Airworthiness standards: Special conditions— Airbus Model A320 airplanes,

[Federal Register: October 8, 2003 (Volume 68, Number 195)]

[Proposed Rules]

[Page 58042-58043]

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

[DOCID:fr08oc03-14]

Proposed Rules Federal Register

This section of the FEDERAL REGISTER contains notices to the public of the proposed issuance of rules and regulations. The purpose of these notices is to give interested persons an opportunity to participate in the rule making prior to the adoption of the final rules.

[[Page 58042]]

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 25

[Docket No. NM266; Notice No. 25-03-07-SC]

Special Conditions: Airbus Model A320 Airplanes; Child Restraint System

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed special conditions.

SUMMARY: This notice proposes special conditions for Airbus Model A320 airplanes. These airplanes, as modified by AMSAFE Inc., will have novel and unusual design features associated with a child restraint system that attaches to the existing passenger lap belt. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These proposed 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: Comments must be received on or before November 7, 2003.

ADDRESSES: Comments on these proposed special conditions may be mailed in duplicate to: Federal Aviation Administration, Transport Airplane Directorate, Attn: Rules Docket (ANM-113), Docket No. NM266, 1601 Lind Avenue SW., Renton, Washington 98055-4056; or delivered in duplicate to the Transport Airplane Directorate at the above address. Comments must be marked: Docket No. NM266. Comments may be inspected 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 and Cabin Safety Branch, ANM-115, Transport Airplane Directorate, Aircraft Certification Service, 1601 Lind Avenue SW., Renton, Washington, 98055- 4056; telephone (425) 227-2195; facsimile (425) 227-1149, e-mail alan.sinclair@faa.gov.

SUPPLEMENTARY INFORMATION:

Comments Invited

The FAA invites interested persons to participate in this rulemaking by submitting 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 concerning these special conditions. The docket is available for public inspection 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 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays.

We will consider all comments we receive on or before 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 the FAA to acknowledge receipt of your comments on these proposed special conditions, include with your comments a pre- 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 12, 2003, AMSAFE Inc., P.O. Box 1570, Higley, Arizona 85236, applied for a supplemental type certificate for the modification of Airbus Model A320 airplanes. The modification includes a child restraint system that attaches to the existing passenger lap belt and can be installed on certain seats of Airbus Model A320 airplanes in order to reduce the potential for injury in the event of an accident. The Model A320 is a swept-wing, conventional tail, twin-engine, turbofan-powered transport airplane.

Type Certification Basis

Under the provisions of Sec. 21.101, AMSAFE Inc. must show that the Airbus Model A320 airplanes, as changed, continue to meet the applicable provisions of the regulations incorporated by reference in Type Certificate No. A28NM, 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 Type Certificate No. A28NM are as follows: 14 CFR part 25, effective February 1, 1965, including Amendments 25-1 through 25-56; SFAR 27, effective February 1, 1974, including Amendments 27-1 through 27-5; and 14 CFR part 36 effective December 1, 1969, including Amendments 36-1 through 36-12. In addition, the certification basis includes other regulations and special conditions that are not pertinent to these special conditions.

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 Airbus Model A320 airplanes because of a novel or unusual design feature, special conditions are prescribed under the provisions of Sec. 21.16.

In addition to the applicable airworthiness regulations and special conditions, the Airbus Model A320 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.

Special conditions, as defined in Sec. 11.19, are issued in accordance with Sec. 11.38 and become part of the type certification basis in accordance with Sec. 21.101.

Special conditions are initially applicable to the model for which they are issued. Should AMSAFE Inc. apply for a supplemental type certificate to modify any other model included on the same type certificate to incorporate 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 AMSAFE Inc. Child Safety System (CSS) is an improved harness type Child Restraint System (CRS) that utilizes the seat back and the lap belt on

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passenger seats to provide upper torso restraint and improve the restraint of small children. The physical characteristics of small children will govern the use of the CSS and must be defined according to accepted classification standards. The device is intended for children in the 2- to 4-year age group who are prohibited from being held in their parents' arms during taxi, take-off, and landing and must occupy their own passenger seat, typically with no supplemental restraint. The CSS is made with webbing and fastening hardware and consists of an adjustable strap that wraps horizontally around the seat back to secure the device to the passenger seat, and a double shoulder harness that is fastened around the child's upper torso. The ends of the device's shoulder harness are held in place using the existing passenger lap belt that is passed through two open loops on the lower ends of the device's shoulder straps. The current part 25 airworthiness regulations are not adequate to define the necessary certification criteria.

