What was found
DURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS IN THE FUSELAGE FRAME ANGLE AT FS 150.00 & STRINGER 6L AT THE UPPER & LOWER A/S DOOR GAS STRUT MOUNT NUTPLATE AREA, 1" IN LENGTH. REPAIRED IAW EO 13-1900-53-046.
- Difficulty date
- June 18, 2013
- Submitted
- June 18, 2013
- Operation
- Air carrier
- Aircraft
- N251GL
- Make and model
- Beech 1900D
- Aircraft serial
- UE251
- Aircraft time
- 35,193 hours, 43,140 cycles
- System (JASC)
- 5311 · Fuselage Main, Frame
- Part
- Frame
- Condition
- Cracked
- Location
- Bs 150
- 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.