Service difficulty report · Bracket · Diamon DA20C1

Difficulty date
February 16, 2006
Submitted
June 6, 2006
Operation
General aviation
Make and model
Diamon DA20C1
Aircraft time
1,529 hours
Engine
Cont IO240B
Part
Bracket
Part number
2224121400
Condition
Cracked
Location
Alternator
Part time
550 hours
Stage of operation
IN
How discovered
9
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

DURING ROUTINE INSPECTION, A SMALL CRACK WAS DISCOVERED ON THE ALTERNATOR BRACKET. FURTHER INSPECTION REVEALED THAT THE TOP NUT TCM P/N 2443 WHICH IS USED TO MOUNT THE BRACKET TO THE ENGINE WAS STRIPPED. THE NUT ATTACHES TO ONE OF THE ENGINE THRU STUDS AT THE FORWARD MAIN BEARING. LUCKILY THE STUD WAS NOT DAMAGED AND A NEW BRACKET AND NUT WERE INSTALLED AND TQ`D. IT WAS ALSO NOTED THAT ALT BRACKET MOUNTING HOLES ARE LARGER THAN THE STUDS AND BOLT USED TO SECURE THE BRACKET TO ENG. THESE WERE TAUGHT AT FIRST TO BE ELONGATED BUT THE NEW BRACKET SUPPLIED BY THE MANUFACTURE REVEALED THEY WERE MANUFACTURED THIS WAY. A REQUEST WAS SENT TO THE MANUFACTURE FOR EXPLANATION.

More about the Diamon DA20-C1