Service difficulty report · Structure · Beech A200C

Difficulty date
November 1, 2011
Submitted
November 1, 2011
Operation
General aviation
Make and model
Beech A200C
Part
Structure
Condition
Cracked
Location
Mlg Ww
Part time
7,500 hours, 13,000 cycles
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

DURING TROUBLESHOOTING OF AN OIL LEAK ON ACFT, A CRACK WAS FOUND IN THE UPPER LT WHEELWELL, ABOVE THE LANDING GEAR FENDER. FOUND 3 ADDITIONAL CRACKS IN THE LT WHEELWELL SIDE WALL STRUCTURE LIGHTENING HOLE. ALL 4 CORNERS OF LIGHTENING HOLE WERE CRACKED. THE LOWER FWD CORNER IS CRACKED THROUGH THE OUTER AND INNER DOUBLERS AND YOU CAN VISUALLY SEE SEPARATION. THE OTHER 3 CORNERS ARE CRACKED BUT NOT TO THE SAME DEGREE AS THE FIRST. SIMILAR CRACKS FOUND IN THE RT MAIN GEAR WELL ALSO. INSP OF 14 ADDITIONAL ACFT FOUND CRACKS ON 6 ACFT. CAUSE OF CRACKING IS UNDETERMINED, HOWEVER THESE ACFT HAVE HIGH USAGE AS TRAINERS. ADDITIONALLY, PROP BALANCE ISSUES MAY ALSO BE A CONTRIBUTING FACTOR.

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