Source: https://www.federalregister.gov/documents/2016/07/29/2016-17846/special-conditions-atr-model-atr-42-200-300-320-500-and-atr-72-102-202-212-212a-airplanes-seats-with
Timestamp: 2018-04-24 17:03:57
Document Index: 61440419

Matched Legal Cases: ['art 25', '§\u200921', 'art 34', 'art 36', 'art 25', '§\u200925', 'art 25', 'art 25']

Federal Register :: Special Conditions: ATR Model ATR-42-200/-300/-320/-500 and ATR-72-102/-202/-212/-212A Airplanes; Seats With Non-Traditional, Large, Non-Metallic Panels
This action is effective on ATR on July 29, 2016. We must receive your comments by September 12, 2016.
81 FR 49871
49871-49873 (3 pages)
Docket No. FAA-2016-8246
Special Conditions No. 25-624-SC
2016-17846
FAA-2016-8246
https://www.federalregister.gov/d/2016-17846 https://www.federalregister.gov/d/2016-17846
These special conditions are issued for ATR Model ATR-42-200/-300/-320/-500 and ATR-72-102/-202/-212/-212A airplanes. These airplanes will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport-category airplanes. This design feature is seats with non-traditional, large, non-metallic panels. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
Start Printed Page 49872
Send comments identified by docket number FAA-2016-8246 using any of the following methods:
The FAA has determined that notice of, and opportunity for prior public comment on, these special conditions is impracticable because these procedures would significantly delay issuance of the design approval, and thus delivery, of the affected airplanes.
On March 2, 2016, ATR applied for a change to type certificate no. A53EU for the installation of seats constructed of non-traditional, non-metallic materials in the Model ATR-42-200/-300/-320/-500, and ATR-72-102/-202/-212/-212A airplanes.
The Model ATR-42/-72 series airplanes are twin-engine, turbopropeller-powered, transport-category airplanes with maximum passenger capacity up to 74, depending upon airplane model.
Under the provisions of Title 14, Code of Federal Regulations (14 CFR) 21.101, ATR must show that the Model ATR-42-200/-300/-320/-500 and ATR-72-102/-202/-212/-212A airplanes, as changed, continue to meet the applicable provisions of the regulations listed in type certificate no. A53EU, or the applicable regulations in effect on the date of application for the change, except for earlier amendments as agreed upon by the FAA.
If the Administrator finds that the applicable airworthiness regulations (i.e., 14 CFR part 25) do not contain adequate or appropriate safety standards for the Model ATR-42-200/-300/-320/-500 and ATR-72-102/-202/-212/-212A airplanes because of a novel or unusual design feature, special conditions are prescribed under the provisions of § 21.16.
In addition to the applicable airworthiness regulations and special conditions, the Model ATR-42-200/-300/-320/-500 and ATR-72-102/-202/-212/-212A airplanes must comply with the fuel-vent and exhaust-emission requirements of 14 CFR part 34, and the noise-certification requirements of 14 CFR part 36.
The Model ATR-42-200/-300/-320/-500 and ATR-72-102/-202/-212/-212A airplanes will incorporate the following novel or unusual design feature:
Passenger seats that incorporate non-traditional, large, non-metallic panels in lieu of the traditional metal frame covered by fabric.
In the early 1980s, the FAA conducted extensive research on the effects of post-crash flammability in the passenger cabin. As a result of this research and service experience, the FAA adopted new standards for interior surfaces associated with large surface-area parts. Specifically, the rules require measurement of heat release and smoke emission (part 25, Appendix F, parts IV and V) for the affected parts. Heat release has been shown to have a direct correlation with post- crash-fire survival time. Materials that comply with the standards (i.e., § 25.853, “Compartment interiors” at Amendment 25-61 and Amendment 25-66) extend survival time by approximately 2 minutes over materials that do not comply.
