What was found
11 INCH BY 11 INCH AREA OF DELAMINATION ON FLOOR PANEL AT FRAME 19A, STRINGER 23R & -Y28. REPLACED FLOOR PANEL AT FRAME 19A, STRINGER 23R, -Y28 IAW AMM 53-12-12.
- Difficulty date
- June 21, 2014
- Submitted
- June 23, 2014
- Operation
- Air carrier
- Aircraft
- N564UW
- Make and model
- Airbus A321231
- Aircraft serial
- 5374
- Aircraft time
- 5,023 hours, 2,188 cycles
- System (JASC)
- 5321 · Fuselage Floor Panel
- Part
- Floor Panel
- Part number
- E5367148100000
- Condition
- Delaminated
- 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.