What was found
(CAN) DURING C CHECK, CORROSION FOUND ON FUSELAGE SKIN BS 559+32 TO 559+112 STRINGER 27. NO DAMAGE IS ALLOWED IN THIS AREA IAW SRM 53-00-31. MINIMUM REMAINING THICKNESS IS 0.057", ORIGINAL THICKNESS IS 0.063".
- Difficulty date
- November 11, 2015
- Submitted
- April 22, 2016
- Operation
- General aviation
- Make and model
- Cndair CL6002B19
- System (JASC)
- 5330 · Fuselage Main, Plate/Skin
- Part
- Skin
- Part number
- 601R38328
- Condition
- Corroded
- 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.