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Airworthiness Directive

AD 2025-15-10 90 FR 35831 Active

Federal Aviation Administration · 14 CFR part 39

Federal Register (opens in a new tab)FAA DRS (opens in a new tab)

FR document
2025-14390
Amendment
39-23097
Published
2025-07-30
Effective
2025-09-03
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/2025-15-10 · 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

2025-15-10

FR doc 2025-14390 · 90 FR 35831

AD 2025-15-10Published 2025-07-30Effective 2025-09-03

Supersedes 2023-25-03

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) 2023-25- 03, which applied to certain Piaggio Aviation S.p.A.

Full official abstract

The FAA is superseding Airworthiness Directive (AD) 2023-25- 03, which applied to certain Piaggio Aviation S.p.A. (Piaggio) Model P- 180 airplanes. AD 2023-25-03 required a one-time detailed inspection of the horizontal stabilizer (HS) central box for corrosion; an assessment of the corrosion level; and depending on the determination, repetitive detailed inspections of the HS central box for corrosion and the internal composite structure for surface cracks, distortion, and damage; and repair or replacement of the HS assembly. Repair or replacement of the HS assembly was terminating action for the repetitive inspections. Since the FAA issued AD 2023-25-03, it was determined that AD 2023-25-03 imposed an unintended restriction that is not in the mandatory continuing airworthiness information (MCAI). This AD retains certain actions of AD-2023-25-03 and removes the unintended restriction. The FAA is issuing this AD to address the unsafe condition on these products.

More directives for Piaggio P.180 Avanti

  1. AD 2026-06-05 Airworthiness Directives; Baykar Piaggio Aerospace S.p.A. (Type Certific... Effective 2026-05-11
  2. AD 2026-05-10 Airworthiness Directives; Baykar Piaggio Aerospace S.p.A. (Type Certific... Effective 2026-04-27
  3. AD 2025-26-05 Airworthiness Directives; Baykar Piaggio Aerospace S.p.A. (Type Certific... Effective 2026-02-17
  4. AD 2023-25-03 Airworthiness Directives; Piaggio Aviation S.p.A. Airplanes Effective 2024-02-02
  5. AD 2023-16-04 Airworthiness Directives; Piaggio Aviation S.p.A. Airplanes Effective 2023-08-30

All Piaggio P.180 Avanti 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