Discussion

The CSS is a non-conforming CRS (that is, not approved for use on aircraft per Federal Motor Vehicle Safety Standard (FMVSS) 213 and as such the design requirements are established in these special conditions. It is a safety restraint device specifically designed for use by small children on JetBlue Airways Airbus A320 aircraft.

The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this particular design feature. Additional safety standards are therefore necessary to establish a level of safety equivalent to that established by the existing airworthiness standards for transport category airplanes.

Additionally, the operating regulations, 14 CFR 91.107 and 121.311, prohibit the use of any ``vest-type child restraints, and harness-type child restraints'' for commercial and private use operations. In order for the CSS, which is a harness-type child restraint, to be useable in the U.S., AMSAFE Inc., or their agent, must petition the FAA for an exemption from the operating regulations. The petition must be granted in order to allow use of the CSS.

The following special conditions can be characterized as addressing the safety performance of the system and the capability of the system to be installed and utilized without creating additional safety concerns. Because of the nature of the system and the direct interface with the crew and passengers, as well as the intended occupants, these special conditions are more rigorous from a design standpoint than for the standard lapbelt installation.

Applicability

As discussed above, these special conditions are applicable to the Airbus Model A320 airplanes modified by AMSAFE Inc. Should AMSAFE Inc. apply at a later date for a supplemental type certificate to modify any other model included on Type Certificate No. A28NM to incorporate the same or similar novel or unusual design feature, these special conditions would apply to that model as well under the provisions of Sec. 21.101.

Conclusion

This action affects only certain novel or unusual design features on Airbus Model A320 airplanes. It is not a rule of general applicability, and it affects only the applicant who applied to the FAA for approval of these features on the airplane.

List of Subjects in 14 CFR Part 25

Aircraft, Aviation safety, Reporting and recordkeeping requirements.

Authority Citation

The authority citation for these special conditions is as follows:

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

The Proposed Special Conditions

Accordingly, the Federal Aviation Administration (FAA) proposes the following special conditions as part of the type certification basis for Airbus Model A320 airplanes modified by AMSAFE Inc.

1. The child restraint system (CSS) must provide child restraint protection under dynamic emergency landing conditions to prevent serious head and other injuries. It must protect a range of occupant statures for which the system is designed in accordance with Sections 2.3 and 2.4 of the Society of Automotive Engineers (SAE) document AS5276/1. The CSS must provide a consistent approach to energy absorption throughout that range.

2. Means must be provided to prevent the use of the CSS with children who are outside the range of statures for which the system was designed and tested. The range of statures for which the CSS is approved must be clearly labeled on the device.

3. There must be obvious, clear, and concise instructions readily available to the flight and cabin crew as to the proper installation and use of the CSS system for children.

4. The design of the CSS must prevent it from being incorrectly buckled and/or incorrectly installed such that the CSS would not properly perform its intended function.

5. The CSS must meet the minimum performance standards of Appendix 1 and the test conditions of Appendix 2 of Technical Standard Order C100b.

6. The CSS must not impede rapid egress of the occupant using the CSS and the occupants seated in the same row.

7. Means must be provided to prohibit the installation and use of the CSS in the emergency exit rows.

8. The CSS must be shown to operate safely in the following locations, or means must be provided to prohibit the installation and use of the CSS at these seat locations:

   1. Behind any wall or seat back that has an inflatable airbag.

   2. Any passenger seat that has an inflatable restraint system.

   3. Side-facing seats.

9. It must be shown that the CSS will not cause the occupant's passenger seat back to fold over during a crash situation and cause injury to the occupant.

10. It must be shown that tray tables, phones or other devices installed in the seat back will not degrade the performance of the CSS.

11. Passenger seats approved for installation of the CSS must be clearly identified to the installer by location and part number.

12. The operating regulations, 14 CFR 91.107 and 14 CFR 121.311, prohibit the use of any ``vest-type child restraints, and harness-type child restraints'' in commercial and private use operations. It is therefore incumbent upon AMSAFE Inc., or their agent, to petition the FAA for exemption from these two regulations. The exemption must be granted in order for the system to be used by a U.S. operator.

    Issued in Renton, Washington, on September 25, 2003. Ali Bahrami, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service.

    [FR Doc. 03-25423 Filed 10-7-03; 8:45 am]

    BILLING CODE 4910-13-P