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Instructions of Airbus Service Bulletin A300-24-0100, dated April 7, 2005.
(2) For Model A300 B4-601, B4-603, B4-620, B4-622, B4-605R, B4-622R, A300 F4-605R, F4-
622R, and C4-605R Variant F airplanes; except those on which Airbus Modifications 11763 and
12995 have been done: Do the actions specified in paragraph (i) of this AD in accordance with the
Accomplishment Instructions of Airbus Service Bulletin A300-24-6084, Revision 01, dated June 28,
2005.
(3) For Model A310 airplanes, except those on which Airbus Modification 11763 has been done:
Do the actions specified in paragraph (i) of this AD in accordance with the Accomplishment
Instructions of Airbus Service Bulletin A310-24-2091, dated March 4, 2005.
2007-03-10 3
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Parts Installation
(j) After the effective date of this AD, no person may install on any airplane plate assemblies
with part numbers A5351088000000 or A5351088000100 unless they have been modified in
accordance with paragraph (f) of this AD.
Actions Accomplished According to Previous Revisions of Service Bulletins
(k) Actions done before the effective date of this AD in accordance with the service bulletins
identified in Table 1 of this AD are acceptable for compliance with the corresponding requirements in
this AD.
Table 1 – Previous Revisions of Service Bulletins
Airbus Service Bulletin Revision Level Date
A300-24-0085 Original December 12, 1994
A300-24-0085 03 January 17, 1996
A300-24-0085 04 July 23, 1996
A300-24-0085 05 March 6, 2001
A300-24-6004 1 January 28, 1988
A300-24-6004 2 February 24, 1995
A300-24-6004 03 June 30, 1998
A300-24-6043 Original December 12, 1994
A300-24-6043 01 February 7, 1995
A300-24-6043 02 May 10, 1995
A300-24-6043 03 January 17, 1996
A300-24-6043 04 March 6, 2001
A300-24-6043 05 August 30, 2001
A300-24-6043 06 October 13, 2005
A300-24-6084 Original March 4, 2005
A300-28-6056 Original February 18, 1998
A310-24-2009 Original May 31, 1985
A310-24-2009 1 January 28, 1988
A310-24-2009 2 February 24, 1995
A310-24-2009 03 June 30, 1998
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Alternative Methods of Compliance (AMOCs)
(l)(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 § 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
(m) European Aviation Safety Agency airworthiness directive 2006-0074, dated April 3, 2006,
also addresses the subject of this AD.
Material Incorporated by Reference
(n) You must use the service information specified in Table 2 of this AD to 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 2 – Material Incorporated by Reference
Airbus Service Bulletin Revision Level Date
A300-24-0085 06 October 13, 2005
A300-24-0100 Original April 7, 2005
A300-24-6004 04 November 15, 2005
A300-24-6043 07 October 11, 2006
A300-24-6084 01 June 28, 2005
A300-28-6056 01 January 20, 2006
A310-24-2009 04 November 15, 2005
A310-24-2091 Original March 4, 2005
Issued in Renton, Washington, on January 24, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification Service.
[FR Doc. E7-1602 Filed 2-2-07; 8:45 am]
2007-03-10 3
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FAA
Aircraft Certification Service
AIRWORTHINESS DIRECTIVE
www.faa.gov/aircraft/safety/alerts/
www.gpoaccess.gov/fr/advanced.html
2007-03-11 Bombardier, Inc. (Formerly Canadair): Amendment 39-14922. Docket No. FAA-
2006-26046; Directorate Identifier 2006-NM-172-AD.
Effective Date
(a) This AD becomes effective March 12, 2007.
Affected ADs
(b) None.
Applicability
　
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