Is AD 2016-06-14 a recurring Airworthiness Directive?

No — AD 2016-06-14 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2016-06-14 apply to?

AD 2016-06-14 applies to General Electric — models CF6-80E1. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2016-06-14

one-time

Official AD 2016-06-14 · FR doc 2016-07377 · 2016-04-04 · 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) CF6-80E1 turbofan engines with rotating compressor discharge pressure (CDP) seal, part number (P/N) 1669M73P02, installed. This AD was prompted by reports from the manufacturer of cracks in the teeth of two rotating CDP seals found during engine shop visits. This AD requires stripping of the coating, inspecting, and recoating the teeth of the affected rotating CDP seals. We are issuing this AD to prevent cracking of the CDP seal teeth, uncontained part release, damage to the engine, and damage to the airplane.

Which aircraft AD 2016-06-14 applies to

MakesGeneral Electric

ModelsCF6-80E1

Part-conditional — 1669M73P02.

Applies only to engines with rotating compressor discharge pressure (CDP) seal P/N 1669M73P02 installed.

Whether AD 2016-06-14 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 2016-06-14 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.