What was found
INSPECTION TYPE:C2 LEFT WING T/E INBOARD VERTICAL STIFFENER AT FLAP HINGE 98 IS CRACKED AT BOTTOM. REMOVED, FABRICATED, AND INSTALLED STIFFENER IAW DWG 3643320, AND SRM 51-3-0.
- Difficulty date
- July 23, 2002
- Submitted
- August 12, 2002
- Operation
- Air carrier
- Aircraft
- N772UP
- Make and model
- Doug DC871F
- Aircraft serial
- 46072
- Aircraft time
- 67,542 hours, 44,705 cycles
- System (JASC)
- 5720 · Wing Miscellaneous Structure
- Part
- Stiffener
- Part number
- 36433191
- Condition
- Cracked
- Location
- Lt Wing
- 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.