Is AD 2016-19-09 a recurring Airworthiness Directive?

No — AD 2016-19-09 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2016-19-09 apply to?

AD 2016-19-09 applies to General Electric Company — models GE90-76B, GE90-77B, GE90-85B, GE90-90B, GE90-94B, GE90. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2016-19-09

one-time

Official AD 2016-19-09 · FR doc 2016-23740 · 2016-09-30 · turbine engine

Airworthiness Directives; General Electric Company Turbofan Engines

What this AD requires

We are adopting a new airworthiness directive (AD) for all General Electric Company (GE) GE90-76B, GE90-77B, GE90-85B, GE90-90B, and GE90-94B turbofan engines with high-pressure compressor (HPC) stage 8-10 spool, part numbers (P/Ns) 1694M80G04, 1844M90G01, or 1844M90G02, installed. This AD was prompted by reports of cracks found on the seal teeth of the HPC stage 8-10 spool. This AD requires eddy current inspections (ECIs) or fluorescent penetrant inspections (FPIs) of the HPC stage 8-10 spool seal teeth and removing from service those parts that fail inspection. We are issuing this AD to prevent failure of the HPC stage 8-10 spool, uncontained rotor release, damage to the engine, and damage to the airplane.

Which aircraft AD 2016-19-09 applies to

MakesGeneral Electric Company

ModelsGE90-76B, GE90-77B, GE90-85B, GE90-90B, GE90-94B, GE90

Part-conditional — 1694M80G04, 1844M90G01, 1844M90G02.

Applies only to engines with a high-pressure compressor (HPC) stage 8-10 spool, P/N 1694M80G04, 1844M90G01, or 1844M90G02, installed.

Whether AD 2016-19-09 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 2016-19-09 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.