Service difficulty report · Skin · Cndair CL6002B19

Difficulty date
September 11, 2014
Submitted
September 12, 2014
Operation
Air carrier
Aircraft
N851AS
Make and model
Cndair CL6002B19
Aircraft serial
7360
Aircraft time
33,738 hours, 30,286 cycles
Part
Skin
Condition
Damaged
Location
Bs 654-672
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

DENT AND HOLE IN FUSELAGE SKIN BETWEEN BS 654-672 AND STRINGERS 26 - 27R. FOUND DAMAGE TO BE IN A NON-REPAIRABLE LOCATION IAW SRM 53-00-31. SUBMITTED DAMAGE REPORT TO STS IAW SRM TR 51-27. RECEIVED EA 12-2014-219, P1, 09/11/2014. CUT AWAY DAMAGED SECTION, PUNCTURE TO .5625" CIRCLE REPORTED CUT-OUT DIMENSION TO STS FOR FINAL REPAIR, DRESSED BACK DENTS , AND ENSURED NO UNDERLYING STRUCTURE DAMAGE. TOUCHED UP CUT LINES. ALL WORK ACCOMPLISHED IN IAW EA 12-2014-219, P1. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3. RECEIVED EA 12-2014-219, 09/12/2014. FABRICATED REPAIR DOUBLER, 2024-T3 .050" BATCH 1852686, LAYED OUT NEW FASTENER PATTERN , DRILLED AND FINAL SIZED ALL NEW HOLES IN SKIN , AND DOUBLER. DEBURRED AND REMOVED ALL SHARP EDGES, ALODINED, AND PRIMED DOUBLER. ALL WORK ACCOMPLISHED IAW EA 12-2014-219. OK TO PROCEED WITH INSTALLATION OF REPAIR DOUBLER. APPLIED SEALANT TO BOTH FAYING SURFACES, DOUBLER + SKIN, WET INSTALLED ALL FASTENERS, NAS1097AD5 RIVETS, REMOVED ALL EXCESS SEALANT, RESTORED SURFACE FINISH AND CORROSION PROTECTION, ALL WORK ACCOMPLISHED IAW EA 12-2014-219. THIS JOB IS CONSIDERED A PERMANENT REPAIR.