Testing of flame retardant properties and fire protection properties of aircraft materials

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Flame retardant properties and fire protection properties of aircraft materials:

In the standard fire test, the object should have the ability to meet the required stability and/or integrity and/or thermal insulation and/or other performance requirements within a set period of time.

Aircraft Materials - Reaction to Fire:

As the name suggests, if a fire breaks out, a relatively safe place cannot guarantee safety without certainty of safety. Therefore, materials for vehicle construction and trim must be non-flammable and have a low overall release of heat, smoke, and toxic gases.

Aircraft material flame retardant test, fire test to prove

• Achieve acceptable control of fire hazard

• Achieve acceptable control of the total levels of heat, smoke and toxic gases when all major material surfaces used are exposed to a fire source

• All materials or items required to be used as fireproof panels, and materials and items required to function when exposed to fire sources, should achieve acceptable fire resistance

Aircraft fireproof materials

• Rubber products (sealing rings)

• Plastic products

• Fire retardant coating

• Fireproof glue

• Wires and cables

• Fire-resistant fabrics (curtains, seat covers, carpets, etc.)

Flame retardant test of aircraft materials, fire test - standard

• ABD 0031

• ASTM E 662

• BSS7238: Smoke

• BSS7239: Toxicity

• FAR/JAR/CS 25

• HB 5469: Combustion test of non-metallic materials inside civil aircraft cabin

• HB 7068

Airbus standard ABD 0031 test method – aircraft material flame retardant test, fire test

• Vertical combustion according to ABD 0031- 7.1.2 (AITM 2.0002 B/A)

• Combustion smoke density test according to ABD 0031- 7.3.1 (AITM 2.0007)

• Combustion smoke toxicity test according to ABD 0031- 7.4 (AITM 3.0005)

• Combustion heat release test according to ABD 0031 (AITM 2.0006)

• Horizontal combustion test according to ABD 0031-7.1.3 / -7.1.4 (AITM 2.0003):

• 45° combustion test ABD 0031- 7.1.5 performed

Far 25.853 Test Method – Flame Retardant Test of Aircraft Materials, Fire Test

• Vertical burning test is conducted in accordance with 14 FAR 25.853 b(4)), (App. F to part 25 part I § (a), 12-second vertical burning test and 60-second vertical burning test

• Smoke density test performed in accordance with 14 FAR 25.853 (d), (App. F to part 25, part V)

• Combustion heat release test performed in accordance with 14 FAR 25.853 (d), Appendix F, Part IV

• Passenger seat in accordance with 14 FAR 25.853 (c, App.F to part II)

• Horizontal combustion test performed in accordance with 14 FAR 25.853 b(2,3), (App. F to part 25 part I § (a),(1)

• Cargo rack fire test is conducted in accordance with 14 FAR 25.855 (App. F to part III)

• 45° combustion test 14 FAR 25.853 (b), (App. F to part 25, part I § (6)) performed