What was found
CORROSION PITS ON TOP SKIN PANEL BETWEEN FRAME 80-95, STRG 6 RT TO 6 LT. REPAIR PERFORMED BY REWORK AND FLAP PEENING IAW EA 6-5319-92157 AND RAS/DAHAM/4019752/2005 ISSUE A.
- Difficulty date
- September 13, 2007
- Submitted
- September 13, 2007
- Operation
- Air carrier
- Aircraft
- N815FD
- Make and model
- Airbus A310324
- Aircraft serial
- 638
- Aircraft time
- 29,280 hours, 8,574 cycles
- System (JASC)
- 5330 · Fuselage Main, Plate/Skin
- Part
- Skin Panel
- Part number
- A53985240204
- Condition
- Corroded
- Location
- Zone 200
- 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.