Airworthiness Directive

AD 2024-06-13 89 FR 29247 Active

Federal Aviation Administration · 14 CFR part 39

Requires replacing the rudder T-yoke bolt (axle) with a serviceable part, installing a new self-locking nut, and applying torque seal marks on the rudder T-yoke bolt head and self-locking nut.

FR document
2024-08539
Amendment
39-22718
Published
2024-04-22
Effective
2024-05-28
Models covered
1

Last live check: 2026-08-19

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.
AD

2024-06-13

FR doc 2024-08539 · 89 FR 29247

AD 2024-06-13Published 2024-04-22Effective 2024-05-28

Supersedes 2022-21-15

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 replacing the rudder T-yoke bolt (axle) with a serviceable part, installing a new self-locking nut, and applying torque seal marks on the rudder T-yoke bolt head and self-locking nut.

Full official abstract

The FAA is superseding Airworthiness Directive (AD) 2022-21-15 for certain Diamond Aircraft Industries GmbH (DAI) Model DA 42, DA 42 NG, and DA 42 M-NG airplanes. AD 2022-21-15 required replacing the rudder T-yoke axle with an improved rudder T-yoke axle. Since the FAA issued AD 2022-21-15, the European Union Aviation Safety Agency (EASA) superseded its mandatory continuing airworthiness information (MCAI) to correct an unsafe condition on these products. This AD requires, for certain airplanes, inspecting the rudder steering bracket edge distance and depending on the inspection results, inspecting the T-yoke bolt hole for wear and play, and corrective action if necessary. For certain airplanes this AD requires replacing the rudder T-yoke bolt (axle) with a serviceable part, installing a new self-locking nut, and applying torque seal marks on the rudder T-yoke bolt head and self-locking nut. For all airplanes this AD requires repetitively inspecting the torque seal marks on the rudder T-yoke bolt head for proper alignment and the self-locking nut for proper installation and corrective action if necessary. This AD also prohibits the installation of affected parts. The FAA is issuing this AD to address the unsafe condition on these products.

More directives for Diamond DA42 Twin Star

  1. AD 2026-14-08 Airworthiness Directives; Diamond Aircraft Industries GmbH Effective 2026-07-20
  2. AD 2025-24-07 Airworthiness Directives; Diamond Aircraft Industries GmbH Airplanes Effective 2026-02-12
  3. AD 2022-21-15 Airworthiness Directives; Diamond Aircraft Industries GmbH Airplanes Effective 2022-12-14
  4. AD 2022-06-08 Airworthiness Directives; Diamond Aircraft Industries GmbH Airplanes Effective 2022-05-09
  5. AD 2022-03-01 Airworthiness Directives; Diamond Aircraft Industries GmbH Airplanes Effective 2022-03-17

All Diamond DA42 Twin Star directives

Applies to 1 model in our index