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Airworthiness Directive 00-21314

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AD 00-21314 · 2000-08-23 · turbine engine

Airworthiness Directives; Rolls-Royce plc. RB211 Trent 768-60, Trent 772-60, and Trent 772B-60 Turbofan Engines; Correction

What this AD requires

This document makes a correction to Airworthiness Directive (AD) 2000-13-05 applicable to Rolls-Royce plc. (RR) RB211 Trent 768-60, Trent 772-60, and Trent 772B-60 turbofan engines that was published in the Federal Register on July 3, 2000 (65 FR 40983). The statement regarding the reports of fan blade failures in the Summary section and the Internet address for AD comments in the Addresses section are incorrect. This document corrects that statement and that address. In all other respects, the original document remains the same.

Which aircraft AD 00-21314 applies to

MakesRolls-Royce Plc. Rb211 Trent 768-60, Trent 772-60, And Trent 772B-60 Turbofan

Whether AD 00-21314 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 00-21314 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.