What was found
PIT - C11/SY6 - DELAMINATION ON FLOOR PANEL 261AG BETWEEN FR64 TO FR66 & BETWEEN Y254 TO -Y254. REPLACED FLOOR PANEL 261AG BETWEEN FR64 TO FR66 & BETWEEN Y254 TO -Y254 IAW MCGILL IRM 9701 REV G.
- Difficulty date
- May 2, 2011
- Submitted
- May 5, 2011
- Operation
- Air carrier
- Aircraft
- N835AW
- Make and model
- Airbus A319132
- Aircraft serial
- 2458
- Aircraft time
- 20,618 hours, 8,672 cycles
- System (JASC)
- 5321 · Fuselage Floor Panel
- Part
- Floor Panel
- Part number
- D5367063700000
- 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.