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Plastic materials are a good solution to reduce fuel consumption thanks to their low weight in comparison to metals.
In order to be considered for an Aircraft Interior application, interior materials have to fulfill several technical requirements designed to limit the consequences of fire in the cabin, and maintain reasonable safety levels for the passengers.
To ensure fire protection in aircraft, the Federal Aviation Administration (FAA) requires various fire testing procedures (such as FAR 25.853) to demonstrate that aircraft materials meet specific performance criteria when exposed to heat or flames.
When we consider the standard range of plastic stock shapes, high performance materials such as PEEK, PEI, PPS typically meet requirements for flame resistance without modification; on the other hand, standard materials such as PA usually do not unless they have been modified with special additives.
This is the reason why we have developed several new thermoplastic products, with a flame retardant additive: these materials are designed to meet the typical demands of aircraft interiors, and can be a lower cost alternative to high performance materials when high mechanical performance or temperature resistance is not required.
These new aircraft interior plastics tested according to FAR 25.853 are:
We offer semi-finished plastic products as rods, sheets and pipes / tubes, and keep a large stock portfolio. Custom production runs are also possible.
We have tested as well several high performance thermoplastics for flammability :
Tested to either a 60 second vertical burn test standard or a 12 second vertical burn test standard, additional smoke emission and toxicity, and heat release tests can also be done if required.
We offer a wide range of materials to cover the requirments for many applications in aircraft interior applications such as seats, lighting, galleys or cockpit equipment.
Given our ability to share these extensive test results with our customers, these “ready for use” materials truly open up new possibilities and opportunities for design improvements in commercial aircraft interiors and VIP aircraft interiors alike.
Aircraft interior materials designated for use in an aircraft cabin environment must meet certain flammability requirements.
However, it is the actual position of the part in the plane that will determine whether just the flammability test or the whole FST (Fire, smoke and toxicity) test (detailed below) is required:
Ensinger's flammability test for plastics always indicates the thickness tested, and will correspond to the thinnest wall thickness admissible on the finished machined part from our semi-finished plastics. Please refer to material data sheets to check which test was passed for a given material. Flammability test certificates are available upon request at time of order.
The test results provided on our plastic materials are a great supplement customers can use to give an indication of potential results when performing final FST tests on machined parts or their subassemblies. It definitely allows them to select quickly, and with confidence the right material for a given application.
We remain available for additional questions, and can perform additional tests if necessary: for example, we may test additional thickness for flammability if required.
In order to define more detailed instructions and safety precautions, individual aircraft manufacturers have prepared their own internal documentation, all have similar content regarding FST requirements.
Test description |
FAR 25.853 |
Airbus ABD 0031
|
Boeing
|
Flammability 60 seconds Vertical |
FAR Part 25, § 25.853 (a) and Appendix F, Part I, |
AITM 2.0002A | BSS 7230 F1 |
Flammability 12 seconds Vertical |
FAR Part 25, § 25.853 (a) and Appendix F, Part I, |
AITM 2.0002B | BSS 7230 F2 |
Flammability 15 seconds Horizontal |
FAR Part 25, § 25.853 (a) and Appendix F, Part I, |
AITM 2.0003 | BSS 7230 F3 |
FAR Part 25, § 25.853 (a) and Appendix F, Part I |
BSS 7230 F4 | ||
Heat Release |
FAR Part 25, § 25.853 (d) and Appendix F, Part IV |
AITM 2.0006 | BSS 7322 |
Smoke Density |
FAR Part 25, § 25.853 (d) and Appendix F, Part V |
AITM 2.0007A & B | BSS 7238 |
Combustion Toxicity | N/A | AITM 3.0005 | BSS 7239 |