This section of the FEDERAL REGISTER contains regulatory documents having general applicability and legal effect, most of which are keyed to and codified in the Code of Federal Regulations, which is published under 50 titles pursuant to 44 U.S.C. 1510.

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# Rules and Regulations Federal Register 

### 11679

Vol. 79, No. 41

Monday, March 3, 2014

**DEPARTMENT OF TRANSPORTATION**

**Federal Aviation Administration**

**14 CFR Part 25**

**[Docket No. FAA–2014–0078; Special Conditions No. 25–543–SC]** 

**Special Conditions: Embraer S.A., Model ERJ–170 Airplanes; Seats With**  **Large, Non-Traditional, Non-Metallic**
**Panels**

**AGENCY :**  Federal Aviation Administration (FAA), DOT.

**ACTION :**  Final special conditions; request
for comments.

**SUMMARY :**  These special conditions are issued for Embraer Model ERJ–170 airplanes. This airplane will have a novel or unusual design feature associated with interior arrangements that include passenger seats thatincorporate non-traditional, large, nonmetallic panels in lieu of the traditional metal frame covered by fabric. 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 March 3, 2014. We must receive your comments by April

17, 2014.

**ADDRESSES :**  Send comments, identified by docket number FAA–2014–0078, using any of the following methods:

• Federal eRegulations Portal: Go to http://www.regulations.gov/ and follow the online instructions for sending your comments electronically.

• Mail: Send comments to Docket Operations, M–30, U.S. Department of Transportation (DOT), 1200 New Jersey Avenue SE., Room W12–140, West Building Ground Floor, Washington, DC, 20590–0001.

• Hand Delivery or Courier: Take comments to Docket Operations in Room W12–140 of the West Building Ground Floor at 1200 New Jersey Avenue SE., Washington, DC, between 8 a.m. and 5 p.m., Monday through Friday, except federal holidays.

• Fax: Fax comments to Docket Operations at 202–493–2251.

Privacy: The FAA will post all comments it receives, without change,

to http://www.regulations.gov/, including any personal information the commenter provides. Using the search function of the docket Web site, anyone
can find and read the electronic form of all comments received into any FAA docket, including the name of the individual sending the comment (or signing the comment for an association, business, labor union, etc.). DOT’s complete Privacy Act Statement can be
found in the Federal Register published on April 11, 2000 (65 FR 19477– 19478), as well as at http:// DocketsInfo.dot.gov/

.

Docket: Background documents or comments received may be read at http://www.regulations.gov/ at any time. Follow the online instructions for accessing the docket or go to the Docket Operations in Room W12–140 of the West Building Ground Floor at 1200 New Jersey Avenue SE., Washington, DC, between 9 a.m. and 5 p.m., Monday through Friday, except federal holidays.

**FOR FURTHER INFORMATION CONTACT :**  Jayson Claar, FAA, Airframe/Cabin Safety Branch, ANM–115, Transport Airplane Directorate, Aircraft Certification Service, 1601 Lind Avenue SW., Renton, Washington, 98057–3356; telephone 425–227–2194; facsimile

425–227–1232.

**SUPPLEMENTARY INFORMATION :**  The FAA has determined that notice of, and opportunity for prior public comment on, these special conditions are impracticable because these procedures would significantly delay issuance of the design approval and thus delivery of the affected aircraft. In addition, the substance of these special conditions has been subject to the public-comment process in several prior instances with
no substantive comments received. The FAA therefore finds that good cause exists for making these special conditions effective upon publication in
the Federal Register

. 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 will consider all comments we receive on or before the closing date for comments. We may change these special
conditions based on the comments we

receive.

Background

On July 2, 2013, Embraer applied for a change to Type Certificate No. A57NMto include seats with large, nontraditional, non-metallic panels in Embraer Model ERJ–170 airplanes. TheEmbraer ERJ–170 airplanes are lowwing, conventional tail, twin turbofan, transport-category airplanes. They can seat up to 88 passengers.

The applicable regulations to airplanes currently approved under Type Certificate No. A57NM 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, their
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 tooccasionally include large, nontraditional, 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 established by the airworthiness standards, these large, non-traditional, non-metallic panels in
the cabin must meet the standards of Title 14, Code of Federal Regulations (CFR) part 25, Appendix F, parts IV and V, heat-release and smoke-emission requirements.


