2007-02-19: Bruce floor plan electrical emergency path marking system (FPEEPMS)

2007-02-19 Airbus: Amendment 39-14906. Docket No. FAA-2006-26047; Directorate Identifier 2006-NM-146-AD. Effective Date (a) This AD becomes effective March 5, 2007. Affected ADs (b) None. Applicability (c) This AD applies to Airbus Model A300 B4-605R airplanes and Model A310-308, -324, and -325 airplanes, certificated in any category; on which Airbus Modification 06810 or 06934 (Bruce floor proximity emergency escape path marking system (FPEEPMS)) has been installed in production; or on which Airbus Service Bulletin A300- 33-6047 or A310-33-2045, both dated March 5, 2004, has been done. Unsafe Condition (d) This AD results from a report that in the case of vertical separation of the fuselage forward of door 1, the FPEEPMS and the exit signs do not turn on. We are issuing this AD to prevent inadequate lighting and marking of the escape path, which could delay or impede the flightcrew and passengers when exiting the airplane during an emergency landing. Compliance (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. Modification (f) Within 16 months after the effective date of this AD, modify the Bruce FPEEPMS in accordance with the Accomplishment Instructions of Airbus Service Bulletin A300-33-6047, Revision 01, dated January 20, 2006 (for Model A300 B4-605R airplanes); or Airbus Service Bulletin A310-33-2045, Revision 01, dated January 20, 2006 (for Model A310-308, -324, and -325 airplanes); as applicable. (g) For Model A310-308, -324, and -325 airplanes: Prior to or concurrently with the modification required in paragraph (f) of this AD, modify the automatic switching of the emergency lighting system in accordance with the Accomplishment Instructions of Airbus Service Bulletin A310-33-2025, Revision 01, dated April 17, 2001. Modifications Accomplished According to Previous Issue of Service Bulletin (h) Modifications accomplished before the effective date of this AD in accordance with Airbus Service Bulletin A310-33-2025, dated March 1, 1993, are considered acceptable for compliance with the corresponding action specified in paragraph (g) of this AD. Alternative Methods of Compliance (AMOCs) (i)(1) The Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA, has the authority to approve AMOCs for this AD, if requested in accordance with the procedures found in 14 CFR 39.19. (2) Before using any AMOC approved in accordance with Sec. 39.19 on any airplane to which the AMOC applies, notify the appropriate principal inspector in the FAA Flight Standards Certificate Holding District Office. Related Information (j) EASA airworthiness directive 2006-0077, dated April 3, 2006, also addresses the subject of this AD. Material Incorporated by Reference (k) You must use the applicable service bulletin identified in Table 1 of this ADto perform the actions that are required by this AD, unless the AD specifies otherwise. The Director of the Federal Register approved the incorporation by reference of these documents in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Contact Airbus, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France, for a copy of this service information. You may review copies at the Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street, SW., Room PL-401, Nassif Building, Washington, DC; on the Internet at http://dms.dot.gov; or at the National Archives and Records Administration (NARA). For information on the availability of this material at the NARA, call (202) 741-6030, or go to http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html . Table 1.--Material Incorporated by Reference Airbus Service Bulletin Revision Level Date A300-33-6047 01 January 20, 2006 A310-33-2025 01 April 17, 2001 A310-33-2045 01 January 20, 2006