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Final rule 2026-16655

Airworthiness Directives; Pratt & Whitney Canada Corp. Engines

The FAA is superseding Airworthiness Directive (AD) 2026-13- 09, which applied to all Pratt & Whitney Canada Corp. (P&WC) Model PW210A, PW210A1, and PW210S engines. AD 2026-13-09 required repetitive visual inspections of the turbine exhaust frame for cracks and, depending on the results of the inspections, replacement of the turbine exhaust frame. Since the FAA issued AD 2026-13-09, a manufacturer's analysis revealed that turbine exhaust frames manufactured from a certain material were less durable and more susceptible to developing cracks under thermal stress. This AD requires repetitive visual inspections of the turbine exhaust frame for cracks at different initial inspection thresholds than required by AD 2026-13-09 based on the material used during manufacture and, depending on the results of the inspections, replacement of the turbine exhaust frame. 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
2026-16655
Published
Aug 14, 2026
Effective
Aug 31, 2026
Comments close
Sep 28, 2026 (open)
Federal Register citation
91 FR 52487

Docket identifiers

  • Docket No. FAA-2026-7238
  • Project Identifier MCAI-2026-00764-E
  • Amendment 39-23443
  • AD 2026-16-13

CFR references

  • Title 14, part 39