Airworthiness directives › 2017-14-01
AD 2017-14-01 Airworthiness Directives; Airbus Airplanes
Models named: A330-201, -202, -203, -223, -223F, -243, -243F, -301, -302, -303. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to Airbus airplanes identified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category, all serial numbers, except those airplanes that have embodied Airbus Modification 204421 or Airbus Modification 205289 in production. (1) Model A330-201, -202, -203, -223, -223F, -243, -243F, -301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes. (2) 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 Model A330-200, -200 Freighter, and -300 series airplanes; and Model A340-200 and -300 series airplanes; equipped with a MLG having part number (P/N) 201252 series, P/N 201490 series, or P/N 10-210 series: Do the applicable actions required by paragraph (g)(1) or (g)(2) of this AD. (1) For airplanes equipped, as of the effective date of this AD, with a MLG that has been previously inspected, as specified in Airbus Service Bulletin A330-32-3220, Airbus Service Bulletin A330-32-3248, Airbus Service Bulletin A340-32-4264, or Airbus Service Bulletin A340-32-4286, as applicable: At the applicable times specified in paragraphs (h)(1) and (h)(2) of this AD, do a detailed inspection for damage ( e.g., cracking and fretting) and corrosion of the MLG sliding piston sub-assembly, bogie beam stop pad, and the bogie beam under the stop pad; and do all applicable related investigative and corrective actions; in accordance with the Accomplishment Instructions of Airbus Service Bulletin A330-32-3248, Revision 05, including Appendix 1, dated May 4, 2016; or Airbus Service Bulletin A340-32-4286, Revision 02, including Appendix 1, dated January 5, 2016; as applicable; except as required by paragraph (j) of this AD. Do all applicable related investigative and corrective actions before further flight. Repeat the inspection of the MLG sliding piston sub-assembly, bogie beam stop pad, and the bogie beam under the stop pad, thereafter, at intervals not to exceed 2,500 flight cycles or 24 months, whichever occurs first. (2) For airplanes equipped, as of the effective date of this AD, with a MLG that has not been previously inspected, as specified in Airbus Service Bulletin A330-32-3220, Airbus Service Bulletin A330-32-3248, Airbus Service Bulletin A340-32-4264, or Airbus Service Bulletin A340-32-4286, as applicable: At the applicable times specified in paragraphs (h)(3) and (h)(4) of this AD, do a detailed inspection for damage ( e.g., cracking and fretting) and corrosion of the MLG sliding piston sub-assembly, bogie beam stop pad, and the bogie beam under the stop pad; and do all applicable related investigative and corrective actions; in accordance with the Accomplishment Instructions of Airbus Service Bulletin A330-32-3248, Revision 05, including Appendix 1, dated May 4, 2016; or Airbus Service Bulletin A340-32-4286, Revision 02, including Appendix 1, dated January 5, 2016; as applicable; except as required by paragraph (j) of this AD. Do all applicable related investigative and corrective actions before further flight. Repeat the inspection of the MLG sliding piston sub-assembly, bogie beam stop pad, and the bogie beam under the stop pad, thereafter, at intervals not to exceed 2,500 flight cycles or 24 months, whichever occurs first.
Unsafe condition
This AD was prompted by reports of corroded and cracked bogie beams under the bogie stop pad. We are issuing this AD to detect and correct damage or corrosion under the bogie stop pad of both main landing gear (MLG) bogie beams; this condition could result in a damaged bogie beam and consequent detachment of the beam from the airplane, collapse of the MLG, or departure of the airplane from the runway, possibly resulting in damage to the airplane and injury to occupants.
Affected ADs
This AD replaces AD 2013-10-03, Amendment 39-17456 (78 FR 31386, May 24, 2013) (“AD 2013-10-03”).
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