What was found
DURING C4/S1 C-CHECK, INSPECTION NOTED FLOOR PANEL 131DG WAS PERFORATED. MX REPAIRED THE FLOOR PANEL IAW THE REQUIREMENTS OF A319 SRM 53-02-00 PARA 8C. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.
- Difficulty date
- September 22, 2008
- Submitted
- October 20, 2008
- Operation
- Air carrier
- Aircraft
- N919FR
- Make and model
- Airbus A319111
- Aircraft serial
- 1980
- Aircraft time
- 19,348 hours, 9,194 cycles
- System (JASC)
- 5321 · Fuselage Floor Panel
- Part
- Floor Panel
- Part number
- 5367221600000
- Condition
- Perforated
- 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.