Airworthiness directives › 2019-14-08
AD 2019-14-08 Airworthiness Directives; Airbus SAS Airplanes
Models named: A300 B4-601, B4-603, B4-620, B4-622, A300 B4-605R, B4-622R, A300 F4-605R, F4-622R, A300 C4-605R Variant F, A310-203. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to all Airbus SAS airplanes identified in paragraphs (c)(1), (c)(2), (c)(3), (c)(4), and (c)(5) of this AD, certificated in any category. (1) Model A300 B4-601, B4-603, B4-620, and B4-622 airplanes. (2) Model A300 B4-605R and B4-622R airplanes. (3) Model A300 F4-605R and F4-622R airplanes. (4) Model A300 C4-605R Variant F airplanes. (5) Model A310-203, -204, -221, -222, -304, -322, -324, and -325 airplanes.
Compliance
Comply with this AD within the compliance times specified, unless already done.
Required actions
Except as specified in paragraph (h) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, European Aviation Safety Agency (EASA) AD 2019-0014, dated January 29, 2019 (“EASA AD 2019-0014”). (h) Exceptions to EASA AD 2019-0014 (1) For purposes of determining compliance with the requirements of this AD: Where EASA AD 2019-0014 refers to its effective date, this AD requires using the effective date of this AD. (2) Where paragraph (1) of EASA AD 2019-0014 specifies a compliance time of “Within 36 months after 19 February 2014,” for this AD, the compliance time for that paragraph is “Within 30 months after May 16, 2016 (the effective date of AD 2016-07-22).” (3) Where paragraph (3) of EASA AD 2019-0014 specifies a date of “06 September 2016,” for this AD, use “May 16, 2016 (the effective date of AD 2016-07-22).” (4) For Group 1 and Group 3 airplanes: This paragraph provides credit for actions required by paragraph (1) of EASA AD 2019-0014, if those actions were performed before the effective date of this AD using Airbus Service Bulletin A300-24-6103, Revision 03, dated July 3, 2015, provided that the additional work specified in paragraphs (6) and (7) of EASA AD 2019-0014 is accomplished. (5) The “Remarks” section of EASA AD 2019-0014 does not apply to this AD.
Unsafe condition
This AD was prompted by reports of insufficient clearance for the electrical wiring bundles in the leading and trailing edges of the right-hand (RH) and left-hand (LH) wings. The FAA is issuing this AD to address insufficient clearance between wing structures and electrical wiring, which could lead to chafing damage and arcing, possibly resulting in an on-board fire.
Affected ADs
This AD replaces AD 2016-07-22, Amendment 39-18467 (81 FR 21236, April 11, 2016) (“AD 2016-07-22”).
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