Is AD 98-2641 a recurring Airworthiness Directive?

No — AD 98-2641 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 98-2641 apply to?

AD 98-2641 applies to Airbus — models A300-600, A310. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 98-2641

one-time

AD 98-2641 · 1998-02-05 · airframe

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

What this AD requires

This amendment adopts a new airworthiness directive (AD), applicable to all Airbus Model A300, A310, and A300-600 series airplanes. For certain airplanes, this amendment requires replacing the bearings of the throttle control levers with new sealed bearings. For certain other airplanes, this amendment requires replacing the throttle control assemblies with new assemblies. This amendment is prompted by the issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by this AD are intended to prevent asymmetric engine thrust on the airplane when the autothrottle is engaged, which could result in roll and yaw disturbances, and consequent reduced controllability of the airplane.

Which aircraft AD 98-2641 applies to

MakesAirbus

ModelsA300-600, A310

certain

Whether AD 98-2641 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 98-2641 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.