What was found
FUSELAGE FRAME CRACKED .5 INCH AT FS 183 AT STRINGER 9R. MAINT REPAIRED FRAME CRACK AT STR RELIEF HOLE FS 183, STRINGER 9R IAW SRM REF 51-70. REPAIR APPROXIMATELY 5.5 INCH X 2.5 2024-T3 .071. RII INSPCOMPLIED WITH IAW TASKCARD 8.2.1.
- Difficulty date
- February 25, 2008
- Submitted
- February 28, 2008
- Operation
- Air carrier
- Aircraft
- N122UX
- Make and model
- Beech 1900D
- Aircraft serial
- UE122
- Aircraft time
- 23,825 hours, 33,147 cycles
- Engine
- Pwa PT6*
- System (JASC)
- 5311 · Fuselage Main, Frame
- Part
- Frame
- Condition
- Cracked
- Location
- Bs 183
- 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.