FAA Adopts Fatigue Limits For Transport Aircraft

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Key Takeaways:

  • The FAA has adopted a new rule requiring aircraft manufacturers to set a "limit of validity" (LOV) for transport-category aircraft, defining the operational period before additional fatigue damage inspections are mandatory.
  • While not explicit "life limits," this rule may lead operators to retire older aircraft due to the time-consuming and costly approvals and maintenance schedules required to extend these limits.
  • The regulation aims to address "widespread fatigue damage" in aging aircraft, which involves numerous tiny cracks caused by repeated stress that together can impair structural integrity.
  • This rule applies to airliners weighing 75,000 pounds or more, as well as all future transport designs, impacting 4,198 U.S.-registered airplanes.
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A new rule adopted by the FAA this week stops short of requiring “life limits” for transport-category aircraft, but in practice that may be the result. The rule requires manufacturers to set a “limit of validity,” the number of flight cycles or hours that an airplane can operate before it must be subjected to additional inspections for fatigue damage. Once those limits are determined, the FAA must approve any extension of the limit. Operators may choose to retire older airplanes rather than submit to more time-consuming and costly approvals and maintenance schedules, according to the Dallas Morning News. Deadlines to set the limits vary from 18 months to five years away. “We’ve addressed the problem of aging aircraft with numerous targeted regulations and 100 airworthiness directives over the years,” said FAA Administrator Randy Babbitt. “This rule is a comprehensive solution to ensure the structural safety of today’s airliners and the airplanes of tomorrow.”

An airplane’s metallic structures are stressed and can develop cracks when they experience repeated loads such as the pressurization and depressurization that happens on every flight, the FAA said. While airlines regularly inspect aircraft for cracks exceeding a certain size, widespread fatigue damage is characterized by the development of numerous tiny cracks, none of which would have raised concerns individually but which together run the risk of joiningup and impairing the structural integrity of the aircraft. The new regulation applies to airliners with a takeoff weight of 75,000 pounds and heavier, as well as to all transport designs certificated in the future. The affected models total 4,198 U.S.-registered airplanes.

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