Airworthiness Directive 2018-22-05
one-timeAirworthiness Directives; Engine Alliance Turbofan Engines
What this AD requires
We are adopting a new airworthiness directive (AD) for all Engine Alliance (EA) GP7270, GP7272, and GP7277 turbofan engines with a certain high-pressure turbine (HPT) case installed. This AD requires removal of affected HPT stator cases (HPT cases) from service and their replacement with a part eligible for installation. This AD was prompted by the discovery of a quality escape at a manufacturing facility involving unapproved welds on HPT cases. We are issuing this AD to address the unsafe condition on these products.
Which aircraft AD 2018-22-05 applies to
Applies only to engines with HPT stator case P/N 2060M40G02 or 2137M29G01 installed, with an HPT case serial number listed in EA ASB EAGP7-A72-401 (dated August 23, 2018) Table 1 or EA SB EAGP7-72-399 (dated June 4, 2018) Table 1 (specific serial numbers not included in provided applicability text).
Whether AD 2018-22-05 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:
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.