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WC9910295-14 RH_Twin_Cessna_Stack_Nicrocraft_Twin_Stack_Assemblies
Part Number WC9910295-14

WC9910295-14, STACK ASSEMBLY

Part # WC9910295-14

STACK ASSEMBLY


$1,325.00 Retail Price: $1,656.25
In Stock

Get everything you need

CLAMP, V-band

490127-0001

CLAMP, V-band

$828.52 / was $1,035.65

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STACK ASSEMBLY, RH, SS, Cessna, 3pc part

$1,431.78 / was $1,789.72

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STACK ASSY, Inconel, RH,

$3,728.33 / was $4,660.42

Expected ship date is 11-26-2026.
EXHAUST LUBE, 4.0 oz

$39.03 / was $48.03

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STACK ASSEMBLY

WC9910295-13

STACK ASSEMBLY

$1,325.00 / was $1,656.25

In Stock

Product Details

Specifications

Approval
Condition
New
Manufacturer
Wall Colmonoy
Dimensions
L: 24 x W: 12 x H: 24 in
Weight
5 lbs
Unit of Measure
Each
McFarlane Part Number
WC9910295-14

Product Description

Twin Cessna Exhaust Stack Assemblies

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 approved WC9910295-13 (LH) and WC9910295-14 (RH)
  • Stainless steel construction
  • High-temperature durability and corrosion resistance
  • Direct replacement for stacks removed during AD 2000-01-16 inspections and overhauls
  • Reduces downtime compared to OEM repair or limited overhaul availability

Nicrocraft Exhaust Components

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.

  • Carefully designed for longer service life and proper alignment
  • All factory-new parts are heat-resistant 321 stainless steel construction
  • Bellows are made of Inconel alloy for superior heat resistance
  • Most components are in stock and ready to ship today!

WARNING: Cancer and/or Reproductive Harm - California Proposition 65 Resources

Eligible Aircraft
Make Model Start S/N End S/N Eligibility Chart
Cessna T310PT310PS/N 310P0001 – 310P0240310P0240Eligibility Chart 1482
Cessna T310QT310QS/N 310Q0001 – 310Q1160310Q1160Eligibility Chart 1482
Cessna T310RT310RS/N 310R0001 – 310R2140310R2140Eligibility Chart 1482
Cessna 320D320DS/N 320D0001 – 320D0130320D0130Eligibility Chart 1482
Cessna 320E320ES/N 320E0001 – 320E0110320E0110Eligibility Chart 1482
Cessna 320F320FS/N 320F0001 – 320F0045320F0045Eligibility Chart 1482
Cessna 340340S/N 340-0001 – 340-0555340-0555Eligibility Chart 1482
Cessna 340A340AS/N 340A0001 – 340A1817340A1817Eligibility Chart 1482
Cessna 401401S/N 401-0001 – 401-0322401-0322Eligibility Chart 1482
Cessna 401A401AS/N 401A0001 – 401A0132401A0132Eligibility Chart 1482
Cessna 401B401BS/N 401B0001 – 401B0221401B0221Eligibility Chart 1482
Cessna 402402S/N 402-0001 – 402-0322402-0322Eligibility Chart 1482
Cessna 402A402AS/N 402A0001 – 402A0129402A0129Eligibility Chart 1482
Cessna 402B402BS/N 402B0001 – 402B1384402B1384Eligibility Chart 1482
Cessna 402C402CS/N 402C0001 – 402C1020402C1020Eligibility Chart 1482
Cessna 404404S/N 404-0001 – 404-0859404-0859Eligibility Chart 1482
Cessna 414414S/N 414-0001 – 414-0965414-0965Eligibility Chart 1482
Cessna 414A414AS/N 414A0001 – 414A1212414A1212Eligibility Chart 1482
FAQs

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.

Documents

FAA Airworthiness Directives (AD)

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