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Airworthiness directives › 2019-19-07

AD 2019-19-07 Airworthiness Directives; Airbus SAS Airplanes

2019-11-05
2019-10-01
39-19743
FAA-2019-0482
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 all the Airbus SAS airplanes identified in paragraphs (c)(1) through (6) of this AD, certificated in any category. (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

Except as specified in paragraph (h) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, European Union Aviation Safety Agency (EASA) AD 2019-0078, dated March 29, 2019 (“EASA AD 2019-0078”). All provisions specified in EASA AD 2019-0078 apply in this AD.

Unsafe condition

This AD was prompted by a report indicating that the trimmable horizontal stabilizer (THS) actuator ball nut trunnion lower attachment was missing the THS actuator right-hand spherical bearings and retaining parts (bolt, tab washer, and end cap). The FAA is issuing this AD to address missing THS actuator right-hand spherical bearings and retaining parts from the THS actuator ball nut trunnion lower attachment, which could lead to THS actuator failure, possibly resulting in loss of control 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