Service difficulty report · Skin Panel · Cessna 680CE

Difficulty date
April 30, 2025
Submitted
April 30, 2025
Operation
General aviation
Aircraft
N388QS
Make and model
Cessna 680CE
Aircraft serial
6800113
Aircraft time
15,752 hours, 10,537 cycles
Part
Skin Panel
Condition
Corroded
Location
Zone 100
Part time
15,752 hours, 10,537 cycles
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.

What was found

RH FWD FUSELAGE HAS PRESENCE OF CORROSION AROUND AVIONICS DOOR. PERFORMED EDDY CURRENT INSPECTION FOR CRACKS AND CORROSION ON RH FWD FUSELAGE AROUND AVIONICS DOOR IAW CESSNA 680 NDTM PART 6 CHAPTER 20-00-02. NO CRACKS OR CORROSION NOTED DURING TIME OF INSPECTION. PERFORMED ULTRASONIC REMAINING THICKNESS INSPECTION ON RH FWD FUSELAGE AROUND AVIONICS DOOR IAW CESSNA 680 NDTM PART 4 CHAPTER 20-00-01. RECORDED REMAINING THICKNESS ON STRUCTURE. REFER TO SQUAWK 98-1 FOR ADDITIONAL DETAILS. COMPLIED WITH RFTS-113690 REV.0 DATED 29APR25. N388QS (680-0113) RH NOSE FUSELAGE SKIN CORROSION. THIS IS A PERMANENT MINOR REPAIR.