Service difficulty report · Manifold · Cirrus SR22

Difficulty date
April 6, 2016
Submitted
April 6, 2016
Operation
General aviation
Filed by
YD5R855Y
Cirrus Design Corporation
Aircraft
N545WT
Make and model
Cirrus SR22
Aircraft serial
3422
Aircraft time
474 hours
Engine
Cont IO550N
Engine time
474 hours
Part
Manifold
Part number
SR221033
Part serial
UNREADABLE
Condition
Distorted
Location
Exhaust
Part time
474 hours
Stage of operation
IN
How discovered
V
Nature of condition
O
Precautionary procedure
K

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

DISTORTION AND BULGE IN LT EXHAUST MANIFOLD. THIS ACFT HAS AN ENGINE THAT WAS MODIFIED BY STC SE10589SC AND INSTALLED ON THE ACFT UNDER SA10588SC. THIS REPORT IS TO GIVE MY OPINION THAT THERE IS A POTENTIAL FOR FAILURE OF THIS EXHAUST ASSY AND THAT SI11-01 TO INSPECT AND LUBRICATE THE SLIP JOINTS ON THIS ASSY IS INSUFFICIENT TO DETECT AND PREVENT FAILURES. SI11-01 MAINLY ADDRESSES THE ABILITY OF THE SLIP JOINTS TO MOVE BY VISUALLY INSPECTING FOR SLIPPAGE SIGNS. IN THIS ACFT, THE SLIP JOINT NEXT TO THE DISTORTION EXHIBITS THE SIGNS OF MOVEMENT CALLED OUT IN SI11-01 AND CAN BE MOVED BY HAND WITH SOME RESISTANCE. THE DAMAGE OCCURRED ON THE BACK SIDE OF THE EXHAUST PIPE WHICH IS COMPLETELY HIDDEN BY A HEAT SHIELD. SI11-01 IS ONLY INSTRUCTING THE TECH TO VISUALLY INSPECT THE EXHAUST USING A FLASHLIGHT AND MIRROR, NOT TO REMOVE THE HEAT SHIELD. IF THE HEAT SHIELD IS NOT REMOVED, DAMAGE OF THIS TYPE WOULD REMAIN UNDISCOVERED. FAILURE OF THIS MANIFOLD WOULD ALLOW A SIGNIFICANT AMOUNT OF HIGH TEMPERATURE EXHAUST TO ENTER THE ENGINE COMPARTMENT. THIS CONDITION IS NOT UNUSUAL IN AIRCRAFT THAT HAVE BEEN MODIFIED BY THIS STC.

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