|
Airbus A220 |
Analysis |
Computer-aided Design: 3D to 2D drafting for the Bombardier C-Series Thrust Reverser Actuation System components; Testing Services: Thrust reverser components, finite element analysis |
|
Airbus A320 |
Analysis |
Fatigue Testing: Skin-rib-stringers and spars, F&DT; Stress Analysis: Sharklet, fixed trailing edge and leading edge panel support structure (buttstraps), static analysis. Design and type certification stress analysis of FLE and FTE structures; Fatigue Testing: Static and fatigue analyses on A320 family spar flanges and butt strap joints for the use of oversize fasteners. Also, nose and main landing gear structures |
|
Airbus A330 |
Analysis |
Fatigue Testing: Aileron & spoiler support structure, flap support structure, skin-centre spar. F&DT (A330-200 - F); Stress Analysis: Design and type certification stress analysis of FLE and FTE structures |
|
Airbus A350 |
Analysis |
Computer-aided Design: Conversion of A350XWB fuselage brackets; Stress Analysis: Supported Messier-Dowty in the optimization of main landing gear structures (A350-900) |
|
Airbus A380 |
Analysis |
Certification Services: Certification analysis of the lower leading edge composite panel; Stress Analysis: Rear spar, static test; Fatigue Testing: Rear spar, F&DT; Certification Services: Inboard fixed leading edge lower panels and inboard outer fixed leading edge upper & lower panels. Composite certification; Testing Services: A380-800 fixed leading edge composite panels, finite element analysis; Stress Analysis: Design and type certification stress analysis of FLE and FTE structures |
|
Airbus A400M |
Analysis |
Stress Analysis: Design and type certification stress analysis of FLE and FTE structures; Fatigue Testing: Aileron support structure, spoiler support structure, F&DT. Also, nose and main landing gear structures |
|
BAE Systems Hawk 100 |
Analysis |
Fatigue Testing: Fatigue life assessment |
|
Leonardo AW101 |
Analysis |
Stress Analysis: Civil 510 static stress analysis of the foward fuselage region |
