What was found
INSPECTION TYPE: C. LT WING FRONT SPAR VERTICLE STIFFENER/RIB ATTACH ANGLE CRACKED AT NR 3 SLAT I/B TRACK I/B ROLLER MOUNTING RIB. REMOVED AND REPLACED STIFFENER ANGLE IAW DWG 65-16200 AND SRM 57-10-2 AND 51-30-2.
- Difficulty date
- June 14, 1996
- Submitted
- March 26, 2000
- Operation
- Air carrier
- Aircraft
- N903UP
- Make and model
- Boeing 72751C
- Aircraft serial
- 18945
- System (JASC)
- 5754 · Leading Edge Devices
- Part
- Angle
- Condition
- Cracked
- Location
- N 3 Slat Track
- 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.