Is AD 88-24-07 a recurring Airworthiness Directive?

No — AD 88-24-07 is a one-time directive. Verify it was complied with in the aircraft's records.

Airworthiness Directive 88-24-07

Q: Which aircraft does AD 88-24-07 apply to?

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

one-time

AD 88-24-07 · 1988-01-01 · turbine engine

Airworthiness Directives; cycles since new (CSN), but the N1 speed has been limited to 91 percent maximum, the tie rod restretch must be accomplished within

Which aircraft AD 88-24-07 applies to

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

Whether AD 88-24-07 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.

Supersession

Superseded by AD 97-24910 — comply with the superseding directive.

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 88-24-07 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 →

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.