What was found
TWO AREAS ON LT FLOOR PANEL ARE BEYOND MAXIMUM BLEND DEPTH LIMITS OF REO 601R-53-41-666, SUBSECTION 1.1 AND TABLE 1, REV.C 2012-11-06. C/W REO 601R-53-41-1777 FOR REPAIR OF DAMAGE TO LT PRESSURE FLOOR PANEL
- Difficulty date
- February 12, 2014
- Submitted
- March 5, 2014
- Operation
- Air carrier
- Aircraft
- N825AS
- Make and model
- Cndair CL6002B19
- Aircraft serial
- 7207
- Aircraft time
- 37,647 hours, 33,694 cycles
- System (JASC)
- 5321 · Fuselage Floor Panel
- Part
- Floor Panel
- Condition
- Corroded
- Location
- Cabin
- 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.