Rule 4 Aug 2025 safety standards, regulations, aviation, faa, aircraft, aviation safety, reporting and recordkeeping requirements, aircraft engines, composites

✈️FAA Issues Special Conditions for LEAP-1B Engine Compliance

This action amends Special Condition No. 33-017-SC for the CFM International (CFM) Model LEAP-1B engines. These engines have a novel or unusual design feature associated with the engine fan blades-- incorporation of woven composite fan blades. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions, as amended, contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.

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Rule 4 Mar 2025 incorporation by reference, safety, faa, aircraft engines, airworthiness directives, air transportation, regulatory compliance, aviation safety, aviation, aircraft, maintenance

✈️Airworthiness Directives for CFM Engines

The FAA is adopting a new airworthiness directive (AD) for certain CFM International, S.A. (CFM) Model LEAP-1A, LEAP-1B, and LEAP- 1C engines. This AD was prompted by a manufacturer investigation that revealed a quality escape for low-pressure turbine (LPT) disks made from forgings with nonconforming grain size. This AD requires removal and replacement of the LPT stage 4 and stage 5 disks. The FAA is issuing this AD to address the unsafe condition on these products.

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Regulatory Requirements, Financial Impact, Aviation Safety 30 Jan 2025 compliance, faa, safety, aircraft, aviation safety, incorporation by reference, air transportation, airworthiness directive, general electric, aircraft engines

✈️New FAA Airworthiness Directive for GE CF6-80E1A2 and A3 Engines

The FAA proposes to adopt a new airworthiness directive (AD) for certain General Electric Company (GE) Model CF6-80E1A2, CF6-80E1A3, CF6-80E1A4, and CF6-80E1A4/B engines. This proposed AD was prompted by a manufacturer investigation that revealed certain high-pressure turbine (HPT) stage 1 and HPT stage 2 disks were manufactured from powder metal material suspected to contain iron inclusion. This proposed AD would require replacement of affected HPT stage 1 and HPT stage 2 disks with parts eligible for installation. The FAA is proposing this AD to address the unsafe condition on these products.

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