What was found
FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH ANGLES ARE CRACKED. INBOARD AND OUTBOARD; FS 280.00; LBL - 9.0. REPLACED ATTACH ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-23-00, 51-42-21, 51-25-16, 51-21-11, 57-42-13.
- Difficulty date
- April 22, 2005
- Submitted
- July 15, 2005
- Operation
- Air carrier
- Aircraft
- N962SW
- Make and model
- Cndair CL6002B19
- Aircraft serial
- 7859
- Aircraft time
- 4,302 hours, 3,874 cycles
- System (JASC)
- 5340 · Fuselage Main, Attach Fittings
- Part
- Attach Angle
- 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.