Airworthiness Directive 97-8250
recurringAirworthiness Directives; The New Piper Aircraft, Inc. PA24, PA28R, PA30, PA32R, PA34, and PA39 Series Airplanes; Correction
What this AD requires
This document makes a correction to Airworthiness Directive (AD) 97-01-01, which was published in the Federal Register on January 2, 1997 (62 FR 10), and concerns The New Piper Aircraft, Inc. (Piper) PA24, PA28R, PA30, PA32R, PA34, and PA39 series airplanes. The amendment number in this AD is incorrectly referenced as Amendment 39- 9782 instead of 39-9872 in two places. All other reference is correct. The AD currently requires repetitively inspecting the main gear sidebrace studs for cracks, and replacing any main gear sidebrace stud found cracked. This action corrects the AD to reflect the right amendment number throughout the entire document.
Which aircraft AD 97-8250 applies to
Whether AD 97-8250 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:
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.