What was found
(AUS) FUSELAGE FRAME 20 LOCATED IN R1 DOOR CUTOUT SEVERELY CORRODED.AREA OF CORROSION 152.4MM BY 101.6MM (6IN BY 4IN) WITH A MAXIMUMDEPTH OF 2.8MM (0.112IN). EVIDENCE OF PREVIOUS CORROSION REMOVALIN THE SAME AREA.
- Difficulty date
- March 15, 2000
- Submitted
- June 23, 2000
- Operation
- Air carrier
- Make and model
- Airbus A320211
- Engine
- Cfmint CFM565A1
- 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.