Piper PA-42 Cheyenne III / IV Airworthiness Directives (ADs)

12 ADs referencing the Piper PA-42 Cheyenne III / IV (PA-42-1000 Cheyenne 400LS) family · FAA quick reference

Quick reference only — not a compliance record. This list is for research convenience and may be incomplete or out of date. It is not an airworthiness compliance determination. Always verify against the official FAA record, and check directly with the FAA before relying on it. ADs are mandatory; STCs indicate approval for the type (not installation on a specific airframe); SAIBs are advisory.

Airworthiness Directives (ADs) applicable to the Piper PA-42 Cheyenne III / IV family, sourced from the FAA. ADs are mandatory; this list is a quick reference for research and is NOT a compliance record.

Document	Title / Subject	Date
2009-13-06 R1	Airworthiness Directives; Piper Aircraft, Inc. Airplanes	2011-09-20
2009-13-06	Airworthiness Directives; Piper Aircraft, Inc. PA-23, PA-31, and PA-42 Series Airplanes	2009-06-12
2005-01-19	Airworthiness Directives; GARMIN International Inc. GTX 33, GTX 33D, GTX 330, and GTX 330D Mode S Transponders	2005-01-07

+ 9 more ADs for the Piper PA-42 Cheyenne III / IV family.

The complete, searchable Airworthiness Directives list — with in-app PDF viewing and a combined download — is part of AeroTell.

See all 12 ADs in the AeroTell app →