Airworthiness Directive

AD 2012-01-02 77 FR 1624 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2012-208
Amendment
39-16913
Published
2012-01-11
Effective
2012-02-15
Models covered
1
Last live check
2026-10-01
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AD

2012-01-02

FR doc 2012-208 · 77 FR 1624

AD 2012-01-02Published 2012-01-11Effective 2012-02-15

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 Schempp-Hirth Flugzeugbau GmbH Model Discus 2cT gliders. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as small cracks which have been found on engine pylons in the area of the lower engine support that have not been detected during the standard daily inspection. This condition, if not detected and corrected, could lead to an engine pylon failure resulting in loss of control of the glider. We are issuing this AD to require actions to address the unsafe condition on these products.

More directives for Schempp-Hirth

  1. AD 2026-03-04 Airworthiness Directives; Schempp-Hirth Flugzeugbau GmbH Gliders 2026-03-05
  2. AD 2025-04-14 Airworthiness Directives; Schempp-Hirth Flugzeugbau GmbH Gliders 2025-03-04
  3. AD 2023-17-05 Airworthiness Directives; Schempp-Hirth Flugzeugbau GmbH Gliders 2023-09-07
  4. AD 2023-03-14 Airworthiness Directives; Schempp-Hirth Flugzeugbau GmbH Gliders 2023-03-01
  5. AD 2023-03-22 Airworthiness Directives; DG Flugzeugbau GmbH and Schempp-Hirth Flugzeug... 2023-03-01

All Schempp-Hirth directives

Applies to 1 model in our index