What was found
AREA OF DELAMINATION ON LT SIDE OF VERTICAL STABILIZER SIDE PANEL APPROXIMATELY 20 INCHES ABOVE FUSELAGE & 2 INCHES FORWARD OF RUDDER L/E. REPAIRED LT SIDE OF VERTICAL STABILIZER SIDE PANEL IAW SRM 51-77-13 & 55-77-13.
- Difficulty date
- October 5, 2013
- Submitted
- November 6, 2013
- Operation
- Air carrier
- Aircraft
- N186US
- Make and model
- Airbus A321211
- Aircraft serial
- 1701
- Aircraft time
- 40,230 hours, 14,831 cycles
- System (JASC)
- 5532 · Vertical Stabilizer, Plate/Skin
- Part
- Panel
- Condition
- Delaminated
- Location
- Vertical Stab
- 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.