### 11680 Federal Register / Vol. 79, No. 41 / Monday, March 3, 2014 / Rules and Regulations

Type Certification Basis

Under the provisions of § 21.101, Embraer must show that the ERJ–170, as changed, continues to meet the applicable provisions of the regulations incorporated by reference in A57NM or the applicable regulations in effect on the date of application for the change. The regulations incorporated by reference in the type certificate are commonly referred to as the ‘‘original type-certification basis.’’ The regulations incorporated by reference in
A57NM are as follows:

14 CFR part 25, Amdts. 25–1 through 25–101 in entirety. In addition, the
certification basis includes certain special conditions, exemptions, or later amended sections of the applicable part that are not relevant to these special
conditions.

If the Administrator finds that the applicable airworthiness regulations (e.g., 14 CFR part 25) do not contain adequate or appropriate safety standards for Embraer Model ERJ–170 airplanes because of a novel or unusual design feature, special conditions are prescribed under the provisions of § 21.16.

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 novel or unusual design feature, or should any other model already included on the same type certificate be modified to incorporate the same novel or unusual design feature, the special conditions would also apply to the other model.

In addition to the applicable airworthiness regulations and special conditions, ERJ–170 airplanes mustcomply with the fuel-vent and exhaustemission requirements of 14 CFR part 34, and the noise-certification requirements of 14 CFR part 36.

The FAA issues special conditions, as defined in 14 CFR 11.19, in accordance with § 11.38, and they become part of the type-certification basis under § 21.101.

Novel or Unusual Design Features

The ERJ–170 will incorporate the following novel or unusual design
features:

These models offer interior arrangements that include passengerseats that incorporate large, nontraditional, 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 cabin occupants 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 thatincorporate large, non-traditional, nonmetallic panels in their designs. To provide a level of safety that is equivalent to that afforded to the balance of the cabin, additional airworthiness standards, in the form of special conditions, are necessary. These special conditions supplement § 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, toseats with large, non-traditional, nonmetallic panels.

Discussion

In the early 1980s, the Federal Aviation Administration (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 interiorsurfaces associated with larger surfacearea 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 to post-crash fire-survival time. The materials that comply with the standards (e.g., § 25.853, ‘‘Compartment Interiors,’’ as amended by Amendments 25–61 and 25–66) were found to extend survival time by approximately two minutes over materials that do not comply.

At the time Amendment 25–61 was written, the potential application of the requirement to seats was explored. The
seat frame itself was not a concern because it was primarily made of aluminum and incorporated only small amounts of non-metallic materials (for example, a food-tray table and armrest closeout). The FAA determined that the overall effect on survivability was negligible, whether or not these panels
met the heat-release and smokeemission requirements. The requirements therefore did not address seats, and the preambles to both Notice of Proposed Rule Making (NPRM) 85–10 and the final rule (Amendment 25–61) specifically note that they were excluded ‘‘. . . because the recently adopted standards for flammability of seat cushions will greatly inhibit involvement of the seats’’ in their postcrash fire.

In the late 1990s, when it became clear that seat designs were evolving to include large non-metallic panels with surface area that would impact survivability during a cabin-fire event compared to partitions or galleys, the FAA issued Policy Memorandum 97– 112–39. This 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 would have been an exception to the airworthiness standards, which could result in an unacceptable decrease in survivability during a cabin-fire event.

Definition of ‘‘Large, Non-Traditional,
Non-Metallic Panel’’

A large, non-traditional panel, in thiscase, is defined as a panel with exposedsurface 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 non-traditional areas include, but are not limited to, seat backs, bottoms and leg/foot rests, kick panels, back shells, and associated furniture. Examples of traditional, exempted areas include, but are not limited to, arm caps, armrest close-outs, and items such as end-bays and center consoles, food trays, 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 the special conditions. These materials must still comply with § 25.853(a) and (c) if used as a covering for a seat cushion, or § 25.853(a) if installed elsewhere on the seat. Large, non-metallic panels covered with
traditional fabrics or leathers will be tested without their coverings or covering attachments.

Applicability

As discussed above, these special conditions are applicable to Embraer Model ERJ–170 airplanes. Should Embraer 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.


