EXHAUST SYSTEM FOR CONTINENTAL 0-200

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.