What was found
RIGHT UPPER VENTRAL DOOR CORNER STIFFENER BEAM ATTACH ANGLE IS CRACKED, LOCATED BETWEEN LONGERON 3 AND 4 RIGHT ON AFT PRESSURE BULKHEAD FORWARD SIDE. REMOVED AND REPLACED STIFFENER.
- Difficulty date
- February 8, 2002
- Submitted
- February 12, 2002
- Operation
- Air carrier
- Aircraft
- N203ME
- Make and model
- Doug DC932
- Aircraft serial
- 47673
- Aircraft time
- 66,720 hours, 39,500 cycles
- System (JASC)
- 5320 · Fuselage Miscellaneous Structure
- Part
- Stiffener
- Part number
- 991556253
- Condition
- Cracked
- 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.