What was found
PANEL AFT OF DOUBLE DRAINS ON FWD FUSELAGE L/E EXPOSED AND SCREW PULLING THRU-POS DELAMINATED. APPLIED SPEED TAPE IAW MT 53-00-02, PANEL MUST BE REPLACED WITHIN 300 HOURS.
- Difficulty date
- June 16, 2013
- Submitted
- June 19, 2013
- Operation
- Air carrier
- Aircraft
- N463UA
- Make and model
- Airbus A320232
- Aircraft serial
- 1282
- Aircraft time
- 45,159 hours, 17,512 cycles
- Engine
- Iae V2527A5
- System (JASC)
- 5330 · Fuselage Main, Plate/Skin
- Part
- Skin Panel
- Condition
- Delaminated
- 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.