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Airworthiness directives › 2017-12-06

AD 2017-12-06 Airworthiness Directives; Airbus Airplanes

2017-07-25
2017-06-20
39-18921
FAA-2016-9574
Airframe
—

Models named: A300 B2-1A, B2-1C, B2K-3C, B2-203, B4-2C, B4-103, B4-203, A300 B4-601, B4-603, B4-620. 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) through (c)(6) of this AD, certificated in any category, all manufacturer serial numbers. (1) Model A300 B2-1A, B2-1C, B2K-3C, B2-203, B4-2C, B4-103, and B4-203 airplanes. (2) Model A300 B4-601, B4-603, B4-620, and B4-622 airplanes. (3) Model A300 B4-605R and B4-622R airplanes. (4) Model A300 F4-605R and F4-622R airplanes. (5) Model A300 C4-605R Variant F airplanes. (6) 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

Within 36 months after the effective date of this AD, or before exceeding the applicable airplane design service goal specified in table 1 to paragraph (g) of this AD, whichever occurs later: Identify the part number on the forward passenger doors on the left-hand and right-hand sides, in accordance with the Accomplishment Instructions of the applicable service information identified in paragraph (g)(1), (g)(2), or (g)(3) of this AD. (1) Airbus Service Bulletin A300-52-0180, Revision 01, dated October 14, 2014 (for Model A300 airplanes). (2) Airbus Service Bulletin A300-52-6084, Revision 01, dated October 16, 2014 (for Model A300-600 series airplanes). (3) Airbus Service Bulletin A310-52-2076, Revision 01, dated October 14, 2014. Table 1 to Paragraph ( g ) of This AD—Design Service Goal Airplane model/series Design service goal flight cycles or flight hours A300 B2-100, B2-200, B2-320 Before the accumulation of 48,000 total flight cycles. A300 B4-100 Before the accumulation of 40,000 total flight cycles. A300 B4-200 Before the accumulation of 34,000 total flight cycles. A300 B4-600, B4-600R, F4-600R, C4-600R Before the accumulation of 30,000 total flight cycles or 67,500 total flight hours, whichever occurs first. A310-200 Before the accumulation of 40,000 total flight cycles or 60,000 total flight hours, whichever occurs first. A310-300 Before the accumulation of 35,000 total flight cycles or 60,000 total flight hours, whichever occurs first.

Unsafe condition

This AD is intended to complete certain mandated programs intended to support the airplane reaching its limit of validity (LOV) of the engineering data that support the established structural maintenance program. We are issuing this AD to detect and correct widespread fatigue damage of the forward passenger doors, which could result in reduced structural integrity of the airplane.

Affected ADs

None.

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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