Service difficulty report · Manifold · Cirrus SR22

Difficulty date
March 30, 2016
Submitted
March 30, 2016
Operation
General aviation
Filed by
YD5R855Y
Cirrus Design Corporation
Aircraft
N215EM
Make and model
Cirrus SR22
Aircraft serial
2453
Aircraft time
1,308 hours
Engine
Cont IO550N
Engine time
1,308 hours
Propeller
Hartzl PHCJ3YF1
Part
Manifold
Part number
226850002
Condition
Failed
Location
Left Exhaust
Part time
718 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

SIGNIFICANT DISTORTION AND HEAT STRESS IN THE LT EXHAUST MANIFOLD BETWEEN CYLINDERS 2 AND 4. DAMAGE OF THIS TYPE IS FREQUENTLY FOUND IN THIS GENERAL AREA ON ENGINES MODIFIED WITH STC SE10589SC. WE HAVE ANOTHER SIMILARLY MODIFIED ACFT WITH SIMILAR DAMAGE IN THE SAME AREA. ANOTHER SDR FORTHCOMING ON IT. DAMAGE OF THIS TYPE IS COMPLETELY HIDDEN FROM CASUAL INSPECTION BECAUSE IT IS COVERED BY A CLOSE FITTING HEAT SHIELD. DISCOVERY REQUIRES REMOVAL OF COVERING HEAT SHIELD. VISIBLE MANIFOLD NORMALLY APPEARS UNDAMAGED. MANIFOLDS WITHOUT CRACKING AND BULGES FREQUENTLY EXHIBIT HEAT STRESS IN THIS AREA IN THE FORM OF A RIPPLED, TEXTURED SURFACE. TAT SI11-01 DATED 03/31/2011 ADDRESSES INSPECTION OF THE EXHAUST PIPES FOR THIS DAMAGE BUT IS POSSIBLY INADEQUATE TO DETECT THIS DAMAGE IN A TIMELY MANNER. THIS EXHAUST MANIFOLD WAS INSTALLED AT 589.8 TOTAL TIME. IT HAS 119.3 HOURS SINCE LAST ANNUAL INSPECTION. THE HEAT SHIELD IS PREVENTING COOLING AIRFLOW ACROSS THE EXHAUST MANIFOLD AND TRAPPING AND/OR REFLECTING HEAT BACK AT THE MANIFOLD CAUSING TEMPERATURES BEYOND WHAT THE METAL CAN WITHSTAND. PROBLEMS OF THIS TYPE EXIST FLEET WIDE IN ACFT MODIFIED WITH THIS STC.

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