AD 2005-05-01

The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 757 series airplanes. This AD requires identification of the part number for the cable assembly for the lower anti-collision light, and related \ninvestigative and corrective actions if necessary. This AD is prompted by a report of damage caused by an electrical arc in a connector on the cable assembly for the lower anti-collision light. We are issuing this AD to prevent an electrical arc in the cable assembly for the lower anti-collision light, which could result in a fire in a flammable leakage zone of the airplane.

Final rule.

2005-05-01 Boeing: Amendment 39-13989. Docket No. FAA-2004-19202; Directorate Identifier 2004-NM-95-AD. \n\nEffective Date \n\n\t(a) This AD becomes effective April 6, 2005. \n\nAffected ADs \n\n\t(b) None. \n\nApplicability \n\n\t(c) This AD applies to Boeing Model 757-200, -200CB, and -200PF series airplanes identified in Boeing Alert Service Bulletin 757- 33A0048, dated March 28, 2002; and Boeing Model 757-300 series airplanes identified in Boeing Alert Service Bulletin 757-33A0049, dated March 28, 2002; certificated in any category. \n\nUnsafe Condition \n\n\t(d) This AD was prompted by a report of damage caused by an electrical arc in a connector on the cable assembly for the lower anti-collision light. We are issuing this AD to prevent an electrical arc in the cable assembly for the lower anti-collision light, which could result in a fire in a flammable leakage zone of the airplane. \n\nCompliance \n\n\t(e) You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done. \n\nIdentification of Cable Assembly Part Number (P/N) \n\n\t(f) Within 60 months after the effective date of this AD: Do an inspection or a review of airplane maintenance records to identify the P/N of the cable assembly for the lower anti-collision light. If Boeing P/N S283T012-15 or Grimes P/N 60-3414-9 is identified, or if the part number of the cable assembly cannot be positively identified, do the related investigative and corrective actions required by paragraph (g) of this AD. \n\nRelated Investigative and Corrective Actions \n\n\t(g) For airplanes having Boeing P/N S283T012-15 or Grimes P/N 60-3414-9, or airplanes on which the P/N of the cable assembly cannot be positively identified: Within 60 months after the effective date of this AD, replace the cable assembly for the lower anti-collision light with a new, improved cable assembly, or modify the existing cable assembly; and do the related investigative actions; in accordance with the Accomplishment Instructions of Boeing Alert Service Bulletin 757-33A0048 (for Model 757-200, - 200CB, and -200PF series airplanes); or 757-33A0049 (for Model 757- 300 series airplanes); both dated March 28, 2002; as applicable. \n\nParts Installation \n\n\t(h) As of the effective date of this AD, no person may install a cable assembly, Boeing P/N S283T012-15 or Grimes P/N 60-3414-9, in a flammable leakage zone on any airplane. \n\nAlternative Methods of Compliance (AMOCs) \n\n\t(i) The Manager, Seattle Aircraft Certification Office, FAA, has the authority to approve AMOCs for this AD, if requested in accordance with the procedures found in 14 CFR 39.19. \n\nMaterial Incorporated by Reference \n\n\t(j) You must use the service information that is specified in Table 1 of this AD to perform the actions that are required by this AD, as applicable, unless the AD specifies otherwise. The Director of the Federal Register approves the incorporation by reference of those documents in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. For copies of the service information, contact Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124-2207. For information on the availability of this material at the National Archives and Records Administration (NARA), call (202) 741-6030, or go to http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html. \n\n\tYou may view the AD docket at the Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street SW., room PL-401, Nassif Building, Washington, DC. \n\n\tTable 1.--Material Incorporated by Reference \n\n\nBoeing alert service bulletin\nRevision level \nDate\n757-33A0048\n757-33A0049\nOriginal\nOriginal\nMarch 28, 2002.\nMarch 28, 2002.

The FAA proposed to amend 14 CFR Part 39 with an AD for certain Boeing Model 757 series airplanes. That action, published in the Federal Register on September 29, 2004 (69 FR 58107), proposed to require identification of the part number for the cable assembly for the lower anti-collision light, and related investigative and corrective actions if necessary. \n\nComments \n\n\tWe provided the public the opportunity to participate in the development of this AD. We have considered the comment that has been submitted on the proposed AD. \n\nRequest for an Additional Method of Corrective Action \n\n\tThe commenter states that potting and/or sealing the backshells of the connectors on the existing cable, to preclude liquid contamination, could provide an equivalent level of safety. We infer that the commenter is requesting that we revise the proposed AD to include potting and/or sealing the backshells of the connectors on the existing cable as an additional method forcorrecting the unsafe condition. \n\n\tWe do not agree. Due to the variety of potting material and methodologies available, we would need to review each operator's proposed potting material and methodology on a case-by-case basis. Operators may apply for an alternative method of compliance under the provisions of paragraph (i) of this AD. We have not made any changes to this AD regarding this issue. \n\nClarification of Applicability of Paragraph (g) \n\n\tWe have revised paragraph (g) of this AD to clarify that only airplanes having a cable assembly with a certain Boeing or Grimes part number, or airplanes on which the part number of the cable assembly cannot be positively identified, are required to accomplish the actions specified in paragraph (g). \n\nConclusion \n\n\tWe have carefully reviewed the available data, including the comment that has been submitted, and determined that air safety and the public interest require adopting the AD with the changes described previously. We havedetermined that these changes will neither increase the economic burden on any operator nor increase the scope of the AD. \n\nCosts of Compliance \n\n\tThis AD affects about 974 airplanes worldwide, and 650 airplanes of U.S. registry. The following table provides the estimated costs for U.S. operators to comply with this AD. \n\n\tEstimated Costs \n\n\nAction\nWork hours \nAverage labor rate per hour\nParts\nCost per airplane\nNumber of U.S. - registered airplanes\nFleet cost\nInspection/Records Review\n1\n$65\nNone\n$65\n650\n$42,250 \n\n\nAuthority for this Rulemaking \n\n\tTitle 49 of the United States Code specifies the FAA's authority to issue rules on aviation safety. Subtitle I, Section 106, describes the authority of the FAA Administrator. Subtitle VII, Aviation Programs, describes in more detail the scope of the Agency's authority. \n\n\tWe are issuing this rulemaking under the authority described in Subtitle VII, Part A, Subpart III, Section 44701, "General requirements." Underthat section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action. \n\nRegulatory Findings \n\n\tWe have determined that this AD will not have federalism implications under Executive Order 13132. This AD 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. \n\n\tFor the reasons discussed above, I certify that this AD: \n\n\t(1) Is not a "significant regulatory action" under Executive Order 12866; \n\n\t(2) Is not a "significant rule" under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); and \n\n\t(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. \n\n\tWe prepared a regulatory evaluation of the estimated costs to comply with this AD. See the ADDRESSES section for a location to examine the regulatory evaluation. \n\nList of Subjects in 14 CFR Part 39 \n\n\tAir transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. \n\nAdoption of the Amendment \n\nAccordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: \n\nPART 39--AIRWORTHINESS DIRECTIVES \n\n1. The authority citation for part 39 continues to read as follows: \n\n\tAuthority: 49 U.S.C. 106(g), 40113, 44701. \n\nSec. 39.13 (Amended) \n\n2. The FAA amends Sec. 39.13 by adding the following new airworthiness directive (AD):