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Final rule 2026-16636

Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines

The FAA is adopting a new airworthiness directive (AD) for all Rolls-Royce Deutschland Ltd & Co KG (RRD) Model Trent 1000-A2, Trent 1000-AE2, Trent 1000-C2, Trent 1000-CE2, Trent 1000-D2, Trent 1000-E2, Trent 1000-G2, Trent 1000-H2, Trent 1000-J2, Trent 1000-K2, and Trent 1000-L2 engines. This AD was prompted by reports of cracking of the intermediate pressure (IP) compressor variable inlet guide vanes (VIGVs) due to high-cycle fatigue propagation. This AD requires repetitive borescope inspections (BSIs) for cracks of the IP compressor VIGVs and, depending on the inspection results, reduced inspection intervals for the repetitive BSIs or removal of the engine from service and replacement of the IP compressor VIGVs. The FAA is issuing this AD to address the unsafe condition on these products.

Source: FederalRegister.gov API v1Recently refreshed. Last successful refresh: 2026-08-15 08:49:02 UTC.

Source-supplied record

Document details

Document number
2026-16636
Published
Aug 14, 2026
Effective
Sep 18, 2026
Comments close
Not supplied
Federal Register citation
91 FR 52496

Docket identifiers

  • Docket No. FAA-2026-2294
  • Project Identifier MCAI-2025-00011-E
  • Amendment 39-23438
  • AD 2026-16-08

CFR references

  • Title 14, part 39