Airworthiness Directive 2005-15-15

one-time
Official AD 2005-15-15 · FR doc 05-14685 · 2005-07-28 · airframe

Airworthiness Directives; Boeing Model 757-200, -200PF, and -200CB Series Airplanes Equipped With Pratt & Whitney or Rolls-Royce Engines

What this AD requires

The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 757-200, -200PF, and -200CB series airplanes. This AD requires inspecting to determine the part number of the upper link forward fuse pins of the engine struts and replacing the fuse pins as necessary. This AD is prompted by a report indicating that, due to an incorrect listing in the illustrated parts catalog, persons performing maintenance on the engine strut(s) could have installed an incorrect upper link forward fuse pin. We are issuing this AD to prevent a ruptured wing box, due to the engine not separating safely during certain emergency landing conditions, which could lead to a fuel spill and consequent fire.

Which aircraft AD 2005-15-15 applies to

MakesBoeing
Models757-200, 757-200PF, 757-200CB, 757
Serial-conditional — narrows to serials 1–735.
Part-conditional311N5501-2.

Applies to airplanes with line numbers 1 through 735 inclusive, certificated in any category, equipped with Pratt & Whitney or Rolls-Royce engines. Concerns possible installation of an incorrect engine strut upper link forward fuse pin, P/N 311N5501-2, due to an error in the illustrated parts catalog.

Whether AD 2005-15-15 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 2005-15-15 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.