Is AD 05-14174 a recurring Airworthiness Directive?

No — AD 05-14174 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 05-14174 apply to?

AD 05-14174 applies to Boeing — models 747-200F. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 05-14174

one-time

AD 05-14174 · 2005-07-22 · airframe

Airworthiness Directives; Boeing Model 747-200C and 747-200F Series Airplanes

What this AD requires

The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 747-200C and 747-200F series airplanes. This AD requires one-time inspections for cracks and material loss in the fuselage skin above the stringer (STR) 23 lap splice, between Body Station (BS) 282 and BS 298, and repair if necessary. This AD is prompted by a report of a crack above the STR 23 lap splice on one airplane. We are issuing this AD to detect and correct cracks or material loss in the fuselage skin, and consequent reduced structural integrity of the skin panel, which could result in rapid depressurization of the airplane.

Which aircraft AD 05-14174 applies to

MakesBoeing

Models747-200F

certain

Whether AD 05-14174 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 05-14174 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.