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Airworthiness Directive 2026-06532

recurring
AD 2026-06532 · 2026-04-03 · airframe

Airworthiness Directives; Costruzioni Aeronautiche Tecnam S.P.A. Airplanes

What this AD requires

The FAA is adopting a new airworthiness directive (AD) for certain Costruzioni Aeronautiche Tecnam S.P.A. (Tecnam) Model P2010 airplanes. This AD was prompted by a report of unrecoverable loss of engine power. This AD requires repetitive detailed borescope inspections (BSIs) of the exhaust muffler flame tube and, depending on the results, repair of the exhaust muffler flame tube. This AD includes an optional terminating action for the inspection and repair requirements. The FAA is issuing this AD to address the unsafe condition on these products.

Repetitive inspection. Re-inspect every 200 hours. The next-due date/hours depend on this aircraft’s time in service — a records report computes it from the logbooks.

Which aircraft AD 2026-06532 applies to

MakesCostruzioni Aeronautiche Tecnam S.P.A.
ModelsP2010
Serial-conditional — narrows to serials ?–335.
Part-conditional — MOD2010/078.

Applies up to and including serial number 335, and only to airplanes equipped with a Lycoming IO-390 engine (MOD2010/078).

Whether AD 2026-06532 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 2026-06532 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.