What was found
CRACK ON FLOORBEAM UPPER/AFT FLANGE IN STA FS= 280 AND 14LBL AT PAX CABIN FWD WET AREA. FLOORBEAM WAS REPLACED PER SRM 51-42-06-001-001-A01 PAR 6 C; SRM 51-42-20-001-001-A01 PAR 6 C. AND SRM 5 1-42-13-001-001-A01 PAR 6 C
- Difficulty date
- February 2, 2019
- Submitted
- February 12, 2019
- Operation
- Air carrier
- Aircraft
- N918XJ
- Make and model
- Cndair CL6002D24
- Aircraft serial
- 15156
- Aircraft time
- 26,657 hours, 17,623 cycles
- System (JASC)
- 5315 · Fuselage Main, Floor Beam
- Part
- Floorbeam
- Condition
- Cracked
- 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.