What was found
AT SCHEDULED INSPECTION, DISCOVERED ONE INCH LATERAL CRACK IN FUSELAGE BELLY SKIN IN SPAR AREA AT BL 30.62. STOP DRILLED CRACK AND INSTALLED REINFORCEMENT DOUBLER REF SRM 53-90-18, (FUSELAGE SKIN CRACK REPAIR IN SPAR AREA).
- Difficulty date
- January 21, 2008
- Submitted
- March 24, 2008
- Operation
- Air carrier
- Aircraft
- N81538
- Make and model
- Beech 1900D
- Aircraft serial
- UE199
- Aircraft time
- 24,220 hours, 29,483 cycles
- Engine
- Pwa PT6A67D
- System (JASC)
- 5330 · Fuselage Main, Plate/Skin
- Part
- Skin
- Condition
- Cracked
- Location
- Fuselage
- 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.