Service difficulty report · Frame · Beech 200BEECH

Difficulty date
February 6, 2004
Submitted
June 4, 2004
Operation
General aviation
Make and model
Beech 200BEECH
Engine
Pwa PT6A42
Propeller
Hartzl HCB3TN3
Part
Frame
Condition
Cracked
Location
Fuselage
Part time
10,156 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

(AUS) FUSELAGE FRAME LOCATED AT RF 265-760 CRACKED IN AREA ADJACENT TO FLOORBEAM. FOUND DURING INSPECTION IAW AD/BEECH200/65.