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Turbocharger V-Band Clamp AD Proposed

Gemini Sparkle

Key Takeaways:

  • The FAA has proposed a new airworthiness directive (AD) requiring annual inspections and a 500-hour life limit for specific v-band couplings on turbocharged engine exhaust systems to prevent in-flight fires and loss of control.
  • A separate, effective FAA AD mandates urgent inspection or replacement of certain new-manufacture Bendix S-1200 magnetos due to improper lubrication during assembly, which could lead to component failure.
  • President Biden has nominated Phillip Washington, CEO of Denver International Airport, to serve as the new FAA Administrator.
  • Congress is examining regulatory obstacles for the approval of unleaded aviation fuel alternatives, with the FAA committing to a 2030 deadline for their introduction.
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On July 27, 2022, the FAA proposed a new airworthiness directive (AD) that would require repetitive inspections of turbocharged, reciprocating engine-powered airplanes and helicopters, and turbocharged, reciprocating engines with “spot-welded, multi-segment v-band couplings at the tailpipe to the turbocharger exhaust housing flange.” Under the proposed AD, the clamps/couplings would be inspected annually, regardless of their accumulated time-in-service (TIS) and a life limit for the components would be established by removing them from service every 500 hours TIS. Since it is a proposed AD, not final, the FAA is requesting comments from the public by November 4, 2022.

New-manufacture Bendix S-1200 magnetos, like the one pictured above, are the subject of another airworthiness directive (AD 2022-16-03), effective August 15, 2022. The components were produced without a specific grease being applied to internal bearings, which may lead to failure.

According to the preamble in the notice of proposed rulemaking (NPRM), the NTSB has made seven recommendations regarding the components since 1974. Additionally, there are 10 ADs already on the books, plus an additional 11 special airworthiness information bulletins (SAIBs) addressing the components as installed on various turbocharged piston engines, whether installed at the time of production, under a supplemental type certificate (STC) or other means. The FAA said, “In spite of these efforts, failures continue to occur and the number of significant safety events continues to increase.”

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