Service difficulty report · Skin · Cndair CL6002D24

Difficulty date
November 28, 2015
Submitted
November 30, 2015
Operation
Air carrier
Aircraft
N907XJ
Make and model
Cndair CL6002D24
Aircraft serial
15139
Aircraft time
20,396 hours, 13,255 cycles
Part
Skin
Condition
Cracked
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.

What was found

3"" SCRATCH AFT & ABOVE FWD CARGO DOOR APPROX 18"" FROM THE TOP RT CORNER IN THE 2 O' CLOCK POSITION. DURING ROUTINE LINE MX FOUND THE FUSELAGE SKIN AT FS 541 & 3.25” BELOW STRINGER 16L TO BE DENTED. THE DENT MEASURES 4” X 0.75” X 0.040” DEEP. FOLLOWING REWORK OF THE SKIN A CRACK WAS NOTED IN THE DENT. THE SKIN IS FORMED FROM 0.150” THICK 2024 T3 CLAD ALUMINUM, CHEM MILLED TO 0.061”, IN THE BAY. MX CONTACTED ENGINEERING FOR EVALUATION & DISPOSITION. REPAIRED DAMAGED AREA IAW EA CRJ953-03835 ALL CHECKED GOOD. EA CRJ953 03835 REVISION A WAS ISSUED TO PROVIDE REPAIR INSTRUCTIONS FOR THE FUSELAGE SKIN. THE DAMAGE WAS CUT OUT RESULTING IN A 4.25” X 1.75” CUT OUT & THE SKIN REPAIRED WITH A 0.063” THICK 2024 T3 CLAD ALUMINUM EXTERNAL DOUBLER, INSTALLED USING HST11AG6 LOCK FASTENERS IN PRODUCTION LOCATIONS & HST11AG5 LOCK FASTENERS IN REPAIR LOCATIONS.