Airworthiness Directive 2017-14-07
one-timeAirworthiness 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) V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5, and V2531-E5 turbofan engines. This AD was prompted following a self- disclosure by IAE regarding manufacturing quality escapes. This AD requires replacing the affected and suspect parts within the time limits specified in the compliance section. We are issuing this AD to address the unsafe condition on these products.
Which aircraft AD 2017-14-07 applies to
Applies to engines with one or more of the following installed: HPT stage 2 air seal, P/N 2A4157, with an S/N listed in Table 1 of IAE NMSB V2500-ENG-72-0676, dated October 14, 2016; HPT 1st stage air seal, P/N 2A3423, with an S/N listed in Table 1 of IAE NMSB V2500-ENG-72-0677, Revision 1, dated January 11, 2017, or IAE NMSB V2500-ENG-72-0678, Revision 1, dated January 5, 2017; or HPT stage 2 ring plate, P/N 2A3437, with an S/N listed in Table 1 of IAE NMSB V2500-ENG-72-0682, dated December 2, 2016, or IAE NMSB V2500-ENG-72-0681, Revision 2, dated January 9, 2017.
Whether AD 2017-14-07 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.