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Airworthiness Directive

AD 2025-26-02 91 FR 555 Active

Federal Aviation Administration · 14 CFR part 39

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FR document
2026-00162
Amendment
39-23224
Published
2026-01-08
Effective
2026-02-12
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/2025-26-02 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

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.

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AD

2025-26-02

FR doc 2026-00162 · 91 FR 555

AD 2025-26-02Published 2026-01-08Effective 2026-02-12

Supersedes 2007-06-11

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.

The FAA is superseding Airworthiness Directive (AD) 2007-06-11 (AD 2007-06-11) for certain SOCATA (type certificate now held by DAHER AEROSPACE) Model TBM 700 airplanes.

Full official abstract

The FAA is superseding Airworthiness Directive (AD) 2007-06-11 (AD 2007-06-11) for certain SOCATA (type certificate now held by DAHER AEROSPACE) Model TBM 700 airplanes. AD 2007-06-11 required repetitively inspecting the vertical stabilizer attachment fittings and bolts for cracks or corrosion, and, if necessary, repairing or replacing the damaged part and then applying a corrosion protection reinforcement. Since the FAA issued AD 2007-06-11, the European Union Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union, superseded the previous Direction generale de l'aviation civile (DGAC) France AD to introduce new service information providing instructions for installing new vertical stabilizer attachment fittings having improved corrosion resistant material as an optional terminating action for the repetitive inspections. This AD retains the requirements of AD 2007-06-11 and includes a new optional terminating action for the repetitive inspections. The FAA is issuing this AD to address the unsafe condition on these products.

More directives for SOCATA/Daher TBM 700

  1. AD 2025-02-08 Airworthiness Directives; DAHER AEROSPACE (Type Certificate Previously H... Effective 2025-03-19
  2. AD 2025-01-04 Airworthiness Directives; DAHER AEROSPACE (Type Certificate Previously H... Effective 2025-03-11
  3. AD 2023-11-12 Airworthiness Directives; DAHER AEROSPACE (Type Certificate Previously H... Effective 2023-07-21
  4. AD 2021-25-10 Airworthiness Directives; Daher Aerospace (Type Certificate Previously H... Effective 2022-01-24
  5. AD 2021-24-13 Airworthiness Directives; Daher Aerospace (Type Certificate Previously H... Effective 2022-01-12

All SOCATA/Daher TBM 700 directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 1 model in our index