Airworthiness Directive 2004-19-04

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Official AD 2004-19-04 · FR doc 04-21912 · 2004-09-30 · turbine engine

Airworthiness Directives; Rolls-Royce plc RB211-22B, RB211-524, and RB211-535 Series Turbofan Engines

What this AD requires

This document makes a correction to Airworthiness Directive (AD) 2004-19-04. That AD applies to Rolls-Royce plc (RR) RB211-22B, RB211-524, and RB211-535 series turbofan engines. That AD was published in the Federal Register on September 22, 2004 (69 FR 56683). In the amendatory language, under Sec. 39.13 [Amended], the amendment number for the AD was inadvertently omitted. This document corrects that omission. In all other respects, the original document remains the same.

Which aircraft AD 2004-19-04 applies to

MakesRolls-Royce Plc Rb211-22B, Rb211-524, And Rb211-535

Whether AD 2004-19-04 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 2004-19-04 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.