Airworthiness Directive 2001-02-07

one-time
Official AD 2001-02-07 · FR doc 01-1947 · 2001-01-29 · airframe

Airworthiness Directives; Boeing Model 767 Series Airplanes Powered by Pratt & Whitney Engines

What this AD requires

This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing Model 767 series airplanes powered by Pratt & Whitney engines, that requires modification of the nacelle strut and wing structure. The actions specified by this AD are intended to prevent fatigue cracking in primary strut structure and consequent reduced structural integrity of the strut.

Which aircraft AD 2001-02-07 applies to

MakesBoeing
Models767

Requires modification of nacelle strut and wing structure per Boeing Service Bulletin 767-54-0080 at a flight-cycle threshold or within 20 years since date of manufacture, whichever occurs first, plus prior/concurrent accomplishment of related Boeing service bulletins (767-54-0069, 767-54-0083, 767-54-0088, 767-54A0094, 767-57-0053, 767-29-0057); terminates repetitive inspections required by AD 94-11-02 and AD 99-07-06. Specific 767 series/variant not stated in the extracted applicability text.

Whether AD 2001-02-07 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 complianceThe specific action taken (inspected, replaced, modified) and to what revision.
DateWhen the work was done.
Aircraft timeTotal time in service / tach at compliance — how recurring next-due is computed.
Signature & certificateThe A&P/IA who returned it to service, with certificate number.
Is AD 2001-02-07 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 →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.