What was found
DURING C-3 CHECK, INSPECTION REPORTED STIFFENER ANGLE CRACKED AT STA 298 - STA 304. FABRICATED AND INSTALLED REPLACEMENT CLIP PER SRM 51-10-2 AND 51-30-2.
- Difficulty date
- February 28, 2002
- Submitted
- March 4, 2002
- Operation
- Air carrier
- Aircraft
- N118RW
- Make and model
- Boeing 7372Y5
- Aircraft serial
- 23040
- Aircraft time
- 58,984 hours, 28,541 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.