Each type of tape requires qualification on each material on which it is used. The average burn length may not exceed 6 inches and the average flame time after removal of the flame source may not exceed 15 seconds. All 16g aircraft seats are certified for use in aircraft as a complete upholstered seat. As our business continues to grow it will ensure our … Single element vertical burn tests do not meet all of the requirements for installing materials in aircraft or on aircraft seating. You would need to cut enough material from existing panels to perform the testing and then make a repair to replace what was used. For transport category airplanes type certificated after January 1, 1958: From Part 121 – Operating Requirements: Domestic, Flag and Supplemental Operations §121.312 Materials for Compartment Interiors: The FAA extended, by 24 months, the date for operators to comply with the fire penetration resistance requirements of thermal/acoustic insulation used in transport category airplanes manufactured after September 2, 2007. Part 23 aircraft – radiant panel testing; b. If you have a TSO seat and desire to follow AC 21-25A, Skandia can provide guidance. Skandia’s flammability engineering, testing and certification department has two newly appointed Designated Engineering Representatives (DERs). 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. The global company works in aircraft cabin component testing, development, production … (12-second burn), (iv) Clear plastic windows and signs, parts constructed in whole or part of elastomer materials, edge lighted instrument assemblies consisting of two or more instruments in a common housing, seat belts, shoulder harnesses, and cargo and baggage tie-down equipment, including containers, bins, pallets, etc., used in passenger or crew compartments, may not have an average burn rate greater than 2.5 inches per minute when tested horizontally in accordance with the applicable portions of this appendix. “When our customers see the A2LA logo on our documents they will have every confidence that the testing they receive from Skandia is done at the highest level of detail and will meet any regulation they require.”. Skandia INC 500 N Highway 251 Davis Junction IL 102 Phone: 15.393.460 info@skandia.com 1 OSU Heat Release and Smoe Emission Flammability Testing & Certification FAA Form 8110-3 may only be issued aircraft specific for U.S. registered or U.S. state of design aircraft using 14 CFR regulations only Step 2: Test Data Step 1: General Information Please enter all the general … 14 CFR 25.853(c) is for the seat cushions (backrest, bottom cushion, footrest, and headrest). 14 CFR 23.856 Thermal/Acoustic insulation materials states – “Thermal/acoustic materials installed in the fuselage must meet the flame propagation test requirements of part II of Appendix F to this part or other approved equivalent test requirements. Seats manufactured to meet Dynamic test criteria have additional requirements or restrictions. The edge to which the burner flame is applied must not consist of the finished or protected edge of the specimen but must be representative of the actual cross-section of the material or part as installed in the airplane. Skandia Announces New Improved Damping Product Line: AeroDamp Advanced. These seats would have been manufactured to either TSO C127A or 14 CFR 25.562. Mackenzie Kacvinsky, flammability department manager, and Jennifer Asbury, flammability supervisor, were awarded DER status by the FAA. Skandia is one of the aviation industry’s most recognized and respected FAA and EASA approved Flammability Testing laboratories. The average burn length may not exceed 8 inches, and the average flame time after removal of the flame source may not exceed 15 seconds. Many of the thermal/acoustic insulation materials are used in combinations and must be tested in a composite build-up form. “We are growing the on-staff engineering capacity … Skandia’s systems, equipment, engineering test planning and processes were analyzed in an extensive on-site review. This requirement does not apply to “small parts,” as defined in Part I of Appendix F Part 25. The pre-amble of rule 25.853 exclude seats from the requirements of Part IV and Part V. However, with the invention of larger seats with integral stowage compartments and other console assemblies, the FAA has issued additional guidance. Those that won’t may require samples to be cut from the part to be tested. also require flammability testing which Skandia can also perform. Skandia is one of the aviation industry’s most recognized and respected Flammability Testing laboratories, conducting testing in accordance with FAA, EASA and numerous other civil air … m. Can I just get an FAA 8110-3 for stock so that I can use the material or composite in many different aircraft? k. What information is needed for testing to 14 CFR 25.856(a)? See page 16. See page 16, www.epa.gov/EPA-IMPACT/2007/January/Day-12/i338.htm. On aircraft seats that have to meet 14 CFR 25.562, flammability testing is just part of the overall process when reupholstering these seats. 