AD 2004-13-19

This amendment adopts a new airworthiness directive (AD), applicable to certain Airbus Model A300 B2 and A300 B4; Model A300 B4- 600, B4-600R, C4-605R Variant F, and F4-600R (collectively called A300- 600); and Model A310 series airplanes. This AD requires an inspection to determine the part number of certain passenger/crew escape slides; and related investigative action and corrective action, if necessary. This action is necessary to prevent the failure of an escape slide to deploy during emergency evacuation, which could impede an evacuation and result in injury to flightcrew and passengers. This action is intended to address the identified unsafe condition.

Final rule.

2004-13-19 Airbus: Amendment 39-13701. Docket 2003-NM-274-AD.

Applicability: Model A300 B2 and A300 B4; Model A300 B4-600, B4- 600R, C4-605R Variant F, and F4-600R (collectively called A300-600); and Model A310 series airplanes; equipped with Goodrich escape slides; certificated in any category.

Compliance: Required as indicated, unless accomplished previously.

To prevent the failure of an escape slide to deploy during emergency evacuation, which could impede an evacuation and result in injury to flightcrew and passengers, accomplish the following:

Service Bulletin Reference

(a) The term "service bulletin," as used in this AD, means the Accomplishment Instructions of the following service bulletins, as applicable:

(1) For Model A300 B2 and A300 B4 series airplanes: Airbus Service Bulletin A300-25A0475, dated October 3, 2003;

(2) For Model A300 B4-600, B4-600R, C4-605R Variant F, and F4- 600R (collectively called A300-600) series airplanes: Airbus Service Bulletin A300-25A6184, dated October 3, 2003; and

(3) For Model A310 series airplanes: Airbus Service Bulletin A310-25A2165, dated October 3, 2003.

Note 1: These service bulletins reference Goodrich Alert Service Bulletin 7A1296/7A1298-25A345, dated October 15, 2003, as an additional source of service information for accomplishment of the inspection and modification.

Inspections and Corrective Action

(b) Within 180 days after the effective date of this AD: Do an inspection to determine the part number (P/N) of the passenger/crew door escape slides. If any Goodrich P/N 7A1298-001, 7A1298-002, 7A1296-001, or 7A1296-002 is found during the inspection, prior to further flight, do the related investigative action, any applicable corrective action, and replace the slide with a new or modified slide which has a girt with the correct P/N. Do all actions per the applicable service bulletin.

Parts Installation

(c) As of the effective date of this AD, no person may install on any airplane a Goodrich escape slide having P/N 7A1298-001, 7A1298-002, 7A1296-001, or 7A1296-002, unless the related investigative action and any applicable corrective action has been done per paragraph (b) of this AD.

Alternative Methods of Compliance

(d) In accordance with 14 CFR 39.19, the Manager, International Branch, ANM-116, FAA, Transport Airplane Directorate, is authorized to approve alternative methods of compliance for this AD.

Incorporation by Reference

(e) The actions shall be done in accordance with Airbus Service Bulletin A300-25A0475, dated October 3, 2003; Airbus Service Bulletin A300-25A6184, dated October 3, 2003; or Airbus Service Bulletin A310-25A2165, dated October 3, 2003; as applicable. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from Airbus, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France. Copies may beinspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call (202) 741-6030, or go to: http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html .

Note 2: The subject of this AD is addressed in French airworthiness directive F-2003-435, dated December 10, 2003.

Effective Date

(f) This amendment becomes effective on August 5, 2004.

A proposal to amend part 39 of the Federal Aviation Regulations (14 CFR part 39) to include an airworthiness directive (AD) that is applicable to certain Airbus Model A300 B2 and A300 B4; Model A300 B4-600, B4-600R, C4-605R Variant F, and F4-600R (collectively called A300-600); and Model A310 series airplanes was published in the Federal Register on May 3, 2004 (69 FR 24099). That action proposed to require an inspection to determine the part number of certain passenger/crew escape slides; and related investigative action and corrective action, if necessary.

Comments

Interested persons have been afforded an opportunity to participate in the making of this amendment. No comments were submitted in response to the proposal or the FAA's determination of the cost to the public.

Conclusion

We have determined that air safety and the public interest require the adoption of the rule as proposed.

Cost Impact

We estimate that 202 airplanes ofU.S. registry will be affected by this AD, that it will take approximately 3 work hours per airplane to accomplish the required actions, and that the average labor rate is $65 per work hour. Based on these figures, the cost impact of the AD on U.S. operators is estimated to be $195 per slide.

The cost impact figure discussed above is based on assumptions that no operator has yet accomplished any of the requirements of this AD action, and that no operator would accomplish those actions in the future if this AD were not adopted. The cost impact figures discussed in AD rulemaking actions represent only the time necessary to perform the specific actions actually required by the AD. These figures typically do not include incidental costs, such as the time required to gain access and close up, planning time, or time necessitated by other administrative actions.

Regulatory Impact

The regulations adopted herein will not have a substantial direct effect on the States, on the relationship between the national Government and the States, or on the distribution of power and responsibilities among the various levels of government. Therefore, it is determined that this final rule does not have federalism implications under Executive Order 13132.

For the reasons discussed above, I certify that this action (1) is not a "significant regulatory action" under Executive Order 12866; (2) is not a "significant rule" under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); and (3) will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act. A final evaluation has been prepared for this action and it is contained in the Rules Docket. A copy of it may be obtained from the Rules Docket at the location provided under the caption ADDRESSES.

List of Subjects in 14 CFR Part 39

Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety.

Adoption of the Amendment

Accordingly, pursuant to the authority delegated to me by the Administrator, the Federal Aviation Administration amends part 39 of the Federal Aviation Regulations (14 CFR part 39) as follows:

PART 39--AIRWORTHINESS DIRECTIVES

1. The authority citation for part 39 continues to read as follows:

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

39.13 [Amended]

2. Section 39.13 is amended by adding the following new airworthiness directive: