Is AD 2006-19-10 a recurring Airworthiness Directive?

No — AD 2006-19-10 is a one-time directive. Verify it was complied with in the aircraft's records.

Airworthiness Directive 2006-19-10

Q: Which aircraft does AD 2006-19-10 apply to?

Applicability depends on the aircraft's type certificate; check it against the specific tail.

one-time

Official AD 2006-19-10 · FR doc E6-15432 · 2006-09-19 · airframe

Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes

What this AD requires

We are adopting a new airworthiness directive (AD) that supersedes AD 2005-17-19, which applies to certain Cirrus Design Corporation (CDC) Models SR20 and SR22 airplanes. AD 2005-17-19 currently requires you to measure and adjust the crew seat break-over bolts and to replace the crew seat recline locks on both crew seats. Since we issued AD 2005-17-19, CDC developed new crew seat break-over pins to replace the old crew seat break-over bolts. Consequently, this AD retains the action from AD 2005-17-19 of replacing the crew seat recline locks on both seats and adds the action of replacing the crew seat break-over bolts with the new crew seat break-over pins on both seats. We are issuing this AD to prevent the crew seats from folding forward during emergency landing dynamic loads with consequent occupant injury.

Which aircraft AD 2006-19-10 applies to

Applicability depends on the aircraft’s type certificate — check it against the specific tail.

Whether AD 2006-19-10 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 2006-19-10 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.