Airworthiness Directive E6-21122

one-time
AD E6-21122 · 2006-12-12 · turbine engine

Airworthiness Directives; Rolls-Royce plc RB211-524 Series Turbofan Engines; Correction

What this AD requires

This document makes a correction to airworthiness directive (AD) 2004-26-05 applicable to certain Rolls-Royce plc (RR) RB211-524 series turbofan engines that was published in the Federal Register on January 5, 2005. The part number UL29916 in the Applicability section is incorrect. This document corrects that part number. In all other respects, the original document remains the same.

Which aircraft AD E6-21122 applies to

MakesRolls-Royce Plc Rb211-524

certain

Whether AD E6-21122 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 E6-21122 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.