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. “As our business continues to grow it will ensure our customer base is confident that we meet the … Large cabinets and cabin stowage compartments, other than underseat stowage compartments for stowing small items such as magazines and maps. Flammability Flammability Testing and Certification is similar to non-dynamic seats and can be performed by Skandia. Aug. 22, 2013, Davis Junction, Il. Davis Junction, IL – Skandia, Inc., Vice President, Jarod Triplett announced today that the company’s advanced flammability testing laboratory has earned the prestigious ISO 17025:2005 accreditation through American Association for Laboratory Accreditation (A2LA) designation. Radiant Panel Testing for Thermal/Acoustic Insulation, 7. a. In this case, there may not be a TSO tag on the seat, however, the seat could be dynamic certified and you should contact the aircraft manufacturer for guidance. 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. Skandia Inc. Receives EASA STC… August 2019. “We are … a. This testing would have to include the cabinet structure, materials being added, glues used to attach, any finish material such as stains, paints, clear coat, etc. Part 91 Aircraft only require 14 CFR 25.853 (c) if they have 16g seats. “The ISO 17025:2005 certification is not something that is easily earned. Additionally, Advisory Circular AC21-25A provides guidance utilizing a DER with 14 CFR25.562 authorization to generate acceptable data that the work can be performed in accordance with. No, you will need to test the completed build-up in the “as installed state” which would include all materials that make up the headliner panel such as the dress cover, foam, glue and substrate material that makes up the headliner. On October 17, 1997, the FAA issued Memorandum 97-112-39 “Guidance for Flammability Testing of Seat/Console Installations.” This document provide guidance as to when Heat Release and Smoke Density testing is required for aircraft seating, with capacity of 20 or more passengers. This information is for guidance only and any specific questions should be directed to your local FAA FSDO or ACO office. Your privacy is … Intermediate Scale Calorimeter (ICAL): Testing to ASTM E1623, to determine … The data tag on the seat should clarify which. This would include the cabinet structure, along with decorative finish as installed in the aircraft. Airbus has granted additional testing approvals to Skandia’s flammability laboratory. You will have to get guidance from your FSDO. Seat components that are upholstered such as armrests, shrouds, back shells, etc. It was developed for what was considered large volumes of foam. h. What if I cannot provide the substrate and the fsdo/aco won’t let me use a surrogate? As of December 2, 2011, the FAA added the requirement for Part 23 aircraft thermal/acoustic materials to meet the radiant panel test requirements. As with any test method, there will be good material that for some unknown reason has a slight after flame and does not meet the pass/fail requirements. Open Calorimeter: Calorimeter tests in compliance with federal, state or local fire codes and requirements including testing to UL 1056 and UL 1895. www.fire.tc.faa.gov/pdf/handbook/00-12_ch24new.pdf. 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. Older Part 23 aircraft are not affected by this new rule. “The accreditation does not only include our processes, but it includes the training and testing procedures for our flammability testing technicians. The specimen may be cut from any location in a fabricated part; however, fabricated units, such as sandwich panels, may not be separated for test. m. Can I get an FAA 8110-3 form for this test? Thermal/acoustic materials may have to meet additional testing requirements dependent on what they are attached to. Does existing material have to be replaced? Skandia Capabilities . The local FAA Engineering or Flight Standards District Office should be contacted regarding approval of the modified article and the basis for the approval.”, Aircraft seats are either manufactured and approved by technical standard order (TSO) or type certificate (TC) of aircraft (please check seat data tag). Skandia’s A2LA certification qualifies the company to administer 12 different flammability tests for its customers, including: • Horizontal burn test (2.5″/min burn rate) • Horizontal burn test (4.0″/min burn rate) • 12-second vertical test • 60-second vertical test • Waste containment testing • Oil burn test • 45 degree angle test Products tested include seat cushions, interior ceiling and wall panels, floor coverings, various textiles, padding, cargo covers, clear plastic windows and signs, parts … As our business continues to grow it will ensure our customer base is confident that we meet the highest levels of flammability testing standards,” Triplett said. DER’s must follow order 8110.113 when issuing an 8110-3. This test is more demanding than the 12- and 60-second verticals and measures both flame propagation and after flame time. Garrrett Ondrus Joins Skandia, Inc.