Airworthiness Directive

AD 2023-03-22 88 FR 12820 Active

Federal Aviation Administration · 14 CFR part 39

Requires repetitive replacement of the eccentric axle, adds the Schempp-Hirth Model Duo Discus T gliders to the applicability, and retains from AD 2015-09-04 R1 the option of operating the glider with the engine non-operative…

FR document
2023-03997
Amendment
39-22347
Published
2023-03-01
Effective
2023-04-05
Models covered
2

Last live check: 2026-08-19

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AD

2023-03-22

FR doc 2023-03997 · 88 FR 12820

AD 2023-03-22Published 2023-03-01Effective 2023-04-05

Supersedes 2015-09-04 R1

Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.

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 repetitive replacement of the eccentric axle, adds the Schempp-Hirth Model Duo Discus T gliders to the applicability, and retains from AD 2015-09-04 R1 the option of operating the glider with the engine non-operative instead of replacing the eccentric axle.

Full official abstract

The FAA is superseding Airworthiness Directive (AD) 2015-09-04 R1, which applied to DG Flugzeugbau GmbH Model DG-1000T gliders equipped with a Solo Kleinmotoren GmbH (currently Solo Vertriebs-und Entwicklungs-GmbH) (Solo) Model 2350 C engine. AD 2015-09-04 R1 prohibited operation of the engine and required performing a magnetic particle or dye penetrant inspection of the propeller shaft and reporting the results of the inspection to Solo. This AD is prompted by mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI identifies the unsafe condition as occurrences of rupture of the eccentric axle on Solo Model 2350 C engines (installed on DG Flugzeugbau GmbH Model DG-1000T gliders in the United States) and an occurrence on a Solo Model 2350 D engine (installed on Schempp-Hirth Flugzeugbau GmbH (Schempp-Hirth) Model Duo Discus T gliders in the United States). This AD requires repetitive replacement of the eccentric axle, adds the Schempp-Hirth Model Duo Discus T gliders to the applicability, and retains from AD 2015-09-04 R1 the option of operating the glider with the engine non-operative instead of replacing the eccentric axle. The FAA is issuing this AD to address the unsafe condition on these products.

More directives for DG Flugzeugbau

  1. AD 2026-07-03 Airworthiness Directives; DG Aviation GmbH (Type Certificate Previously ... Effective 2026-04-20
  2. AD 2025-13-08 Airworthiness Directives; DG Aviation GmbH (Type Certificate Previously ... Effective 2025-07-25
  3. AD 2024-19-12 Airworthiness Directives; DG Aviation GmbH (Type Certificate Previously ... Effective 2024-10-15
  4. AD 2022-04-01 Airworthiness Directives; DG Flugzeugbau GmbH and Schempp-Hirth Flugzeug... Effective 2022-03-29
  5. AD 2021-24-19 Airworthiness Directives; DG Flugzeugbau GmbH Gliders Effective 2022-01-27

All DG Flugzeugbau directives

Applies to 2 models in our index