What was found
UPON COMPLIANCE OF 2C INSPECTION TASK 612-01Z, THE RIGHT WING OUTBOARD LEADING EDGE WAS FOUND TO BE DELAMINATED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND SRM 57-40-01, FIGURE 201.
- 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)
- 5753 · Trailing Edge Flaps
- Part
- Skin
- Part number
- 12034592002
- Condition
- Delaminated
- Location
- Rt Wing
- 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.