Service difficulty report · Frame · Beech 1900D

Difficulty date
September 11, 2007
Submitted
September 19, 2007
Operation
Air carrier
Aircraft
N251GL
Make and model
Beech 1900D
Aircraft serial
UE251
Aircraft time
23,366 hours, 28,623 cycles
Engine
Pwa PT6A67D
Part
Frame
Condition
Cracked
Location
Bs 177
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

FUSELAGE FRAME CRACKED AT F.S. 177.3 AT STRINGER 9AR APPROXIMATELY 1.1 INCH IN LENGTH. MAINTENANCE REPAIRED FUSELAGE FRAME CRACK AT STRINGER RELIEF HOLE AT FS 177.3 STRINGER 9R IAW SRM 51-70. REPAIR DIMENSIONS APPROX 5 INCH BY 2.5 INCH, 2024 T-3 .080. RII INSPECTION COMPLIED IAW TASKCARD 8.2.1.

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