… October 2019. The exposed area of the specimen must be at least 3 inches wide and 12 inches long, unless the actual size used in the airplane is smaller. Electrical wire and cable specimens must be the same size as used in the airplane. “Our flammability testing and certification services are an integral segment of Skandia’s business,” said Gary Palmer, president at Skandia. “Earning this accreditation is a major accomplishment for Skandia. 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. It is the responsibility of the upholsterer/fabricator to ensure that the work performed is compliant with the original certification. In the case of fabrics, both the warp and fill direction of the weave must be tested to determine the most critical flammability condition. b. Skandia is the global leader in providing aviation flammability engineering & testing services. Capabilities include oil burner, vertical burn, horizontal burn, 45 degree burn, 60 degree burn, and aircraft blanket fire testing. Part 25 aircraft – radiant panel testing; c. Radiant panel testing summary; d. … Except as provided in paragraph (e) of this section, the following interior compartments of airplanes with passenger capacities of 20 or more must also meet the test requirements of parts IV and V of appendix F of this part, or other approved equivalent method, in addition to the flammability requirements prescribed in paragraph (a) of this section: Interior ceiling and wall panels, other than lighting lenses and windows; Partitions, other than transparent panels needed to enhance cabin safety; Galley structure, including exposed surfaces of stowed carts and standard containers and the cavity of walls that are exposed when a full complement of such carts or containers is not carried; and. These seats are dynamically certified as an assembly which includes the detailed foam construction and dress cover. 5. Headliners, window liners, and sidewalls all have to be tested to 14 CFR 25.853(a)(i) 60-second vertical test. Skandia is an FAA-recognized flammability testing service. If you are replacing thermal/acoustic insulation, you are not required to meet this rule. “ISO 17025:2005 is specifically created for laboratories conducting testing and calibrations. Upholstery and foam build-ups cannot deviate from the original configuration without an approval process, typically controlled by the TSO holder or aircraft manufacturer. Those that won’t may require samples to be cut from the part to be tested. How do I know if a seat is dynamically certified? Specimens must be mounted in a metal frame so that the two long edges and the upper edge are held securely during the vertical test prescribed in subparagraph (4) of this paragraph and the two long edges and the edge away from the flame are held securely during the horizontal test prescribed in subparagraph (5) of this paragraph. These requirements only apply to aircraft with a capacity of 20 or more passengers. Three specimen of each are required. “The A2LA certification follows the ISO 17025:2005 standard that’s been agreed upon by regulators for setting the highest levels of testing competence within the laboratory,” he said. Skandia, Inc. tests combinations of materials to show compliance to 14 CFR 25.853(c). Contact the TSO holder or aircraft manufacturer for guidance. No, an FAA form 8110-3 can only be issued aircraft specific for U.S. registered or U.S. State of Design aircraft. Skandia Incorporated has received notice from Airbus that their Flammability Laboratory has earned additional testing approvals as an Airbus approved flammability laboratory. FAA New Policy Statement PS-ANM-25.853-01-R2 “Flammability Testing of Interior Materials”: This policy statement gives guidance on aircraft interior materials for how to qualify and what testing is required. k. What has to be tested if we are just changing the finish? 