What was found
WING ANTI ICE CROSS FLOW VALVE STUDS HAVE DAMAGED LOWER FUSELAGE SKIN IN TWO PLACES. BLENDED, OUT DAMAGE TO PREPARE FOR NDT. NO CRACKS NOTED. COMPLETED STANDARD REPAIR SR-680A-ATA53-22175.
- Difficulty date
- July 23, 2019
- Submitted
- July 23, 2019
- Operation
- General aviation
- Aircraft
- N535QS
- Make and model
- Cessna 680A
- Aircraft serial
- 680A0081
- Aircraft time
- 2,411 hours, 1,603 cycles
- System (JASC)
- 5330 · Fuselage Main, Plate/Skin
- Part
- Skin
- Condition
- Damaged
- 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.