What was found
S2 CHECK SURFACE DAMAGE ON TOP FWD END OF FLOOR PANEL 222CF BETWEEN FRAME 12 TO 16, STRINGER 23R, Z-500 & BETWEEN Y=0 TO -Y1497. REPLACED FLOOR PANEL 222CF IAW 9701, REVISION G.
- Difficulty date
- June 25, 2014
- Submitted
- June 26, 2014
- Operation
- Air carrier
- Aircraft
- N668AW
- Make and model
- Airbus A320232
- Aircraft serial
- 1764
- Aircraft time
- 44,898 hours, 16,212 cycles
- System (JASC)
- 5321 · Fuselage Floor Panel
- Part
- Floor Panel
- Condition
- Damaged
- Location
- Fuselage
- 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.