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. - 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. This testing requirement is the same as what has been previously required for Part 25 aircraft. “Many aircraft owners and operators choose to alter seating systems by incorporating such features as different upholstery. are upholstered. In addition to the flammability engineering and lab testing approval given to Skandia in 2015, Skandia now has authorization to engineer and burn aircraft cabin materials to test to heat release, smoke … f. Do armrests, base shrouds, back shells, etc. An FAA Form 8110-3 can be issued for aircraft specific for U.S. registered or U.S. State of Design aircraft when a burn test is in support of an FAA project or in support of a major repair or alteration. Skandia’s policy is not to do any similarities for different aircraft as substrate material, mix ratios and veneers can vary. Skandia DERs are authorized to generate acceptable data for Flammability only. Any Part 25 Transport category aircraft certified after 1988 is required to have passenger seats that meet TSO-C127a or be Type Certificated with seats that meet SAE 8049A and 14 CFR 25.562. Additional testing of seat components is required to show compliance when seat armrest, wraparound shrouds, base shrouds, etc. i. March 15, 2013, Davis Junction, Il. 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 Skandia has developed a procedure to show compliance to the required regulations for “dress cover only” change. e. So footrests and headrests have to meet 14 CFR 25.853(c) even if they have no foam or a very small amount? It is the modifier’s responsibility to ensure that the modified article is approved by the FAA. Flammability testing services to determine the resistance of materials to flame. You may want to contact your FAA FSDO (Flight Standards District Office) or FAA ACO (Aircraft Certification Office) for additional guidance. Headrests and leg rests are required to meet the requirements of 14 CFR 25.853(c) as called out in Advisory Circular AC 25.853-1. Three specimens are required for each test. have to be tested in the “as installed state” which includes substrate, foams, glues, dress cover material, etc. Some aircraft manufacturers include the dynamic seat approval on the aircraft Type Certificate (TC). Step 2: Testing & Fabrication Waste Containment Testing. Any changes to these articles constitutes a modification that must be approved by the FAA, regardless of whether the original article had a TSO approval or was approved as part of the aircraft type design. In the case of fabrics, both the warp and fill direction of the weave must be tested to determine the most critical flammability condition.” (This is only for Part I burns.) Skandia now has five full-time DERs on staff. If there are any other components, the assembly would have to be burned to 14 CFR 25.853 (c). Flammability Certification of Dynamic Certified Seats, 8. c. How do I perform re-upholstery and show FAA-compliance? 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 major difference between the Part 23 14 CFR 23.856 and 14 CFR 25.856(a) is that “Part 23” 23.856 only applies to newly type certificated aircraft which the type design includes Part 23 amendment 23-62. Skandia, headquartered in Davis Junction, Illinois, is a leading provider of highly engineered seating foam, foam fabrication, flammability testing … Aircraft that were built to CFR Part 25 requirements (includes commercial airliners, larger corporate aircraft, etc.). 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. There are some solutions such as using a fireblocker, but industry does not want the cost of adding fireblocker. h. What about having to meet 14 CFR 25.853 (a) and (d)? 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. Skandia’s in-house Flammability Testing is performed by highly trained technicians utilizing state-of-the-art equipment. TSO-C127a is for 16g seats and the TSO certifies the completely upholstered seat and must have 14 CFR 25.853 (c) testing to meet the TSO. Per the Advisory Circular, under certain conditions, we are given the latitude to apply the burner flame for 30 seconds or 60 seconds. A test procedure has been developed to simplify the certification process for hook and loop fasteners (Velcro). Skandia Inc. announces 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.” “The new policy statement allows the streamlining of testing for various material types,” explains Judy Johnson, FAA DAR/DER and Skandia’s flammability manager. 60-second Vertical Test. Oil Burn Test. Turn to Skandia for Expert Flammability Testing and Certification. Part 135 Aircraft do require that the seats in these aircraft meet 14 CFR 25.853 (c). Flame is applied for 15 seconds down on the sample which is under a radiant heat source. Composite panel burn testing and why it is required. This requirement does not apply to “small parts” as defined in 14 CFR 23.853 (d)(3)(v).” [Amdt 23-62, 76 FR 75759, December 2, 2011]. 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