- Installed in aircraft since 2009;
- The result of 10 years of R&D;
- Supported by our full engineering services;
- Business or Commercial: FAR 25.853 {14CFR25.853(a) App. F(a)(1)(I)} (60 seconds vertical test);
- Includies OSU 65/65 heat release requirement;
- Standard shapes or designed to specifications;
- Typical panel construction: 2-Core-2 fiberglass configuration, made with foam core, fiberglass facing and fire retardant resin systems. 5-axis CNC machining available.
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