Airworthiness directives › 2016-18-07
AD 2016-18-07 Airworthiness Directives; Airbus Airplanes
Models named: A330-223F, -243F, -201, -202, -203, -223, -243, -301, -302, -303. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to the airplanes identified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category, all manufacturer serial numbers (MSN), except those on which Airbus modification 58896 has been embodied in production. (1) Airbus Model A330-223F, -243F, -201, -202, -203, -223, -243, -301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes. (2) Airbus Model A340-211, -212, -213, -311, -312, and -313 airplanes.
Compliance
Comply with this AD within the compliance times specified, unless already done.
Required actions
For airplanes equipped with basic MLG (201252 series), or growth MLG (201490 series): After 54 months at the earliest, but no later than 72 months since the left-hand (LH) or right-hand (RH) MLG bogie beam's first flight on an airplane, or since its first flight on an airplane after overhaul, as applicable, clean the internal bore and accomplish a detailed inspection of internal surfaces of the LH and RH MLG bogie beams to detect any damage to the protective treatments and any corrosion, and measure the paint thickness on the internal bore, in accordance with the Accomplishment Instructions of Airbus Service Bulletin A330-32-3225, Revision 02, including Appendix 1, dated October 26, 2012; or Airbus Service Bulletin A340-32-4268, Revision 03, including Appendix 1, dated January 14, 2013; as applicable. Repeat the inspections thereafter at intervals not less than 54 months, but not exceeding 72 months, after the most recent inspection. During overhaul of a MLG bogie beam, any corrosion will be removed, which means that the first inspection after overhaul of that MLG bogie beam, as required by this paragraph, is between 54 months and 72 months since its first flight on an airplane after overhaul.
Unsafe condition
This AD was prompted by reports of thin paint coats and paint degradation on enhanced main landing gear (MLG) bogie beams, as well as reports that some airplanes have been inspected too early and not re-inspected as needed. We are issuing this AD to detect and correct damage or corrosion of the MLG bogie beams, which could cause a runway excursion event, bogie beam detachment from the airplane, or MLG collapse, and could result in damage to the airplane and injury to the occupants.
Affected ADs
This AD replaces AD 2009-15-17, Amendment 39-15980 (74 FR 37523, July 29, 2009) (“AD 2009-15-17”).
Read the original on the Federal Register →
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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1