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Our skilled stress engineers can work with your engineering team to provide stress substantiation reports that match the needs of your design groups for major interior components, as well as modifications to primary and secondary aircraft structures. They are also able to provide damage tolerance analysis (DTA) reports that meet the regulatory requirements for certification. |
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This consulting service goes beyond report creation; we work hand in hand with your engineering teams to assess integrity of your designs. Our role during the design phase is not only critical, but it eliminates unproductive and redundant engineering costs that occur unexpectedly during the certification phase. The Structures team specializes in the analysis of a wide variety of aircraft repairs and modifications by combining traditional analytical techniques with the most advanced computer software technology available. |
Our experience includes:
- Complete aircraft interior analysis including interior monuments and equipment, and all systems associated with VIP interior completions
- Damage tolerance analysis for aircraft skin penetrations (antenna), bulkhead feed through, and other significant fuselage cutouts or expansions (e.g. cargo doors, jump doors, and lavatory service panels)
- Analysis of high stress zones such as engine mounts, and engine nacelle environment
- Analysis of avionic rack installations, crew/passenger seats (both static and dynamic)
- Structural test proposals and test result reports
- Structural repair of damaged aircraft and components
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