What was found
INSPECTION FOUND A 1 INCH CRACK IN VERTICAL STIFFENER 18 INCHES ABOVE RT KEEL BEAM AT MAIN WHEEL WELL FORWARD BULKHEAD, STA 663, RBL 6. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 57-10-60 AND 51-10-01.
- Difficulty date
- April 16, 2001
- Submitted
- April 17, 2001
- Operation
- Air carrier
- Aircraft
- N19357
- Make and model
- Boeing 7373T0
- Aircraft serial
- 23841
- Aircraft time
- 34,125 hours, 37,517 cycles
- System (JASC)
- 5320 · Fuselage Miscellaneous Structure
- Part
- Stiffener
- 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.