Airworthiness Directive 98-24089

one-time
AD 98-24089 · 1998-09-10 · reciprocating engine

Airworthiness Directives; Superior Air Parts, Inc., Piston Pins Installed on Teledyne Continental Motors Reciprocating Engines

What this AD requires

This amendment adopts a new airworthiness directive (AD) that is applicable to Superior Air Parts, Inc., piston pins installed on Teledyne Continental Motors reciprocating engines. This amendment requires removal from service of defective piston pins, and replacement with serviceable parts. This amendment is prompted by reports of numerous piston pin fractures. The actions specified by this AD are intended to prevent a piston pin failure from causing secondary engine damage resulting in loss of oil or total power failure, and from causing jamming of the engine crankshaft resulting in a catastrophic engine failure.

Which aircraft AD 98-24089 applies to

ModelsIO-360-A, IO-360-AB, IO-360-C, IO-360-CB, IO-360-D, IO-360-DB, IO-360-G, IO-360-GB, IO-360-H, IO-360-HB, IO-360-J, IO-360-JB, IO-360-K, IO-360-KB, LTSIO-360-E, LTSIO-360-EB, LTSIO-360-KB, TSIO-360-A, TSIO-360-AB, TSIO-360-B, TSIO-360-C, TSIO-360-CB, TSIO-360-D, TSIO-360-DB, TSIO-360-E, TSIO-360-F, TSIO-360-FB, TSIO-360-GB, TSIO-360-H, TSIO-360-HB, TSIO-360-JB, TSIO-360-KB, TSIO-360-LB, TSIO-360-MB, IO-360, LTSIO-360, TSIO-360
Part-conditionalSA629690.

Applies only to listed TCM engines that had Superior Air Parts, Inc. PMA piston pin P/N SA629690 (shipped by Superior Air Parts between August 1, 1994 and June 20, 1996) installed, and that were overhauled or had cylinder head maintenance performed by a repair facility other than Teledyne Continental Motors after August 1, 1994.

Whether AD 98-24089 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 98-24089 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.