What was found
CLT - FOUND STIFFENER CORRODED 7 INCHES BY 1 INCH, BS 235, RBL 10, WL 195 FORWARD UPPER ACCESS PANEL. INSTALLED ANGLE AND STIFFENER PER SRM 53-10-2 AND 53-30-0. (M)
- Difficulty date
- January 15, 2001
- Submitted
- November 7, 2001
- Operation
- Air carrier
- Aircraft
- N245US
- Make and model
- Boeing 737201
- Aircraft serial
- 22751
- System (JASC)
- 5320 · Fuselage Miscellaneous Structure
- Part
- Stiffener
- Condition
- Corroded
- Location
- Fuselage
- Part time
- 49,326 hours
- 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.