Is AD 98-13-08 a recurring Airworthiness Directive?

No — AD 98-13-08 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 98-13-08 apply to?

AD 98-13-08 applies to Pilatus — models PC-12. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 98-13-08

one-time

Official AD 98-13-08 · FR doc 98-16023 · 1998-06-17 · airframe

Airworthiness Directives; Pilatus Aircraft Ltd. Model PC-12 Airplanes

What this AD requires

This amendment adopts a new airworthiness directive (AD) that applies to certain Pilatus Aircraft Ltd. (Pilatus) Model PC-12 airplanes. This AD requires replacing and re-routing the power return cables on the starter generator and generator 2, inserting a temporary revision to the pilot operating handbook (POH), and installing a placard near the standby magnetic compass. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Switzerland. The actions specified by this AD are intended to prevent directional deviation on the standby magnetic compass caused by an overload of electrical current in the airplane structure, which could result in flight-path deviation during critical phases of flight in icing conditions and instrument meteorologic conditions (IMC).

Which aircraft AD 98-13-08 applies to

MakesPilatus

ModelsPC-12

Requires re-routing/replacing the starter generator cable and generator 2 power return cables, POH revision, and a placard near the standby magnetic compass per Pilatus PC XII SB No. 24-002, Rev. 1, dated Sept 20, 1996, to prevent standby compass deviation from electrical overload. Model identified as 'PC XII' (PC-12) in the text; specific serial-number applicability not present in this excerpt.

Whether AD 98-13-08 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 98-13-08 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.