Service difficulty report · Clamp · Stolac UC1

Difficulty date
February 25, 2005
Submitted
May 5, 2005
Operation
General aviation
Aircraft
N65NE
Make and model
Stolac UC1
Aircraft serial
023
Engine
Lyc IO360A1A
Part
Clamp
Condition
Cracked
Location
Tailpipe
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

LT ENGINE IB EXHAUST TAILPIPE CRACKED, EXPELLING HEAT INTO ENGINE COMPARTMENT, BURNING PAINT ON COWLING. PART FAILURE OCCURRED BECAUSE OF BROKEN SUPPORT CLAMP, NO PN AVAILABLE DUE TO THE LIMITED PRODUCTION OF THIS AIRCRAFT ON EITHER EXHAUST TAILPIPE OR SUPPORT CLAMP. SUSPECTED CAUSE OF FAILURE IS FROM ENGINE VIBRATION AND SHOCK LOADS IMPOSED BY WATER OPERATIONS. ENTIRE EXHAUST SYSTEM SHOULD BE INSPECTED AT EACH 50, 100 HOUR AND ANNUAL INSPECTION SPECIFICALLY THE REAR SUPPORT CLAMPS FOR CRACKS AND DETERIORATION. (K)