What was found
TUL - AT FUSELAGE STATION 804.95 FRAME OUTBOARD SIDE STIFFENER ANGLE CRACKED AT STRINGER 14R ATTACH POINT. REMOVED AND REPLACED OUTBOARD SIDE SECTION OF FRAME CHORD ANGLE PER SRM 51-10-1. (M)
- Difficulty date
- March 9, 1998
- Submitted
- March 26, 2000
- Operation
- Air carrier
- Aircraft
- N878AA
- Make and model
- Boeing 727223
- Aircraft serial
- 21390
- System (JASC)
- 5320 · Fuselage Miscellaneous Structure
- Part
- Angle
- Condition
- Cracked
- Location
- Bs 804.95
- 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.