Is AD 2005-17-19 a recurring Airworthiness Directive?

No — AD 2005-17-19 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2005-17-19 apply to?

AD 2005-17-19 applies to Cirrus — models SR20, SR22. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2005-17-19

one-time

Official AD 2005-17-19 · FR doc 05-16980 · 2005-09-01 · airframe

Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes

What this AD requires

The FAA adopts a new airworthiness directive (AD) for certain Cirrus Design Corporation (CDC) Models SR20 and SR22 airplanes. This AD requires you to measure and adjust the crew seat break-over bolts and to replace the crew seat recline locks on both crew seats. This AD results from CDC discovering that the crew seats, under emergency landing dynamic loads, may fold forward at less than the 26 g required by the regulations. 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 2005-17-19 applies to

MakesCirrus

ModelsSR20, SR22

Whether AD 2005-17-19 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 2005-17-19 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.