What was found
REF HEAVY MX NON ROUTINE N0604. MAIN CABIN FLOOR PANEL 261 PF HAS COMPOSITE DAMAGE. REPAIRED 9 EACH AREAS OF SKIN DAMAGE ON FLOOR PANEL 261PF USING RESIN AND GLASS CLOTH IAW SRM 53-02-00, PARAGRAPH 8.
- Difficulty date
- July 27, 2010
- Submitted
- August 3, 2010
- Operation
- Air carrier
- Aircraft
- N933FR
- Make and model
- Airbus A319111
- Aircraft serial
- 2260
- Aircraft time
- 21,689 hours, 10,561 cycles
- System (JASC)
- 5321 · Fuselage Floor Panel
- Part
- Floor Panel
- Part number
- D5367175604800
- Condition
- Damaged
- Location
- Zone 200
- 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.