What was found
CLT - Q4 - CRACK IN FUSELAGE FRAME REINFORCEMENT ANGLE AT BS 500E BETWEEN S20R TO S21R. REPAIRED FUSELAGE FRAME REINFORCEMENT ANGLE AT BS 500E BETWEEN S20R TO S21R IAW B737 SRM 53-00-07 REPAIR 13.
- Difficulty date
- May 14, 2011
- Submitted
- June 9, 2011
- Operation
- Air carrier
- Aircraft
- N430US
- Make and model
- Boeing 7374B7
- Aircraft serial
- 24552
- Aircraft time
- 57,415 hours, 38,122 cycles
- System (JASC)
- 5311 · Fuselage Main, Frame
- Part
- Angle
- Condition
- Cracked
- Location
- Fuselage
- Stage of operation
- IN
- How discovered
- E
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.