Service difficulty report · Frame · Beech 200BEECH

Difficulty date
December 12, 2005
Submitted
June 6, 2006
Operation
General aviation
Make and model
Beech 200BEECH
Engine
Pwa PT6A41
Propeller
Hartzl HCD4N3A
Part
Frame
Condition
Corroded
Location
Fuselage
Part time
10,743 hours
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

(AUS) FUSELAGE FRAME LOCATED AT FS226.875 UNDER THE RT SEAT ROW CORRODED IN AREA BETWEEN 2 STRINGERS. CORROSION EXTENDED UP THE FRAME WEB. FOUND DURING INSPECTION IAW AD/B200/21 AMDT 11.(AD/SB DESC: AD/B200/21 AMDT 11 ) (CASA NR 510001628)