Overview
| PN 33401 This universal stainless steel exhaust system is designed for experimental aircraft using Continental A65 thru O-200 engines.Consists of 2 manifolds, left hand manifold has heat shroud with 2-1/2 connection for carb heat.Muffler outlet are 3 long. Tailpipe extensions may be required, sold separately PN 33402 8 Tailpipe Extensions.Furnished with slip joint and pin clamp. THIS SYSTEM IS PATTERNED AFTER A CESSNA 150 SYSTEM,BUT WILL NOT FIT A CESSNA 150 OR 152. |
WARNING: Cancer and Reproductive Harm – www.P65Warnings.ca.gov.
