What was found
RT FUSELAGE SKIN AREA AT STA 187.00 AT WING STRUT ATTACH POINT HAS PREVIOUS REPAIR WORN BEYOND LIMITS. INSTALLED FUSELAGE SKIN REPAIR IAW FAA FORM 8110-3 DATED 1-13-13 AND DWG HAS-208-53-02.
- Difficulty date
- January 8, 2013
- Submitted
- January 24, 2013
- Operation
- Air carrier
- Aircraft
- N208SD
- Make and model
- Cessna 208B
- Aircraft serial
- 208B0491
- Aircraft time
- 16,394 hours, 29,785 cycles
- System (JASC)
- 5330 · Fuselage Main, Plate/Skin
- Part
- Skin
- Condition
- Worn
- Location
- Bs 187
- 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.