What was found
2 AREAS OF DAMAGE TO UPPER SURFACE LEADING EDGE LT O/B TE AFT FLAP CAUSED BY MID FLAP COVE PANEL SUPPORT BRACKETS, 0.050 DEPTH X .5 DIA. 15 IN FROM O/B EDGE AND 0.040 DEPTH X .5 DIA. 35 IN FROM O/B EDGE, PANEL THICKNESS .120
- Difficulty date
- August 7, 2006
- Submitted
- August 10, 2006
- Operation
- Air carrier
- Aircraft
- N409
- Make and model
- Boeing 74747UF
- Aircraft serial
- 30558
- Aircraft time
- 26,339 hours, 4,065 cycles
- System (JASC)
- 5753 · Trailing Edge Flaps
- Part
- Skin
- Part number
- 65B01970209C
- Part serial
- 000549
- Condition
- Gouged
- Location
- T/E Flap
- Stage of operation
- UK
- 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.