What was found
C2 CHECK DELAMINATION ON FLOOR PANEL 232XF BETWEEN FRAME 26.1 TO FRAME 26.4 & BETWEEN Y 953 TO Y 1456. REPLACED FLOOR PANEL 232XF IAW SRM 53-02-00, PARA 5I, FIG 211 & 53-02-00.
- Difficulty date
- February 4, 2014
- Submitted
- February 4, 2014
- Operation
- Air carrier
- Aircraft
- N273AY
- Make and model
- Airbus A330323
- Aircraft serial
- 337
- Aircraft time
- 63,993 hours, 8,982 cycles
- System (JASC)
- 5321 · Fuselage Floor Panel
- Part
- Floor Panel
- Part number
- F5367270300000
- 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.