Service difficulty report · Cable · Cndair CL6002B19

Difficulty date
March 19, 2012
Submitted
March 23, 2012
Operation
Air carrier
Aircraft
N857AS
Make and model
Cndair CL6002B19
Aircraft serial
7411
Aircraft time
27,170 hours, 24,024 cycles
Part
Cable
Condition
Corroded
Location
Downlock
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

LEFT EMERGENCY EXIT INTERNAL DOUBLER CORRODED. REMOVED RIVETS TO ROLL SKIN BACK IAW SRM 51-42-011-00. PERFORMED UT THICKNESS INSP IAW MAC NDT PROCEDURE UT-3 MIN MATERAIL REMAINING IS .039", ORIGINAL IS .040", MATERIAL REMOVED IS .001". CORROSION ON INTERIOR OF OUTER DOOR FRAME FLANGE (LOWER AFT) -61 SPLICE ANGLE FLANGE AND SEAL RETAINER. REMOVED CORROSION IAW SRM 51-21-06 FROM FRAME FLANGE .8" X.3" X .005" - .045" REMAINING FROM ANGLE FLANGE .5" X 1.3" X .003" - .047" REMAINING, FROM SEAL RETAINER .8" X 3" X .003" - .037" REMAINING MATERIAL. ALL BLENDS REQUIRE SUBMISSION TO RT ALL ARE BEYOND LIMITS OF SRM 52-00-00. DAMAGE IS ADJACENT TO FASTENER HOLES. RII FOUND TO BE SATISFACTORY. (SDR CLOSED)