What was found
HNL - MAINTENANCE FOUND FUSELAGE SKIN PANEL, UPPER CENTER FORWARD, CORRODED. PANEL CORRODED BEYOND LIMITS FOR 2024T3, .032 INCH THICK. REMOVED AND REPLACED PANEL ASSEMBLY IAW C208 SRM 53-10-10 AND SRM 51-40-00. (X)
- Difficulty date
- October 22, 2000
- Submitted
- November 9, 2000
- Operation
- General aviation
- Aircraft
- N904FE
- Make and model
- Cessna 208B
- Aircraft serial
- 208B0004
- System (JASC)
- 5330 · Fuselage Main, Plate/Skin
- Part
- Skin
- Part number
- 26110002
- Condition
- Corroded
- Location
- Fuselage
- Part time
- 6,433 hours
- 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.