Airworthiness Directive 95-28146

one-time
AD 95-28146 · 1995-11-15 · airframe

Airworthiness Directives; The New Piper Aircraft, Inc. (Formerly Piper Aircraft Corporation) PA24, PA28R, PA30, PA32R, PA34, and PA39 Series Airplanes; Correction

What this AD requires

This action makes a correction to Airworthiness Directive (AD) 95-20-07 concerning The New Piper Aircraft, Inc. (Piper) PA24, PA28R, PA30, PA32R, PA34, and PA39 airplanes, which was published in the Federal Register on October 5, 1995 (60 FR 52073). That publication incorrectly references who may accomplish the inspections of the left and right main gear side brace studs. The AD currently requires the inspection ``* * * by a facility approved by the FAA. * * *'' The Federal Aviation Administration's intent is to have this inspection accomplished ``by a facility or person authorized by the FAA. * * *'' This action corrects the AD to reflect this change.

Which aircraft AD 95-28146 applies to

MakesPiper
ModelsPA-24, PA-28R, PA-30, PA-32R, PA-34, PA-39

Whether AD 95-28146 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.

How AD compliance is recorded

A valid compliance record (14 CFR 43.9) states:

Method of complianceThe specific action taken (inspected, replaced, modified) and to what revision.
DateWhen the work was done.
Aircraft timeTotal time in service / tach at compliance — how recurring next-due is computed.
Signature & certificateThe A&P/IA who returned it to service, with certificate number.
Is AD 95-28146 complied with on your aircraft?

Tailplate reads a tail number’s logbooks and matches every applicable AD — including this one — to its compliance evidence, with recurring next-due dates computed.

Look up a tail number →Read the full directive (Federal Register)

Applicability is derived from the FAA directive corpus and is advisory, not a legal airworthiness determination. Compliance is established only from an aircraft’s actual records.