What was found
INSPECTION TYPE:3CR/H WING TO BODY CANTED PANEL CAP VERTICAL STIFFENER IS CRACKED AT STA. 1256.REMOVED, FABRICATED AND REPPLACED STIFFENER IAW DWG. AYB7104 AND SRM 51-33-01. (MINOR)
- Difficulty date
- May 8, 2022
- Submitted
- May 25, 2022
- Operation
- Air carrier
- Aircraft
- N257UP
- Make and model
- Doug MD11F
- Aircraft serial
- 48451
- Aircraft time
- 79,773 hours, 17,321 cycles
- System (JASC)
- 5310 · Fuselage Main, Structure
- Part
- Stiffener
- Part number
- AYB7104522
- Condition
- Cracked
- Location
- Wing To Body
- Stage of operation
- IN
- How discovered
- 9
- Nature of condition
- O
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.