Airworthiness Directives; General Electric Company Engines, and Various Restricted Category Rotorcraft
airworthiness · Rule · Final rule; request for comments. · Published 2024-03-15 · Effective 2024-04-01 · 89 FR 18771
Document
Document number
2024-05547
Federal Register citation
89 FR 18771
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
General Electric Company
Publication date
2024-03-15
Effective date
2024-04-01
FAA docket
Docket No. FAA-2024-0465
Abstract
The FAA is adopting a new airworthiness directive (AD) for certain General Electric Company (GE) Model CT7-2E1, CT7-2F1, CT7-8A, CT7-8E, CT7-8F5 engines, and various restricted category helicopters with GE Model T700-GE-700,-701A, -701C, -701D/CC, -701D, -401, -401C, CT7-2D or CT7-2D1 engines installed. This AD was prompted by at least four reports of failures of the torque reference tube magnetic insert braze joint of the power turbine drive shaft assembly within the last several months. This AD requires a phase array ultrasonic inspection of the torque reference tube magnetic insert braze joint of the power turbine drive shaft assembly for inadequate braze coverage, and repair or replacement of the power turbine drive shaft assembly if necessary. The FAA previously sent an emergency AD to all known U.S. owners and operators of these engines and helicopters and is now issuing this AD to address the unsafe condition on these products.