AircraftDirectives
MembershipSign inCreate free account
Menu
Airworthiness Directive

AD 99-07-10 64 FR 14824 Active

Federal Aviation Administration · 14 CFR part 39

FR document
99-7382
Amendment
39-11095
Published
1999-03-29
Effective
1999-05-10
Models covered
1
Last live check
2026-09-30

Printed from https://aircraftdirectives.com/ad/99-07-10 · 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.

Opens your browser's print dialog. Choose “Save as PDF” to export a file. Keyboard: Ctrl+P or Cmd+P.

AD

99-07-10

FR doc 99-7382 · 64 FR 14824

AD 99-07-10Published 1999-03-29Effective 1999-05-10

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 inspecting the upper and lower engine nacelle inner panels for any loose or partially detached inner film, and removing any loose or partially detached inner film.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to all Industrie Aeronautiche e Meccaniche (I.A.M.) Model Piaggio P-180 airplanes. This AD requires inspecting the upper and lower engine nacelle inner panels for any loose or partially detached inner film, and removing any loose or partially detached inner film. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Italy. The actions specified by this AD are intended to prevent the accumulation of loose particles on the engine inlet screen caused by film delamination, which could result in reduced engine power and possible loss of airplane control.

More directives for Piaggio P.180 Avanti

  1. AD 2026-06-05 Airworthiness Directives; Baykar Piaggio Aerospace S.p.A. (Type Certific... 2026-04-06
  2. AD 2026-05-10 Airworthiness Directives; Baykar Piaggio Aerospace S.p.A. (Type Certific... 2026-03-23
  3. AD 2025-26-05 Airworthiness Directives; Baykar Piaggio Aerospace S.p.A. (Type Certific... 2026-01-12
  4. AD 2025-15-10 Airworthiness Directives; Piaggio Aviation S.p.A. Airplanes 2025-07-30
  5. AD 2023-25-03 Airworthiness Directives; Piaggio Aviation S.p.A. Airplanes 2023-12-29

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)

Applies to 1 model in our index