Airworthiness Directive

AD 2026-14-08 91 FR 44740 Active

Federal Aviation Administration · 14 CFR part 39

Requires revising the existing airplane flight manual (AFM) for your airplane to provide the flight crew with revised operating limitations, repetitively inspecting certain NLG hydraulic actuator rod ends for cracks, deformation…

FR document
2026-14511
Amendment
39-23409
Published
2026-07-17
Effective
2026-07-20
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

2026-14-08

FR doc 2026-14511 · 91 FR 44740

AD 2026-14-08Published 2026-07-17Effective 2026-07-20

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 revising the existing airplane flight manual (AFM) for your airplane to provide the flight crew with revised operating limitations, repetitively inspecting certain NLG hydraulic actuator rod ends for cracks, deformation, corrosion, damage, and free movement of the spherical bearing, and depending on the results of any inspection, replacing the affected NLG hydraulic actuator rod end with a serviceable part.

Full official abstract

The FAA is adopting a new airworthiness directive (AD) for all Diamond Aircraft Industries GmbH (DAI) Model DA 42, DA 42 NG, and DA 42 M-NG airplanes. This AD was prompted by occurrences of uncommanded rudder deflection caused by a cracked nose landing gear (NLG) hydraulic actuator rod end, which could lead to failure of the NLG actuator and interference with the rudder control system, forcing the rudder into left-hand deflection. This AD requires revising the existing airplane flight manual (AFM) for your airplane to provide the flight crew with revised operating limitations, repetitively inspecting certain NLG hydraulic actuator rod ends for cracks, deformation, corrosion, damage, and free movement of the spherical bearing, and depending on the results of any inspection, replacing the affected NLG hydraulic actuator rod end with a serviceable part. This AD also prohibits the installation of an affected NLG hydraulic actuator rod end unless certain conditions are met. The FAA is issuing this AD to address the unsafe condition on these products.

More directives for Diamond DA42 Twin Star

  1. AD 2025-24-07 Airworthiness Directives; Diamond Aircraft Industries GmbH Airplanes Effective 2026-02-12
  2. AD 2024-06-13 Airworthiness Directives; Diamond Aircraft Industries GmbH Airplanes Effective 2024-05-28
  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