What was found
REMOVED CRACKED STIFFENER FROM MED UPPER WEB ASSEMBLY AND INSTALLED NEW P/N 661039-2 USING MS20426AD4, MS20470AD4, MS20426AD5, AND MS20470AD5 RIVETS REFERENCING STRUCTURAL REPAIR MANUAL 51-40-03 AND 51-40-06.
- Difficulty date
- September 4, 2018
- Submitted
- September 4, 2018
- Operation
- Air carrier
- Filed by
- JGVR194F
Duncan Aviation Inc - Aircraft
- N555QS
- Make and model
- Cessna 560XL
- Aircraft serial
- 5605543
- Aircraft time
- 9,710 hours, 7,474 cycles
- System (JASC)
- 5320 · Fuselage Miscellaneous Structure
- Part
- Stiffener
- Part number
- 6610392
- 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.