What was found
UPON COMPLIANCE OF 2C INSPECTION TASK 231-012, WHILE GAINING ACCESS THE LT FUSELAGE SKIN SUPPORT BETWEEN FRAMES 12 AND 13 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.
- Difficulty date
- May 19, 2000
- Submitted
- May 31, 2000
- Operation
- Air carrier
- Aircraft
- N263CA
- Make and model
- Emb EMB120RT
- Aircraft serial
- 120255
- Aircraft time
- 20,734 hours, 22,260 cycles
- System (JASC)
- 5310 · Fuselage Main, Structure
- Part
- Shear Tie
- Part number
- 12012545001
- Condition
- Cracked
- Location
- Fuselage
- Part time
- 20,734 hours, 22,260 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.