Airworthiness Directive 03-24374

one-time
AD 03-24374 · 2003-09-29 · turbine engine

Airworthiness Directives; Rolls-Royce plc RB211-524G2, -524G2-T, -524G3, -524G3-T, -524H, -524H-T, -524H2, and “524H2-T Series, and Models RB211 Trent 768-60, 772-60, and 772B-60 Turbofan Engines; Correction

What this AD requires

This document makes a correction to Airworthiness Directive (AD) 2003-14-23 applicable to Rolls-Royce plc RB211-524G2, -524G2-T, - 524G3, -524G3-T, -524H, -524H-T, -524H2, and "524H2-T Series, and Models RB211 Trent 768-60, 772-60, and 772B-60 turbofan engines that was published in the Federal Register on July 17, 2003. RB211 Trent 768-60, 772-60, and 772B-60 turbofan engine models were included in this AD in error. This document deletes these models from the AD. In all other respects, the original document remains the same.

Which aircraft AD 03-24374 applies to

MakesRolls-Royce
ModelsRB211-524G2, RB211-524G2-T, RB211-524G3, RB211-524G3-T, RB211-524H, RB211-524H-T, RB211-524H2, RB211-524H2-T, RB211
Part-conditionalFK25502, FW20195.

Applies only to RB211-524 series turbofan engines with high pressure compressor (HPC) rotor stage 1 through stage 6 drums part numbers FK25502 and FW20195 installed.

Whether AD 03-24374 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 03-24374 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.