What was found
VERTICAL STABILIZER LEADING EDGE PANEL 322CL WAS DELAMINATED. THE DIMENSION FOR REPAIR IAW SRM TO GREAT. REPAIR PERFORMED IAW SRM 55-32-00 FIG 203 AND FIG 216, APPROVED BY EA 6-5532-81077 AND RAS/DAHAM/4018735/2004.
- Difficulty date
- September 19, 2007
- Submitted
- September 19, 2007
- Operation
- Air carrier
- Aircraft
- N434FE
- Make and model
- Airbus A310203
- Aircraft serial
- 355
- Aircraft time
- 44,246 hours, 19,687 cycles
- System (JASC)
- 5532 · Vertical Stabilizer, Plate/Skin
- Part
- Panel
- Part number
- A55373311
- Condition
- Delaminated
- Location
- Zone 300
- 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.