What was found
HEAVY MX NON-ROUTINE N0283. REAR FUSELAGE FLOORBEAM AT FRAME 66 HAS CORROSION AROUND FASTENER HOLE. REPAIRED AREA IAW SRM 53-41-14, PAGE 201, FIGURE 201 PRINCIPLE NR 6.
- Difficulty date
- May 8, 2010
- Submitted
- May 22, 2010
- Operation
- Air carrier
- Aircraft
- N931FR
- Make and model
- Airbus A319111
- Aircraft serial
- 2253
- Aircraft time
- 21,093 hours, 10,254 cycles
- Engine
- Cfmint CFM565B5P
- System (JASC)
- 5315 · Fuselage Main, Floor Beam
- Part
- Floorbeam
- Part number
- D5340217220300
- 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.