Special Conditions:

Federal Register: August 4, 2010 (Volume 75, Number 149)

Rules and Regulations

Page 46840-46843

From the Federal Register Online via GPO Access [wais.access.gpo.gov]

DOCID:fr04au10-3

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration 14 CFR Part 25

Docket No. NM431; Special Conditions No. 25-409-SC

Special Conditions: Bombardier Inc. Model CL-600-2E25 Series

Airplane; Passenger Seats With Non-Traditional, Large, Non-Metallic

Panels

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final special conditions; request for comments.

SUMMARY: These special conditions are issued for the Bombardier Inc.

Model CL-600-2E25 Series Airplane. These airplanes will have a novel or unusual design feature associated with seats that include non- traditional, large, non-metallic panels that would affect survivability during a post-crash fire event. 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.

DATES: The effective date of these special conditions is July 27, 2010.

We must receive your comments by September 20, 2010.

ADDRESSES: You must mail two copies of your comments to: Federal

Aviation Administration, Transport Airplane Directorate, Attn: Rules

Docket (ANM-113), Docket No. NM431, 1601 Lind Avenue, SW., Renton,

Washington 98057-3356. You may deliver two copies to the Transport

Airplane Directorate at the above address. You must mark your comments:

Docket No. NM431. You can inspect comments in the Rules Docket weekdays, except Federal holidays, between 7:30 a.m. and 4 p.m.

FOR FURTHER INFORMATION CONTACT: Alan Sinclair, FAA, Airframe/Cabin

Safety Branch, ANM-115, Transport Airplane Directorate, Aircraft

Certification Service, 1601 Lind Avenue, SW., Renton, Washington 98057- 3356; telephone (425) 227-2195;

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facsimile (425) 227-1232; e-mail alan.sinclair@faa.gov.

SUPPLEMENTARY INFORMATION: The FAA has determined that notice of and opportunity for prior public comment on these special conditions is impracticable and would significantly delay issuance of the design approval and thus delivery of the affected aircraft. The substance of these special conditions has previously been subject to the public- comment process and received no substantive comments. The FAA therefore finds that good cause exists for making these special conditions effective upon issuance.

Comments Invited

We invite interested people to take part in this rulemaking by sending written comments, data, or views. The most helpful comments reference a specific portion of the special conditions, explain the reason for any recommended change, and include supporting data. We ask that you send us two copies of written comments.

We will file in the docket all comments we receive, as well as a report summarizing each substantive public contact with FAA personnel about these special conditions. You can inspect the docket before and after the comment closing date. If you wish to review the docket in person, go to the address in the ADDRESSES section of this preamble between 7:30 a.m. and 4 p.m., Monday through Friday, except Federal holidays.

We will consider all comments we receive by the closing date for comments. We will consider comments filed late if it is possible to do so without incurring expense or delay. We may change these special conditions based on the comments we receive.

If you want us to let you know we received your comments on these special conditions, send us a self-addressed, stamped postcard on which the docket number appears. We will stamp the date on the postcard and mail it back to you.

Background

On February 28, 2007, Bombardier Inc., 400 Cote Vertu West, Dorval,

Quebec, Canada, H4S 1Y9, applied for an amended type certificate for the Bombardier Model CL-600-2E25 airplane to be identified on Type

Certificate Data Sheet (TCDS) No. A21EA. The Model CL-600-2E25 series airplane will be a swept-wing, T-tail, twin-engine, fuselage-mounted turbofan-powered, single-aisle, medium-sized, transport-category airplane.

The applicable airplane regulations, currently approved under Title 14, Code of Federal Regulations (14 CFR) part 25, do not require seats to meet the more-stringent flammability standards required of large, non-metallic panels in the cabin interior. At the time the applicable rules were written, seats were designed with a metal frame covered by fabric, not with large, non-metallic panels. Seats also met the then- recently adopted standards for flammability of seat cushions. With the seat design being mostly fabric and metal, the contribution to a fire in the cabin had been minimized and was not considered a threat. For these reasons, seats did not need to be tested to heat-release and smoke-emission requirements.

Seat designs have now evolved to occasionally include non- traditional, large, non-metallic panels. Taken in total, the surface area of these panels is on the same order as the sidewall and overhead stowage bin interior panels. To provide the level of passenger protection intended by the airworthiness standards, these non- traditional, large, non-metallic panels in the cabin must meet the standards of part 25, Appendix F, parts IV and V, heat-release and smoke-emission requirements.

Type Certification Basis

Under provisions of 14 CFR 21.17, Bombardier must show that the

Model CL-600-2E25 series airplane meets the applicable provisions of part 25, as amended by Amendments 25-1 through 25-119. If the

Administrator finds that the applicable airworthiness regulations do not contain adequate or appropriate safety standards for the Model CL- 600-2E25 airplane because of a novel or unusual design feature, special conditions are prescribed under provisions of 14 CFR 21.16.

In addition to the applicable airworthiness regulations and special conditions, the Model CL-600-2E25 series 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. In addition, the

FAA must issue a finding of regulatory adequacy pursuant to section 611 of Public Law 92-574, the ``Noise Control Act of 1972.''

Special conditions, as defined in 14 CFR 11.19, are issued in accordance with Sec. 11.38 and become part of the type certification basis in accordance with Sec. 21.17(a)(2).

Special conditions are initially applicable to the model for which they are issued. Should the type certificate for that model be amended later to include any other model that incorporates the same or similar novel or unusual design feature, the special conditions would also apply to the other model under the provisions of Sec. 21.101.

