What was found
FLOOR PANEL 232YG CENTER TOP SKIN CRACKED APPROX 8 INCHES FWD OF THE CLEVIS ADAPTER. AFT CLEVIS AREA CRACK APPROX 4". FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.
- Difficulty date
- October 19, 2012
- Submitted
- October 19, 2012
- Operation
- Air carrier
- Aircraft
- N675FE
- Make and model
- Airbus A300F4605R
- Aircraft serial
- 789
- Aircraft time
- 21,477 hours, 11,592 cycles
- System (JASC)
- 5321 · Fuselage Floor Panel
- Part
- Floor Panel
- Part number
- B5327050600400
- Condition
- Cracked
- 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.