What was found
UPON COMPLIANCE OF 2C INSPECTION TASK 261-01Z, THE FUSELAGE SKIN SUPPORT BRACKET AT FRAME 40, BETWEEN STRINGERS 3L AND 4L, WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.
- Difficulty date
- May 11, 2000
- Submitted
- May 23, 2000
- Operation
- Air carrier
- Aircraft
- N258CA
- Make and model
- Emb EMB120RT
- Aircraft serial
- 120247
- Aircraft time
- 21,145 hours, 22,062 cycles
- System (JASC)
- 5310 · Fuselage Main, Structure
- Part
- Support Bracket
- Part number
- 12006218001
- Condition
- Cracked
- Location
- Fuselage
- Part time
- 21,145 hours, 22,062 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.