What was found
A 1.75 INCH CRACK WAS DISCOVERED IN THE LOWER FUSELAGE SECTION AFT OF THE MAIN SPAR ON THE LEFT SIDE (FS 292) DURING A ROUTINE INSPECTION. THE CRACK WAS STOP DRILLED AND A DOUBLER INSTALLED IAW BEECH SRM CHAP 53-90-18.
- Difficulty date
- April 3, 2012
- Submitted
- April 24, 2012
- Operation
- Air carrier
- Aircraft
- N154GA
- Make and model
- Beech 1900C
- Aircraft serial
- UB25
- Aircraft time
- 36,116 hours, 47,457 cycles
- System (JASC)
- 5330 · Fuselage Main, Plate/Skin
- Part
- Skin
- Condition
- Cracked
- Location
- Fuselage
- Part time
- 36,116 hours, 47,457 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.