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Yes. When exhaust stacks are removed for AD 2000-01-16 inspections or replacement, adjacent exhaust joints and hardware are often disturbed. On turbocharged models, this may include V-band clamps and couplings at the turbocharger inlet or tailpipe connections, along with gaskets, heat shields, and firesleeve, to ensure proper sealing and fire protection during reassembly. Browse the McFarlane website for those replacement components.
Yes. These FAA-PMA stack assemblies may be installed as direct replacements for OEM stacks removed during inspections and corrective actions required by AD 2000-01-16.
Refer to AC91-59A or Nicrocraft Exhaust system checklist. The American Bonanza society puts out a good video by Bob Ripley on Beechcraft exhaust inspection that is applicable to most types of aircraft.
Refer to STC Paperwork. Should specify if original muffler can fit, or a different style –possibly even for a different brand of Aircraft could be used.
FAA-PMA approved for Cessna 310P/Q/R, 320D/E/F, 340/340A, 401/401A/B, 402/402A/B/C, 404, and 414/414A.
Stainless steel provides improved resistance to high-temperature fatigue, corrosion, and cracking compared to legacy materials, extending service life in turbocharged exhaust environments.
12 month warranty, unlimited hours. Please contact our sales team for further instructions.
8130-3 and the warranty card.
AD 2000-01-16 addresses cracking, corrosion, and exhaust leakage that can lead to in-flight fire risk. Stacks are commonly removed due to wall thinning, heat damage, and slip-joint wear.