What was found
INSPECTION TYPE:3C, UPPER FUSELAGE 1EA STIFFENER CRACKED INSIDE ACCESS PANEL 364FR AT STA 2103.REMOVED CRACKED STIFFENER, FABRICATED AND INSTALLED AT UPPER FUSELAGE STA 2103 THROUGH ACCESS PANEL 364FR IAW DRWG AJC7372. (MINOR)
- Difficulty date
- May 31, 2020
- Submitted
- June 29, 2020
- Operation
- Air carrier
- Aircraft
- N262UP
- Make and model
- Doug MD11F
- Aircraft serial
- 48806
- Aircraft time
- 80,838 hours, 14,956 cycles
- System (JASC)
- 5320 · Fuselage Miscellaneous Structure
- Part
- Stiffener
- Part number
- AJC737257
- Part serial
- NA
- Condition
- Cracked
- Location
- Bs 2103
- Stage of operation
- IN
- How discovered
- 9
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.