### 11681 Federal Register / Vol. 79, No. 41 / Monday, March 3, 2014 / Rules and Regulations

Conclusion

This action affects only certain novel or unusual design features on one model of airplane. 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, because a delay would significantly affect the certification of the airplane, the FAA has determined that prior public notice and comment are unnecessary and impracticable, and good cause exists for adopting these special conditions upon publication in the Federal Register. 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.

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 specialconditions are issued as part of the typecertification basis for Embraer Model ERJ–170 airplanes:

1. Compliance with part 25, Appendix F, parts IV and V, heat release and smoke emission, is required for seats that incorporate large, non-traditional, non-metallic panels that may either be a single component or multiple components in a concentrated area in their design.

2. The applicant may designate up toand including 1.5 square feet of nontraditional, non-metallic panel material per seat place that does not have to comply with No. 1. 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 Title 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:

a. Airplanes with passenger capacities
of 19 or fewer. b. Airplanes that do not have smoke
emission and heat release in their
certification basis and do not need to comply with the requirements of § 121.312.

c. Airplanes exempted from heatrelease and smoke-emission requirements.

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 February

21, 2014. John P. Piccola, Jr., Acting Manager, Transport Airplane Directorate, Aircraft Certification Service.

[FR Doc. 2014–04559 Filed 2–28–14; 8:45 am]

**BILLING CODE 4910–13–P**

**DEPARTMENT OF TRANSPORTATION**

**Federal Aviation Administration**

**14 CFR Part 39**

**[Docket No. FAA–2011–0562; Directorate Identifier 2011–CE–015–AD; Amendment**  **39–17740; AD 2014–03–03]**

**RIN 2120–AA64**

**Airworthiness Directives; Cessna Aircraft Company Airplanes** 

**AGENCY :**  Federal Aviation Administration (FAA), DOT.

**ACTION :**  Final rule.

**SUMMARY :**  We are adopting a new airworthiness directive (AD) for certain Cessna Aircraft Company (Cessna) Models 310, 320, 340, 401, 402, 411, 414, and 421 airplanes. This AD was prompted by an investigation of recent and historical icing-related accidents and incidents for the products listed above. This AD requires either having the supplemental airplane flight manual/airplane flight manual supplement (SAFM/AFMS) inside the airplane and accessible to the pilot during the airplane’s operation or installing a placard that prohibits flight into known icing conditions and installing a placard that increases published airspeed on approach at least 17 mph (15 knots) in case of an inadvertent encounter with icing. We are issuing this AD to correct the unsafe condition on these products.

**DATES :**  This AD is effective April 7,

2014. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in the AD as of April 7, 2014.

**ADDRESSES :**  For service information identified in this AD, contact Cessna Aircraft Company, Product Support, P.O. Box 7706, Wichita, KS 67277; telephone: (316) 517–5800; fax: (316) 517–7271; email: customercare@

cessna.textron.com ; Internet: http:// www.cessna.com/. You may review copies of the referenced service information at the FAA, Small Airplane Directorate, 901 Locust, Kansas City, MO 64106. For information on the availability of this material at the FAA, call (816) 329–4148.

Examining the AD Docket

You may examine the AD docket on
the Internet at http://www. regulations.gov by searching for and locating Docket No. FAA–2011–0562; or in person at the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this AD, the regulatory evaluation, any comments received, and other
information. The address for the Docket Office (phone: 800–647–5527) is Document Management Facility, U.S. Department of Transportation, Docket Operations, M–30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue SE., Washington,

DC 20590.

**FOR FURTHER INFORMATION CONTACT :**  Dan Withers, Program Manager, FAA, Wichita Aircraft Certification Office, 1801 S. Airport Road, Room 100, Wichita, Kansas 67209; telephone: (316) 946–4137; fax: (316) 946–4107; email: dan.withers@faa.gov

. **SUPPLEMENTARY INFORMATION :** 

Discussion

We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to include an AD that would apply to certain Cessna Aircraft Company (Cessna) Models 310, 320, 340, 401, 402, 411, 414, and 421 airplanes. The NPRM published in the Federal Register on June 3, 2011 (76 FR 32103). The NPRM proposed to require you to install a placard that prohibits flight into known icing conditions and install a placard that increases published airspeed on approach at least 17 mph (15 knots) in case of an inadvertent encounter with icing. We are issuing this AD to prohibit flight into known icing conditions as well as increase the approach speed in case of an inadvertent encounter with icing. This condition, if not corrected, could