Service difficulty report · Structure · Beech 200BEECH

Difficulty date
May 27, 2003
Submitted
September 4, 2003
Operation
General aviation
Make and model
Beech 200BEECH
Engine
Pwa PT6A42
Propeller
Hartzl HCB3TN3
Part
Structure
Part number
VARIOUS
Condition
Cracked
Location
Fuselage
Part time
4,701 cycles
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

(AUS) REAR BULKHEAD BEAM EXTENSION CLEATS LOCATED AT STRINGER 5,STRINGER 7, STRINGER 8 AND STRINGER 11 CRACKED. CLEATS ARE INSTALLED DUE TO WIDENING OF THE REAR FUSELAGE FOR STC SA2192CE. FOUND DURING INSPECTION IAW AD/BEECH200/55 AMDT1 AND AD/BEECH200/21 AMDT11.