Is AD 95-06-02 a recurring Airworthiness Directive?

No — AD 95-06-02 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 95-06-02 apply to?

AD 95-06-02 applies to Boeing — models 747. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 95-06-02

one-time

Official AD 95-06-02 · FR doc 95-5781 · 1995-03-14 · airframe

Airworthiness Directives; Boeing Model 747 Series Airplanes, Excluding Airplanes Equipped With Pratt & Whitney PW4000 and General Electric CF6-80C2 Series Engines

What this AD requires

This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing Model 747 series airplanes, that requires replacement of certain fuse pins on the upper link of the inboard and outboard struts. This AD would also require inspections to detect corrosion or cracks of certain fuse pins, and replacement, if necessary. This amendment is prompted by reports of cracked or corroded fuse pins on the upper link of the inboard and outboard struts, which could result in fracturing of the pins. The actions specified by this AD are intended to prevent failure of the strut and separation of an engine from the airplane due to fracturing of the fuse pins.

Which aircraft AD 95-06-02 applies to

MakesBoeing

Models747

Serial-conditional — narrows to serials 1–967, 969–922.

Applies to Model 747 series airplanes by line number, excluding airplanes equipped with Pratt & Whitney PW4000 or General Electric CF6-80C2 series engines; certificated in any category. Does not require action on struts of airplanes with straight-bore fuse pins (PW4000/CF6-80C2-equipped) or 15-5 corrosion-resistant steel (third generation) fuse pins. Note: source text gives the second line-number range as '969 through 922,' which appears to be a transcription anomaly in the source document (to < from); reproduced as-is, not corrected.

Whether AD 95-06-02 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 95-06-02 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.