What was found
INSPECTION FOUND A 1 INCH CRACK AT EACH END OF PANEL 1104 STIFFENER. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0.
- Difficulty date
- December 23, 1999
- Submitted
- March 26, 2000
- Operation
- Air carrier
- Aircraft
- N33785
- Make and model
- Boeing 727232
- Aircraft serial
- 20640
- System (JASC)
- 5320 · Fuselage Miscellaneous Structure
- Part
- Stiffener
- Condition
- Cracked
- Location
- Panel 1104
- Stage of operation
- IN
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.