Novel or Unusual Design Features

The Model CL-600-2E25 series airplanes will incorporate the following novel or unusual design feature: These models offer interior arrangements that include passenger seats that incorporate non- traditional, large, non-metallic panels in lieu of the traditional metal frame covered by fabric. The flammability properties of these panels have been shown to significantly affect the survivability of occupants of the cabin in the event of fire. These seats are considered a novel design for transport-category airplanes that include Amendment 25-61 and Amendment 25-66 in the certification basis, and were not considered when those airworthiness standards were established.

The existing regulations do not provide adequate or appropriate safety standards for seat designs that incorporate non-traditional, large, non-metallic panels. To provide a level of safety equivalent to that provided by the balance of the cabin, additional airworthiness standards, in the form of special conditions, are necessary. These special conditions supplement Sec. 25.853. The requirements contained in these special conditions consist of applying the identical test conditions, required of all other large panels in the cabin, to seats with non-traditional, large, non-metallic panels.

Definition of ``Non-Traditional, Large, Non-Metallic Panel''

A non-traditional, large, non-metallic panel, in this case, is defined as a panel with exposed-surface areas greater than 1.5 square feet installed per seat place. The panel may consist of either a single component or multiple components in a concentrated area. Examples of parts of the seat where these non-traditional panels are installed include, but are not limited to: seat backs, bottoms and leg/foot rests, kick panels, back shells, and credenzas and associated furniture. Examples of traditional exempted parts of the seat include: arm caps, armrest close-outs such as end bays and armrest-styled center consoles, food trays, and video monitors and shrouds.

Clarification of ``Exposed''

``Exposed'' is considered to include those panels directly exposed to the passenger cabin in the traditional sense, plus those panels enveloped such as by a dress cover. Traditional fabrics or leathers currently used on seats are excluded from these special conditions.

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These materials must still comply with Sec. 25.853(a) and Sec. 25.853(c) if used as a covering for a seat cushion, or Sec. 25.853(a) if installed elsewhere on the seat. Non-traditional, large, non- metallic panels covered with traditional fabrics or leathers will be tested without their coverings or covering attachments.

Discussion

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., Sec. 25.853 entitled ``Compartment interiors'' as amended by

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 heat release and smoke emission to seats was explored. The seat frame itself was not a concern because it was primarily made of aluminum and contained only small amounts of non- metallic materials. The FAA determined that the overall effect on survivability was negligible, whether or not the food trays met the heat-release and smoke 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 21, 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 2004, the FAA examined the appropriate flammability standards for passenger seats installed on transport-category airplanes that incorporated non-traditional, large, non-metallic panels in lieu of the traditional metal covered by fabric. The FAA 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 Sec. 25.853(d) to seats with large, non-metallic panels in their design.

Applicability

Because the heat-release and smoke-emission testing requirements of

Sec. 25.853 are part of the type certification basis for the Model CL- 600-2E25 series airplane, these special conditions are applicable to the Model CL-600-2E25 series airplane. Should Bombardier apply at a later date for a change to the type certificate to include another model incorporating the same novel or unusual design feature, the special conditions would apply to that model as well.

Seats do not have to meet these special conditions when installed in compartments that are not otherwise required to meet the test requirements of part 25, Appendix F, parts IV and V. This includes, for example, airplanes that do not have Sec. 25.853, Amendment 25-61 or later, in their certification basis and those airplanes that do not need to comply with the requirements of Sec. 121.312.

Conclusion

This action affects only certain novel or unusual design features on Bombardier Inc. Model CL-600-2E25 series airplanes. It is not a rule of general applicability.

The substance of these special conditions has been subjected to the notice and comment period in several prior instances and has been derived without substantive change from those previously issued. It is unlikely that prior public comment would result in a significant change from the substance contained herein. Therefore, the FAA has determined that prior public notice and comment are unnecessary, and good cause exists for adopting these special conditions upon issuance. The FAA is requesting comments to allow interested persons to submit views that may not have been submitted in response to the prior opportunities for comment described above.

List of Subjects in 14 CFR Part 25

Aircraft, Aviation safety, Reporting and recordkeeping requirements. 0

The authority citation for these special conditions is as follows:

Authority: 49 U.S.C. 106(g), 40113, 44701, 44702, 44704.

The 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 Bombardier Inc. Model CL-600-2E25 series airplane. 1. Except as provided in special condition number 3, below, compliance with heat-release and smoke-emission testing requirements per Sec. 25.853, and Appendix F, parts IV and V, 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 number 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 square foot; middle, 1 square foot; and inboard, 2.5 square feet). 3. Seats do not have to meet the test requirements of part 25,

Appendix F, parts IV and V, when installed in compartments that are not otherwise required to meet these requirements. Examples include:

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1. Airplanes with passenger capacities of 19 or less, b. Airplanes that do not have Sec. 25.853, Amendment 25-61 or later, in their certification basis and do not need to comply with the requirements of Sec. 121.312, and c. Airplanes exempted from Sec. 25.853, Amendment 25-61 or later. 4. Only airplanes associated with new seat-certification programs approved after the effective date of these special conditions will be affected by the requirements in these special conditions. Previously certificated interiors on the existing airplane fleet, and follow-on deliveries of airplanes with previously certificated interiors, are not affected.

Issued in Renton, Washington, on July 27, 2010.

Ali Bahrami,

Manager, Transport Airplane Directorate, Aircraft Certification

Service.

FR Doc. 2010-19072 Filed 8-3-10; 8:45 am

BILLING CODE 4910-13-P