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.
Unit
PR
Hazardous
No
Oversize
No
Weight
0.680 kg
Alternative P/N
33402
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