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Airworthiness directives › 2017-07-05

AD 2017-07-05 Airworthiness Directives; Airbus Airplanes

Superseded. This directive was replaced by AD 2019-03-10. Work to the current one.
2017-05-08
2017-04-03
39-18843
FAA-2016-8184
Airframe
2019-03-10

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)(5) 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.

Compliance

Comply with this AD within the compliance times specified, unless already done.

Required actions

Within the compliance time specified in paragraphs (g)(1) and (g)(2) of this AD, whichever occurs later, and thereafter at intervals not to exceed 100 flight cycles: Accomplish a detailed visual inspection of the internal diameter of each affected MLG hinge arm/barrel pin, in accordance with the instructions of Airbus Alert Operators Transmission (AOT) A32W008-16, dated February 25, 2016, including Appendices 1 through 4. The affected MLG hinge arm/barrel pins are those with part number C66441-(x) and part number C65543-(x), where the x represents a variable number. (1) Within 30 months since the pin's first flight on an airplane, or since the pin's first flight on an airplane after overhaul, as applicable. (2) Within 30 days after the effective date of this AD.

Unsafe condition

This AD was prompted by reports of cracks in main landing gear (MLG) leg components. We are issuing this AD to detect and correct cracking of certain components in the MLG leg, which could result in a MLG collapse, and consequent damage to the airplane and injury to the airplane occupants.

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