress lead analyst on B787 -9 program.
Static analysis of system parts sec.44 and sec.46.
The parts are in metallic
The analysis have been performed hand calculation (BDM ,Niu,Roak and Bruhn) with Boeing tools and fem detail analysis.

Stress lead analyst on B787 -9 program.
Static analysis of system parts sec.44 and sec.46.
The parts are in metallic
The analysis have been performed hand calculation (BDM
,Niu,Roak and Bruhn) with Boeing tools and fem detail
analysis.

Stress lead analyst on Meltam program.
Static analysis of interior parts example: Bin, Wardrobe, toilete,
Side panel and secondary structures
The parts are honeycomb, composite and metallic
The analysis have been performed hand calculation (Niu,Roak
and Bruhn) and fem detail.

Stress analyst on Boeing 787-9 program.
Static and fatigue analysis of primary structure of sect 46 of
fuselage.
The analysis have been performed hand calculation (BDM) with Boeing tools and fem detail analysis.
The parts are in metallic.

Stress lead analyst on Suhkoi program. SSJ100
Static analysis of interior parts example : Sidewall Panel , dado
panel, Bin, surround door, door and secondary structures
The parts are honeycomb, composite and metallic
The analysis have been performed hand calculation (Niu,Roak
and Bruhn) and fem detail.

Stress analyst on Bombardier C Series 700/800 program.
Static analysis of all part avionic door.
The analysis have been performed hand calculation (Niu,
Roak, Bruhn and EDS) and fem detail analysis.
The parts are in metallic

Stress analyst on Boeing 787-9 program.
Static and fatigue analysis of part of the primary structures same
as:
Keel Chord Extension, Frame and shear Tie and secondary
structure (es. Fitting) of sect 44/46 of fuselage.
The parts are in metallic and composite.
The analysis have been performed hand calculation Boeing
tools, BDM and detail analysis

Project leader on Boeing 787-8 program for two work packets
complete ( from parts design to parts production) WP#17 and
WP#18 . Configuration management and support of the
production (MRR).Stress Lead analyst on Boeing 787-8
program. Static and fatigue analysis of Keel Chord Extension
and secondary structure (es. Fitting ) of sect 46 of fuselage.
The analysis have been performed hand calculation (BDM) with
Boeing tools and fem detail analysis

Activity of MRR on Boeing 787-8 program (Grottaglie Alenia
Composite)
Static and fatigue analysis on all parts sect 44/46 of fuselage.
The analysis have been performed hand calculation (BDM) with
Boeing tools.The parts are in composite and metallic

Configuration management and support of the production
( MRR) on Boeing 787-8 and -787-9 program.

Project leader on Boeing 787-8 program for two work packets
complete ( from parts design to parts production) WP#17 and
WP#18 .
Configuration management and support of the production
( MRR)
Stress Lead analyst on Boeing 787-8 program.
Static and fatigue analysis of Keel Chord Extension and
secondary structure (es. Fitting ) of sect 46 of fuselage.
The analysis have been performed hand calculation (BDM) with
Boeing tools and fem detail analysis

Stress analyst on Airbus 380 program.
Static analysis, primary structures es.Frame

Stress analyst on Airbus A321 program.
Static analysis of parts of the SEC14 , in particular floor zone
es. floor beam , structural vertical etc.
The parts are in metallic.
The analysis have been performed with FEM details and hand calculation.

Aerospace Engineer Degree (98/110 )