Airworthiness Directive

AD 2013-23-19 78 FR 70209 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2013-27920
Amendment
39-17674
Published
2013-11-25
Effective
2013-11-25
Models covered
1
Last live check
2026-10-02
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AD

2013-23-19

FR doc 2013-27920 · 78 FR 70209

AD 2013-23-19Published 2013-11-25Effective 2013-11-25

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires actions to address the unsafe condition on these products.

Full official abstract

We are adopting a new airworthiness directive (AD) for XtremeAir GmbH Model XA42 airplanes. This AD results from mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as cracks in a weld seam between the lower left landing gear attachment bearing and the lower engine mount to the firewall attachment plate, which could reduce the structural integrity of the airplane and could result in engine separation. We are issuing this AD to require actions to address the unsafe condition on these products.

More directives for XtremeAir XA42

  1. AD 2020-13-03 Airworthiness Directives; XtremeAir GmbH Airplanes 2020-06-25
  2. AD 2018-07-15 Airworthiness Directives; XtremeAir GmbH Airplanes 2018-04-09

All XtremeAir XA42 directives

Applies to 1 model in our index