What was found
UPON COMPLIANCE OF 2C INSPECTION TASK 263/264-01Z, THE FUSELAGE FRAME 46A WAS FOUND TO BE GOUGED BY INTERIOR LINING SCREWS IN TWO PLACES. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.
- Difficulty date
- June 14, 2000
- Submitted
- June 15, 2000
- Operation
- Air carrier
- Aircraft
- N261CA
- Make and model
- Emb EMB120RT
- Aircraft serial
- 120254
- Aircraft time
- 20,620 hours, 21,446 cycles
- System (JASC)
- 5311 · Fuselage Main, Frame
- Part
- Frame
- Part number
- 12022636501
- Condition
- Gouged
- Location
- Fuselage
- Part time
- 20,620 hours, 21,446 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.