Is AD 04-24630 a recurring Airworthiness Directive?

No — AD 04-24630 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 04-24630 apply to?

AD 04-24630 applies to Raytheon — models B100. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 04-24630

one-time

AD 04-24630 · 2004-11-09 · airframe

Airworthiness Directives; Raytheon Aircraft Company Model B100 Airplanes

What this AD requires

The FAA adopts a new airworthiness directive (AD) for certain Raytheon Aircraft Company (Raytheon) Model B100 airplanes. This AD requires you to drill holes in the hot lip tube "B" nuts, tighten the "B" nuts to specified torque ranges, and secure the "B" nuts with safety wire. This AD is the result of reports of loose "B" nuts on the engine inlet that may loosen and permit a leak in the engine inlet anti-ice system. We are issuing this AD to detect and correct loose "B" nuts on the engine inlet, which could result in failure of the engine inlet anti-ice system and consequent ice buildup. This failure and ice buildup could lead to an engine's ingestion of ice with loss of engine power or loss of engine.

Which aircraft AD 04-24630 applies to

MakesRaytheon

ModelsB100

certain

Whether AD 04-24630 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 04-24630 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.