By declining demand for passenger flights during the current COVID-19 outbreak, airlines tend to use passenger cabin capacity to carry cargo to maintain aircraft productivity. These changes should be reversible and taken place by the minimum expense of time and cabin changes from passenger to cargo, and vice versa.
In this modification, the seats are removed and the loading is placed on the floor surface of the cabin and restrained with ETSO approved net
When the structure or part of the structure is damaged from crack, corrosion, fatigue, or an accident, it must be replaced or repaired to restore the load-carrying capability. Structural engineering often designs a repair with considering that all repairs should restore the damaged structure to its original ultimate strength and durability. After designing a repair, the structural engineer performs Fatigue Analysis and Damage Tolerance Analysis for repairs to maintain continued airworthiness.
Design Organization Approval certification is granted to SCA according to EASA Part 21 Subpart J requirements, to approve changes and repairs on heavy and small aeroplanes covering cabin safety, avionics, electrical systems, and structures.
FAA Form 8110-3 approval for Major Repairs and Major Alterations, including Static, Fatigue, and Damage Tolerance analysis approvals
SCA core team is comprised of the most talented and experienced aerospace, mechanics, electronics, software engineers and support staff in the industry. We support our clients from design, development and test phases through certification to manufacture. Whether you require a design change or repair or consultancy support for a new concept design or cabin modification/installation; we can provide you with the approvals support you need.
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