What was found
UPON INSTALL OF R/H LATERAL SKIN PANEL FOUND SKIN STIFFENER AT L OWER LAP JOINT FR1-2 TO HAVE CRACK AT AFT END. REMOVED AND INSTALLED NEW R/H LATERAL SKIN PANEL SKIN STIFFENER AT LOWER LAP JOINT FR1-2 AS PER A319 SRM 51-42-11.
- Difficulty date
- April 2, 2024
- Submitted
- April 3, 2024
- Operation
- Air carrier
- Aircraft
- N892UA
- Make and model
- Airbus A319132
- Aircraft serial
- 2940
- Aircraft time
- 47,026 hours, 27,671 cycles
- System (JASC)
- 5310 · Fuselage Main, Structure
- Part
- Stiffener
- Part number
- D53110220201
- Condition
- Cracked
- Location
- Lap Joiint
- 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.