曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

(3) Reporting Requirements: For any reporting requirement in this AD, under the provisions of
the Paperwork Reduction Act, the Office of Management and Budget (OMB) has approved the
information collection requirements and has assigned OMB Control Number 2120-0056.
(4) Special Flight Permits: We are not allowing special flight permits, as described in Section
21.197 and Section 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199).
Related Information
(g) Refer to MCAI European Aviation Safety Agency (EASA) Emergency Airworthiness
Directive 2006-0372-E, dated December 14, 2006; and Airbus Service Bulletins A300-57A0248 and
A300-57A6105, both including Appendix 01, both dated December 12, 2006, for related information.
Material Incorporated by Reference
(h) You must use Airbus Service Bulletin A300-57A0248, excluding Appendix 01, dated
December 12, 2006; or Airbus Service Bulletin A300-57A6105, excluding Appendix 01, dated
December 12, 2006; as applicable; to do the actions required by this AD, unless the AD specifies
otherwise.
(1) The Director of the Federal Register approved the incorporation by reference of this service
information under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) For service information identified in this AD, contact Airbus, 1 Rond Point Maurice Bellonte,
31707 Blagnac Cedex, France.
(3) You may review copies 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.
Issued in Renton, Washington, on January 26, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification Service.
22 BW 2007-04
FAA
Aircraft Certification Service
AIRWORTHINESS DIRECTIVE
www.faa.gov/aircraft/safety/alerts/
www.gpoaccess.gov/fr/advanced.html
2007-03-19 Bombardier, Inc. (Formerly Canadair): Amendment 39-14930. Docket No. FAA-
2006-25192; Directorate Identifier 2006-NM-004-AD.
Effective Date
(a) This AD becomes effective March 15, 2007.
Affected ADs
(b) This AD supersedes AD 2004-14-16.
Applicability
(c) This AD applies to Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440)
airplanes, serial numbers 7003 and subsequent; certificated in any category; equipped with main
landing gear (MLG) main fittings, part numbers (P/N) 601R85001-81 and 601R85001-82 (Messier
Dowty Incorporated P/Ns 17064-105 and 17064-106).
Unsafe Condition
(d) This AD results from stress analyses that showed certain main fittings of the MLGs are
susceptible to premature cracking, starting in the radius of the upper lug. We are issuing this AD to
detect and correct premature cracking of the main fittings of the MLGs, which could result in failure
of the fittings and consequent collapse of the MLGs during 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.
Restatement of the Requirements of AD 2004-14-16
Detailed Inspection of Main Fittings of the MLGs
(f) Before the accumulation of 2,500 total flight cycles on the MLGs, or within 250 flight cycles
after August 13, 2004 (the effective date of AD 2004-14-16), whichever occurs later: Do a detailed
inspection on the main fittings of the MLGs to detect discrepancies (i.e., linear paint cracks or lack of
paint (paint peeling), any other paint damage, adhesion, paint bulging, or corrosion), in accordance
with Part A of the Accomplishment Instructions of Bombardier Alert Service Bulletin (ASB) A601R-
32-088, dated February 20, 2003; or Bombardier ASB 601R-32-088, Revision A, dated June 16,
2005, including Appendices, A, B, and C, dated February 20, 2003. Repeat the inspection thereafter
at intervals not to exceed 100 flight cycles until paragraph (k) of this AD is accomplished.
2007-03-19 2
23 BW 2007-04
Note 1: For the purposes of this AD, a detailed inspection is defined as: “An intensive visual
examination of a specific structural area, system, installation, or assembly to detect damage, failure,
or irregularity. Available lighting is normally supplemented with a direct source of good lighting at
intensity deemed appropriate by the inspector. Inspection aids such as mirror, magnifying lenses, etc.,
may be used. Surface cleaning and elaborate access procedures may be required.”
Related Investigative/Corrective Actions
(g) If any discrepancy is detected during any inspection required by paragraph (f) of this AD,
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：航空資料12(32)