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Airworthiness directives › 2017-19-23

AD 2017-19-23 Airworthiness Directives; Airbus Airplanes

2017-11-01
2017-09-27
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Airframe
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Models named: A318-111, -112, -121, -122, A319-111, -113, -114, -115, -131, -132. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to the airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Airbus Model A318-111, -112, -121, and -122 airplanes. (2) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Airbus Model A320-211, -212, -214, -231, -232, and -233 airplanes. (4) Airbus Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes.

Compliance

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

Required actions

For the purposes of this AD, a serviceable THSA is a THSA that does not exceed the life limits as identified in table 1 to paragraphs (g) and (j) of this AD. Table 1 to Paragraphs (g) and (j) of This AD— THSA Life Limits Configuration, based on service bulletin (SB) embodiment Compliance time (whichever occurs first) THSA on which United Technologies Corporation Aerospace Systems (UTAS) SB 47145-27-19 has not been embodied Before exceeding 67,500 flight hours (FH) since first installation on an airplane, or before exceeding 48,000 flight cycles (FC) since first installation on an airplane. THSA on which UTAS SB 47145-27-19 has been embodied Before exceeding 52,500 FH after embodiment of UTAS SB 47145-27-19 on an airplane, without exceeding 120,000 FH since first installation on an airplane; or before exceeding 27,000 FC after embodiment of UTAS SB 47145-27-19 on an airplane, without exceeding 75,000 FC since first installation on an airplane.

Unsafe condition

This AD was prompted by reports of wear at different levels in the trimmable horizontal stabilizer actuator (THSA). We are issuing this AD to detect and correct wear of the THSA, which could reduce the remaining life of the THSA, possibly resulting in premature failure and consequent reduced controllability of the airplane.

Affected ADs

This AD replaces AD 2015-15-10, Amendment 39-18219 (80 FR 43928, July 24, 2015) (“AD 2015-15-10”).

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