What was found
(CAN) DURING INSPECTION IAW 000-53-140-300 FOUND ON FRAME FOOT FS333.00 BETWEEN STR 27-26L CORROSION DAMAGE. AFFECTED AREA A7 DATA (32X17MM): NOMINAL THICKNESS: 1.24MM MINIMUM REMAINING: 1.09MM.
- Difficulty date
- September 28, 2015
- Submitted
- April 22, 2016
- Operation
- General aviation
- Make and model
- Cndair CL6002D24
- System (JASC)
- 5311 · Fuselage Main, Frame
- Part
- Fitting
- Part number
- SH67031356
- 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.