What was found
LEFT UPPER FUSELAGE FRAME 47, BUTT JOINT HOLE 35 AT STRINGER 7, HAS REJECT ABLE NDT INDICATIONS. REAMED HOLE IAW SRM 51-43- 00. NDT IAW NTM51-10-01, NO INDICATIONS. FINAL REAM & COLD WORK IAW SRM 51-43-00 & EA 5330-04861 OP 1.
- Difficulty date
- April 26, 2016
- Submitted
- April 28, 2016
- Operation
- Air carrier
- Aircraft
- N445UA
- Make and model
- Airbus A320232
- Aircraft serial
- 826
- Aircraft time
- 58,761 hours, 23,944 cycles
- Engine
- Iae V2527A5
- System (JASC)
- 5311 · Fuselage Main, Frame
- Part
- Frame
- Condition
- Damaged
- Location
- Fuselage
- Stage of operation
- IN
- How discovered
- O
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.