What was found
RIGHT FRAME 68 FWD FACE JUST ABOVE FLOOR LEVEL IS CORRODED. ORIGINAL THICKNESS .098 INCHES, MATERIAL LOSS OF .035 INCHES IS OUT OF LIMITS IAW SRM 53-41-12 FIG 102. REPAIRED IAW SRM 53-41-12 PAR 5A FIG 201. DOUBLER INSTALLED.
- Difficulty date
- February 23, 2015
- Submitted
- February 26, 2015
- Operation
- Air carrier
- Aircraft
- N405UA
- Make and model
- Airbus A320232
- Aircraft serial
- 452
- Aircraft time
- 71,606 hours, 26,680 cycles
- Engine
- Iae V2527A5
- System (JASC)
- 5311 · Fuselage Main, Frame
- Part
- Frame
- Condition
- Corroded
- 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.