TailplateTailplate
Run a report

Airworthiness Directive E7-19610

one-time
AD E7-19610 · 2007-10-04 · turbine engine

Airworthiness Directives; Rolls-Royce plc RB211 Trent 500 Series Turbofan Engines; Correction

What this AD requires

The FAA is correcting airworthiness directive (AD) 2007-19-10. That AD applies to Rolls-Royce plc RB211 Trent 500 series turbofan engines. We published that AD in the Federal Register on September 18, 2007 (72 FR 53108). The compliance limit of 2,190 cycles-since-new is incorrect in two places. This document corrects that compliance limit to 2,910 cycles-since-new. In all other respects, the original document remains the same.

Which aircraft AD E7-19610 applies to

MakesRolls-Royce Plc Rb211 Trent 500

Whether AD E7-19610 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 E7-19610 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.