What was found
(CAN) VERTICAL STAB LEADING EDGE PANELS 322AL AND 322CL CRACKED. PANEL 322AL CRACKED APPROXIMATELY 4 INCHES FROM LOWER EDGE LT SIDE. PANEL 322CL CRACKED APPROXIMATELY 4 INCHES FROM LOWER EDGE LT SIDE.
- Difficulty date
- February 12, 2002
- Submitted
- March 21, 2002
- Operation
- General aviation
- Make and model
- Airbus A319114
- Aircraft time
- 9,399 hours
- Engine
- Cfmint CFM565A1
- System (JASC)
- 5532 · Vertical Stabilizer, Plate/Skin
- Part
- Panel
- Part number
- D5537002500800
- Condition
- Cracked
- 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.