Is AD 98-32097 a recurring Airworthiness Directive?

No — AD 98-32097 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 98-32097 apply to?

AD 98-32097 applies to Airbus — models A300-600. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 98-32097

one-time

AD 98-32097 · 1998-12-04 · airframe

Airworthiness Directives; Airbus Model A310 and A300-600 Series Airplanes

What this AD requires

This document corrects a typographical error that appeared in airworthiness directive (AD) 98-11-19 that was published in the Federal Register on May 28, 1998 (63 FR 29096). The typographical error in the applicability statement of the AD resulted in a reference to an engine model that does not exist. This AD is applicable to certain Airbus Model A310 and A300-600 series airplanes. This AD requires a visual inspection to detect cracks in the aft mount beam assembly of the engine; and replacement of any cracked beam with a new beam or beam assembly; and a fluorescent penetrant inspection to detect cracks in the aft mount beam assembly of the engine, and various follow-on actions.

Which aircraft AD 98-32097 applies to

MakesAirbus

ModelsA300-600

certain

Whether AD 98-32097 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 compliance — The specific action taken (inspected, replaced, modified) and to what revision.

Date — When the work was done.

Aircraft time — Total time in service / tach at compliance — how recurring next-due is computed.

Signature & certificate — The A&P/IA who returned it to service, with certificate number.

Is AD 98-32097 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.