What was found
STIFFENER BETWEEN FRAMES 38.1-38.2 R/H SIDE WITH CRACK. INSTALLED FLOOR ANGLE AT MAIN CABIN FR38.1 TO FR38.2 IAW SRM 51-40-21-001 AND REMOVED PROTECTION ELECTRICAL (EWIS) IAW ESPM 20-54-50-02. REPLACED STIFFENER IAW SRM 51-40-21-001.
- Difficulty date
- April 10, 2026
- Submitted
- May 11, 2026
- Operation
- Air carrier
- Aircraft
- N141UP
- Make and model
- Airbus A300F4622R
- Aircraft serial
- 0824
- Aircraft time
- 28,223 hours, 17,497 cycles
- System (JASC)
- 5320 · Fuselage Miscellaneous Structure
- Part
- Stiffener
- Part number
- A5378103821500
- 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.