airworthiness · Rule · Final rule. · Published 2026-04-24 · Effective 2026-05-29 · 91 FR 21945
Document
Document number
2026-08106
Federal Register citation
91 FR 21945
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Pratt & Whitney
Publication date
2026-04-24
Effective date
2026-05-29
FAA docket
Docket No. FAA-2025-0918
Abstract
The FAA is adopting a new airworthiness directive (AD) for certain Pratt & Whitney (PW) Model F117-PW-100, PW2037, PW2037D, PW2037M, PW2040, and PW2040D engines. This AD was prompted by an updated analysis of an event involving an International Aero Engines, LLC (IAE LLC) Model PW1127GA-JM engine, which experienced a high- pressure compressor (HPC) 7th-stage integrally bladed rotor (IBR-7) separation that resulted in an engine shutdown and aborted takeoff. This AD requires repetitive angled ultrasonic inspections (AUSIs) of certain high-pressure turbine (HPT) 1st-stage disks and turbine hubs for any crack indications, and if necessary, removal from service and replacement, and removal from service of certain HPT lenticular seal assemblies. The FAA is issuing this AD to address the unsafe condition on these products.