What was found
A 3 X 12 INCH AREA OF CORE DAMAGE/DELAMINATION AT RIGHT I/B MID FLAP T/E WEDGE. REMOVED DAMAGED WEDGE AND INSTALLED NEW WEDGE PER BOEING DWG 113N2003.
- Difficulty date
- November 27, 2006
- Submitted
- November 29, 2006
- Operation
- Air carrier
- Aircraft
- N919UW
- Make and model
- Boeing 757225
- Aircraft serial
- 22198
- Aircraft time
- 69,531 hours, 31,235 cycles
- System (JASC)
- 5753 · Trailing Edge Flaps
- Part
- Wedge
- Condition
- Delaminated
- Location
- Te Flap
- 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.