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Airworthiness Directive

AD 98-12-13 63 FR 31106 Active

Federal Aviation Administration · 14 CFR part 39

FR document
98-15083
Amendment
39-10569
Published
1998-06-08
Effective
1998-07-18
Models covered
1
Last live check
2026-09-30

Printed from https://aircraftdirectives.com/ad/98-12-13 · 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

98-12-13

FR doc 98-15083 · 63 FR 31106

AD 98-12-13Published 1998-06-08Effective 1998-07-18

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 modifying the low pitch stop switch support.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Industrie Aeronautiche e Meccaniche (I.A.M.) Model Piaggio P-180 airplanes. This AD requires modifying the low pitch stop switch support. 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 low pitch stop switch support displacement, which could result in an improper cockpit indication that the propeller is in the Beta range and cause loss of control of the airplane.

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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