Is AD 2016-19-05 a recurring Airworthiness Directive?

No — AD 2016-19-05 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2016-19-05 apply to?

AD 2016-19-05 applies to International Aero Engines Ag — models V2500-A1, V2500. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2016-19-05

one-time

Official AD 2016-19-05 · FR doc 2016-22703 · 2016-09-22 · turbine engine

Airworthiness Directives; International Aero Engines AG Turbofan Engines

What this AD requires

We are adopting a new airworthiness directive (AD) for certain International Aero Engines AG (IAE) V2500-A1 turbofan engines. This AD was prompted by a report of an uncontainment caused by a high-pressure turbine (HPT) seal release. This AD requires removing the HPT No. 4 bearing front seal seat, part numbers (P/Ns) 2A0066, 2A1998, and 2A3432, and the HPT No. 4 bearing rear seal seat, P/Ns 2A0067, 2A1999, and 2A3433, and replacing them with parts eligible for installation. This AD also requires inspecting the HPT rotor and stator assembly, and, if necessary, their replacement with parts that are eligible for installation. We are issuing this AD to prevent failure of the HPT stage 2 seals, uncontained HPT seal release, damage to the engine, and damage to the airplane.

Which aircraft AD 2016-19-05 applies to

MakesInternational Aero Engines Ag

ModelsV2500-A1, V2500

Applies only to engines with serial numbers listed under Planning Information, Effectivity Data in IAE Non-Modification Service Bulletin (NMSB) V2500-ENG-72-0670, dated March 14, 2016.

Whether AD 2016-19-05 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 2016-19-05 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.