If you have a TSO seat and desire to follow AC 21-25A, Skandia can provide guidance. i. Any part 25 aircraft certified after 6/16/88 requires either 16g seats that meet TSO-C127a or seats meeting 14 CFR 25.562 that are TC to the aircraft. Davis Junction, IL – Skandia, Inc. announced today that it has completed Airbus certification requirements and is now approved as an authorized provider of flammability testing … Specimen size is 12.5” x 23” for flexible materials; 11.5” x 23” for rigid materials and 4” x 12” for hook and loop fasteners. Footrests and headrests that are made up of substrate and dress cover only would have to be tested to 14 CFR 25.853(a)(ii) as a composite assembly. “Earning this accreditation is a major accomplishment for Skandia. Seat components that are upholstered such as armrests, shrouds, back shells, etc. There are some solutions such as using a fireblocker, but industry does not want the cost of adding fireblocker. “The ISO 17025:2005 certification is not something that is easily earned. It is the responsibility of the upholsterer/fabricator to ensure that the work performed is compliant with the original certification. have to be tested in the “as installed state” which includes substrate, foams, glues, dress cover material, etc. Skandia, Inc. vice president Jarod Triplett announces that the company’s advanced flammability testing laboratory has earned the prestigious ISO 17025 accreditation through American Association for Laboratory Accreditation (A2LA) designation. Drippings from the test specimen may not continue to flame for more than an average of 5 seconds after failing. Part 23 aircraft – radiant panel testing, b. Our commitment to quality ensures services are performed accurately and products arrive at our customer’s dock on time, with the required documentation. h. What if I cannot provide the substrate and the fsdo/aco won’t let me use a surrogate? In addition to meeting the requirements of paragraph (a) of this section, seat cushions, except those on the flight crew member seats, must meet the test requirements of Part II of the appendix F of this Part, or other equivalent methods, regardless of the passenger capacity of the airplane. - Skandia, Inc. announced today that it has completed Airbus certification requirements and is now approved as an authorized provider of flammability testing and certification services for both the manufacturer, as well as independent Airbus authorized completion centers and maintenance, repair and overhaul (MRO) facilities. 14 CFR 25.562 became effective May 17, 1988 (Amendment 25-64) requiring dynamic testing of seats. These requirements incorporate the foam cushion build-ups and dress cover materials as an integral part of the seat certification. Those that won’t may require samples to be cut from the part to be tested. “We have so many customers around the world and they each require specific testing requirements. For additional information: www.epa.gov/EPA-IMPACT/2007/January/Day-12/i338.htm. Any time you are refinishing cabinetry, composite testing is required. Additional reference materials are Advisory Circulars AC 25.853-1, AC 21-25A, AC 23-2 and Aircraft Materials Fire Test Handbook DOT/FAA/AR-00/12. Part 25 aircraft – radiant panel testing; c. Radiant panel testing summary; d. … If you are replacing thermal/acoustic insulation, you are not required to meet this rule. Aug. 22, 2013, Davis Junction, Il. Flammability testing will always be required when changing materials, but this is not the only requirement. A separate procedure has been developed to show compliance for the use of tape. Specimen sizes are 4” x 12”. k. What has to be tested if we are just changing the finish? Skandia, headquartered in Davis Junction, Illinois, is a leading provider of highly engineered seating foam, foam fabrication, flammability testing … If tape is to be tested, please follow specimen fabrication of draft Advisory Circular 25.856-1 on the Fire Tech Center. 14 CFR 25.853 (c) c. 14 CFR 25.853 (d) d. 14 CFR 25.853 (h) e. 14 CFR 25.856 (a) f. Features & benefits; g. Quality assurance; h. Flammability testing ; 5. You will have to get guidance from your FSDO. Skandia is the global leader in providing aviation flammability engineering & testing services. Skandia is completing its repertoire of flammability tests with the addition of heat-release and smoke-density equipment for heat, smoke and toxicity testing capabilities. If the aircraft has 20 or more seats, then it would also have to meet 14 CFR 25.853(d) is the Heat Release. “ISO 17025:2005 is specifically created for laboratories conducting testing and calibrations. Content How can we help? m. Can I get an FAA 8110-3 form for this test? (horizontal), (b) Test Procedures–(2) Specimen configuration. Headliners, window liners, and sidewalls all have to be tested to 14 CFR 25.853(a)(i) 60-second vertical test. This information is for guidance only and any specific questions should be directed to your local FAA FSDO or ACO office. The global company works in aircraft cabin component testing, development, production … 60-second Vertical Test. An 8110-3 can only be issued when a burn test is in support of an FAA project or in support of a major repair or alteration. With the highest FAA certifications and approvals, our trusted, highly trained technicians utilize state-of-the-art equipment to satisfy all your flammability testing, engineering, conformity and certification needs. FAA STC for Global 5000… September 2020. Some aircraft manufacturers include the dynamic seat approval on the aircraft