What was found
THE DAMAGE CONSISTS OF A BLENDOUT IN THE SKIN MEASURING 2.5 X 1.2 X 0.022 DEEP LOCATED 0.4 BELOW THE LOWER FASTENER ROW COMMON TO S-18L AND 1.1 FORWARD OF THE FORWARD FASTENER ROW COMMON TO FS 621. REPAIRED IAW EA CRJ253-00987A.
- Difficulty date
- November 2, 2012
- Submitted
- November 4, 2012
- Operation
- Air carrier
- Aircraft
- N8709A
- Make and model
- Cndair CL6002B19
- Aircraft serial
- 7709
- Aircraft time
- 22,275 hours, 19,829 cycles
- System (JASC)
- 5330 · Fuselage Main, Plate/Skin
- Part
- Skin
- Condition
- Damaged
- 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.