SDR 99ZZZX579

Service difficulty report · Bolt · Beech 200BEECH

Difficulty date
January 1, 1998
Submitted
March 26, 2000
Operation
General aviation
Aircraft
N15NG
Make and model
Beech 200BEECH
Aircraft serial
BB666
Part
Bolt
Condition
Cracked
Location
Wing
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

8727 AACT 20,988 TL. FIRST FIVE YEAR WING BOLT INSPECTION AFTER REPLACEMENT. THE LEFT AND RIGHT LOWER FORWARD WING (INCONEL) BOLTS WERE FOUND CRACKED USING DIE PENETRANT. ONE BOLT WAS VERIFIED TO BE CRACKED USING A MICROSCOPE. ONE BOLT WAS VERIFIED TO BE CRACKED USING DIE A MICROSCOPE. ONE UPPER FORWARD STEEL BOLT WAS SUSPECTED TO BE CRACKED USING DIE PEN. INCONEL BOLT TIME IN SERVICE 5 YEARS. 1,882 HOURS, 3,418 CYCLES.