Type Certificate (TC). Skandia Inc. Receives EASA STC… August 2019. Step 2: Testing & Fabrication 14 CFR 25.853 (a) b. 14 CFR 25.853(a) is the Vertical Burn requirement. Confidence is extremely important to them.”, “There are a number of accreditation auditors/services we could have used, but we knew that A2LA is held in the highest regard by the industry,” stated Jeff Vardell, Skandia’s Quality Assurance Manager. In order to determine what the seat is certified to, we suggest you inspect the seat frames for TSO tags and also review the aircraft Type Certificate Data Sheet (TCDS). No, only new materials being installed after September 2, 2005 have to meet this requirement. As of September 2, 2005, the new FAA standard for Thermal/Acoustic materials used in Transport Category Airplanes went into effect per www.fire.tc.faa.gov/pdf/handbook/00-12_ch24new.pdf. Flammability testing services to determine the resistance of materials to flame. These standards include new flammability tests and criteria that address flame propagation and entry of an external fire into the airplane. Composite panel burn testing and why it is required. For Part 25 aircraft at Amendment 25-66 (9/26/1988), aircraft must meet the requirement of Part V for Smoke Density. You would need to cut enough material from existing panels to perform the testing and then make a repair to replace what was used. See page 16, www.epa.gov/EPA-IMPACT/2007/January/Day-12/i338.htm. Test specimens of materials that must meet the requirements of Paragraph (a)(1)(v) of Part I of this appendix must be no more than 1/8-inch in thickness. These requirements only apply to aircraft with a capacity of 20 or more passengers. Capabilities include oil burner, vertical burn, horizontal burn, 45 degree burn, 60 degree burn, and aircraft blanket fire testing. Skandia currently performs about 70 percent of all aviation flammability testing in the world, with its main focus on the business aviation market. Skandia INC 5000 N Highway 251 Davis Junction IL 61020 Phone: 815.393.4600 info@skandia.com 1 Seat Fireblocing Checlist Flammability Testing & Certification Step 1: General Information Please enter all the general information and aircraft fields below. Seats manufactured to meet Dynamic test criteria have additional requirements or restrictions. For each compartment occupied by the crew or passengers, the following apply: Materials (including finishes or decorative surfaces applied to the materials) must meet the applicable test criteria prescribed in Part I of Appendix F of this part, or other approved equivalent methods, regardless of the passenger capacity of the airplane. “Many aircraft owners and operators choose to alter seating systems by incorporating such features as different upholstery. - Skandia, Inc., announced today that it has completed the across-the-board implementation of the FAA’s new Policy Statement: PS-ANM-25.853-01, also known as “Flammability Testing of Interior Materials.” Large cabinets and cabin stowage compartments, other than underseat stowage compartments for stowing small items such as magazines and maps. It was developed for what was considered large volumes of foam. What kind of test is it? Electrical wire and cable specimens must be the same size as used in the airplane. Cabinetry, bulkheads, and any large structures have to meet the requirements of 14 CFR 25.853(a)(i) 60-second vertical testing. Skandia’s systems, equipment, engineering test planning and processes were analyzed in an extensive on-site review. These seats would have been manufactured to either TSO C127A or 14 CFR 25.562. Rapid turnaround times result from our in-house staff of DERs and DARs with the authority to perform conformity inspections and issue 8110-3 flammability certification. 14 CFR Part 25 Appendix F Part I and Part II, Aircraft Materials Fire Test Handbook DOT/FAA/AR-00/12, Advisory Circular AC 25.853-1 Flammability Requirements for Aircraft Seat Cushions, Advisory Circular AC 25-17A Transport Airplane Cabin Interiors, Advisory Circular AC 21-25A Approval of Modified Seating, Systems Initially Approved under a Technical Standard Order, Citation seats are covered under the aircraft TCDS (Type Certificate Data Sheet), Mustang, Model 510 (Normally Category Part 23) (see TCDS note 4), 2000EX (2000EX EASy and 2000DX are still 2000EX with additional modification packages for marketing designation), 12- and 60-Second Composite Panel Testing, Radiant Panel Testing with DER Certification, Re-qualify Existing Foam Cushions with New Dress Covers. The new rule, 14 CFR 23.856, is the same test and requirements as defined in 25.856(a) which is for flame propagation testing. Even minor changes, such as changing the leather color, are considered a modification to the seat and its certification. g. I’m just replacing the dress cover material on the headliner so can’t I just use single element vertical burn test results for that? Drippings from the test specimen may not continue to flame for more than an average of 3 seconds after falling. » Services » Flammability Testing & Certification » chamber. Airbus has granted additional testing approvals to Skandia’s flammability laboratory. Per the Advisory Circular, under certain conditions, we are given the latitude to apply the burner flame for 30 seconds or 60 seconds. If neither is willing to provide guidance, then the FAA Advisory Circular 21-25A “Approval of Modified Seating Systems Initially Approved under a Technical Standard Order” would need to be followed. 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