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Part # WC9910295-14
FAA-PMA Approved for 9910295-13 and 9910295-14 Stacks
Address AD 2000-01-16 with these replacement stack assemblies from Nicrocraft. Designed to address cracking, corrosion, and exhaust leakage concerns in aging OEM stacks.
FAA-PMA/STC approved individual exhaust components and complete systems for most single and twin-engine aircraft, including Cessna, Piper, Beech, Bellanca, Grumman, Mooney, and Rockwell.
WARNING: Cancer and/or Reproductive Harm - California Proposition 65 Resources
| Make | Model | Start S/N | End S/N | Eligibility Chart |
|---|---|---|---|---|
| Cessna T310P | T310P | S/N 310P0001 – 310P0240 | 310P0240 | Eligibility Chart 1482 |
| Cessna T310Q | T310Q | S/N 310Q0001 – 310Q1160 | 310Q1160 | Eligibility Chart 1482 |
| Cessna T310R | T310R | S/N 310R0001 – 310R2140 | 310R2140 | Eligibility Chart 1482 |
| Cessna 320D | 320D | S/N 320D0001 – 320D0130 | 320D0130 | Eligibility Chart 1482 |
| Cessna 320E | 320E | S/N 320E0001 – 320E0110 | 320E0110 | Eligibility Chart 1482 |
| Cessna 320F | 320F | S/N 320F0001 – 320F0045 | 320F0045 | Eligibility Chart 1482 |
| Cessna 340 | 340 | S/N 340-0001 – 340-0555 | 340-0555 | Eligibility Chart 1482 |
| Cessna 340A | 340A | S/N 340A0001 – 340A1817 | 340A1817 | Eligibility Chart 1482 |
| Cessna 401 | 401 | S/N 401-0001 – 401-0322 | 401-0322 | Eligibility Chart 1482 |
| Cessna 401A | 401A | S/N 401A0001 – 401A0132 | 401A0132 | Eligibility Chart 1482 |
| Cessna 401B | 401B | S/N 401B0001 – 401B0221 | 401B0221 | Eligibility Chart 1482 |
| Cessna 402 | 402 | S/N 402-0001 – 402-0322 | 402-0322 | Eligibility Chart 1482 |
| Cessna 402A | 402A | S/N 402A0001 – 402A0129 | 402A0129 | Eligibility Chart 1482 |
| Cessna 402B | 402B | S/N 402B0001 – 402B1384 | 402B1384 | Eligibility Chart 1482 |
| Cessna 402C | 402C | S/N 402C0001 – 402C1020 | 402C1020 | Eligibility Chart 1482 |
| Cessna 404 | 404 | S/N 404-0001 – 404-0859 | 404-0859 | Eligibility Chart 1482 |
| Cessna 414 | 414 | S/N 414-0001 – 414-0965 | 414-0965 | Eligibility Chart 1482 |
| Cessna 414A | 414A | S/N 414A0001 – 414A1212 | 414A1212 | Eligibility Chart 1482 |
What aircraft are these exhaust stacks approved for?
FAA-PMA approved for Cessna 310P/Q/R, 320D/E/F, 340/340A, 401/401A/B, 402/402A/B/C, 404, and 414/414A.
Are these parts approved for AD 2000-01-16 compliance?
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.
Why are exhaust stacks frequently replaced on these aircraft?
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.
What is the benefit of stainless steel construction?
Stainless steel provides improved resistance to high-temperature fatigue, corrosion, and cracking compared to legacy materials, extending service life in turbocharged exhaust environments.
Are any other exhaust components commonly replaced when stacks are removed?
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.