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Bulletin A300-57-0244, dated March 4, 2005 (for Model A300 airplanes); A300-57-6099, dated
February 23, 2005 (for Model A300-600 series airplanes); or A310-57-2086, dated March 1, 2005
(for Model A310 airplanes); as applicable.
2007-03-09 2
7 BW 2007-04
Revisions
(c) For all airplanes: Within 3 months after the effective date of this AD: Incorporate the
information in the applicable aircraft maintenance manual (AMM) specified in paragraphs (c)(1),
(c)(2), and (c)(3) of this AD,into the FAA-approved maintenance program to specify an inspection
for breaks of the bottom flange of the RAT swivel coupling yoke fitting after each RAT retraction;
and replacement of the RAT swivel coupling yoke fitting with a new aluminum or steel part as
applicable; in accordance with a method approved by the Manager, International Branch, ANM-116,
Transport Airplane Directorate, FAA; or the Direction Générale de l'Aviation Civile (or its delegated
agent); or European Aviation Safety Agency (or its delegated agent). The page blocks specified in
paragraphs (c)(1), (c)(2), and (c)(3) of this AD, as applicable, are one approved method for the
actions required by paragraph (c) of this AD. Thereafter, except as provided by paragraph (d) of this
AD, no alternative inspection intervals may be approved for the bottom flange of the RAT swivel
coupling yoke fitting.
(1) Airbus A300-600 AMM, Chapter 29-25-00, Page Block 301, dated June 1, 2005.
(2) Airbus A310 AMM, Chapter 29-25-00, Page Block 301, dated June 1, 2005.
(3) Airbus A300 AMM Chapter 29-25-00, Page Block 301, dated March 1, 2006.
Note 2: After revising the maintenance program to include the required periodic inspections
according to this paragraph, operators do not need to make a maintenance log entry to show
compliance with this AD every time those inspections are accomplished thereafter.
Note 3: This AD requires revisions to certain operator maintenance documents to include new
inspections. Compliance with these inspections is required by 14 CFR 91.403(c). For airplanes that
have been previously modified, altered, or repaired in the areas addressed by these inspections, the
operator may not be able to accomplish the inspections described in the revisions. In this situation, to
comply with 14 CFR 91.403(c), the operator must request approval for an alternative method of
compliance according to paragraph (d) of this AD. The request should include a description of
changes to the required inspections that will ensure the continued damage tolerance of the affected
structure. The FAA has provided guidance for this determination in
Advisory Circular (AC) 25-1529-1.
Alternative Methods of Compliance
(d)(1) In accordance with 14 CFR 39.19, the Manager, International Branch, ANM-116, is
authorized to approve alternative methods of compliance for this AD.
(2) Before using any AMOC approved in accordance with § 39.19 on any airplane to which the
AMOC applies, notify the appropriate principal inspector in the FAA Flight Standards Certificate
Holding District Office.
Note 4: The subject of this AD is addressed in French airworthiness directives F-2005-089, dated
June 8, 2005; and F-2005-090 R1, dated July 6, 2005.
2007-03-09 3
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Incorporation by Reference
(e) Unless otherwise specified in this AD, the actions must be done in accordance with the
applicable service information specified in Table 1 of this AD. 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. To get copies of this service information, contact Airbus, 1 Rond Point Maurice Bellonte, 31707
Blagnac Cedex, France. To inspect copies of this service information, go to the FAA, Transport
Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or to 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
Service Information Revision Level Date
Airbus A300-600 All Operators Telex 57A6096 01 April 11, 2005
Airbus A310 All Operators Telex 57A2085 01 April 11, 2005
Airbus Service Bulletin A300-57-0244 Original March 4, 2005
Airbus Service Bulletin A300-57-6099 Original February 23, 2005
Airbus Service Bulletin A310-57-2086 Original March 1, 2005
Effective Date
(f) This amendment becomes effective on March 12, 2007.
Issued in Renton, Washington, on January 24, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification Service.
[FR Doc. E7-1601 Filed 2-2-07; 8:45 am]
　
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