SDR 99ZZZX3578

Service difficulty report · Mount · Beech E55

Difficulty date
September 2, 1999
Submitted
March 26, 2000
Operation
General aviation
Make and model
Beech E55
Part
Mount
Part number
TH472
Condition
Cracked
Location
Engine
Stage of operation
IN
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

ENGINE MOUNT WAS RECEIVED FOR COMPLIANCE TO AD 91-15-20. DURING MAGNETIC PARTICAL INSPECTION, AN INDICATION APPEARED AT UPPER RT DYNA FOCAL ATTACH AREA WHERE REINFORCEMENT STRAP IS WELDED TO PLATE. THE INDICATION WAS APPROXIMATELY 1.50 INCHES IN LENGTH, AREA WAS LIKELY NOT COMPLETELY WELDED. THE WELD WAS GROUND OUT AND RE-WELDED, THEN RE-MAG/PARTICAL INSPECTED. NOTE: SUBMITTER STATED THIS AREA IS NOT CALLED OUT IN AD 91-15-20.

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