At the time these standards were written, the potential application of the requirements of seat heat release and smoke emission was explored. The seat frame itself was not a concern because it was primarily made of aluminum and only small amounts of non-metallic materials. Research determined that the overall effect on survivability was negligible, whether or not the food trays met the heat-release and smoke-emission requirements. The requirements therefore did not address seats. The preambles to both the Notice of Proposed Rule Making (NPRM), Notice No. 85-10 (50 FR 15038, April 16, 1985), and the Final Rule at Amendment 25-61 (51 FR 26206, July Start Printed Page 4987321, 1986), specifically note that seats were excluded “because the recently adopted standards for flammability of seat cushions will greatly inhibit involvement of the seats.”
Subsequently, the Final Rule at Amendment 25-83 (60 FR 6615, March 6, 1995) clarified the definition of minimum panel size: “It is not possible to cite a specific size that will apply in all installations; however, as a general rule, components with exposed surface areas of one square foot or less may be considered small enough that they do not have to meet the new standards. Components with exposed surface areas greater than two square feet may be considered large enough that they do have to meet the new standards. Those with exposed surface areas greater than one square foot, but less than two square feet, must be considered in conjunction with the areas of the cabin in which they are installed before a determination could be made.”
In the late 1990s, the FAA issued Policy Memorandum 97-112-39, “Guidance for Flammability Testing of Seat/Console Installations,” October 17, 1997 (http://rgl.faa.gov). That memo was issued when it became clear that seat designs were evolving to include large, non-metallic panels with surface areas that would impact survivability during a cabin-fire event, comparable to partitions or galleys. The memo noted that large-surface-area panels must comply with heat-release and smoke-emission requirements, even if they were attached to a seat. If the FAA had not issued such policy, seat designs could have been viewed as a loophole to the airworthiness standards that would result in an unacceptable decrease in survivability during a cabin-fire event.
In October of 2004, an issue was raised regarding the appropriate flammability standards for passenger seats that incorporated non-traditional, large, non-metallic panels in lieu of the traditional metal covered by fabric. The FAA Seattle Aircraft Certification Office and Transport Standards Staff reviewed this design, and determined that it represented the kind and quantity of material that should be required to pass the heat-release and smoke-emissions requirements. The FAA has determined that special conditions would be issued to apply the standards defined in 14 CFR 25.853(d) to seats with large, non-metallic panels in their design. Traditional seat panels would not be covered by the special conditions.
As discussed above, these special conditions are applicable to the Model ATR-42-200/-300/-320/-500 and ATR-72-102/-202/-212/-212A airplanes. Should ATR apply at a later date for a change to the type certificate to include another model incorporating the same novel or unusual design feature, these special conditions would apply to that model as well. These special conditions apply to new seat-certification programs. Previously approved seats are not affected by these special conditions.
Accordingly, pursuant to the authority delegated to me by the Administrator, the following special conditions are issued as part of the type certification basis for ATR Model ATR-42-200/-300/-320/-500 and ATR-72-102/-202/-212/-212A airplanes for new seat-certification programs.
1. Compliance with 14 CFR part 25 Appendix F, parts IV and V, “Heat release and smoke emission,” is required for seats that incorporate non-traditional, large, non-metallic panels that may be either a single component or multiple components in a concentrated area in their design.
2. The applicant may designate up to and including 1.5 square feet of non-traditional, non-metallic panel material per seat place that does not have to comply with special condition 1, above. A triple seat assembly may have a total of 4.5 square feet excluded on any portion of the assembly (e.g., outboard seat place, 1 sq. ft.; middle, 1 sq. ft.; and inboard, 2.5 sq. ft.)
3. Seats need not meet the test requirements of 14 CFR part 25 Appendix F, parts IV and V, when installed in compartments that are not otherwise required to meet these requirements. Examples include airplanes:
a. With passenger capacities of 19 or fewer;
b. that do not have smoke-emission and heat-release test requirements in their certification basis, and that are not required by 14 CFR 121.312 to conduct such tests; or
c. that are exempted from smoke-emission and heat-release testing.
[FR Doc. 2016-17846 Filed 7-28-16; 8:45 am]