Service difficulty report · Skin · Cndair CL6002B19

Difficulty date
November 2, 2020
Submitted
November 6, 2020
Operation
Air carrier
Aircraft
N450AW
Make and model
Cndair CL6002B19
Aircraft serial
7823
Aircraft time
37,841 hours, 36,529 cycles
Part
Skin
Part number
601R31016
Condition
Corroded
Location
Fs 295-310
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

TCAS ANTENNA SKIN HAS CORROSION AT FS 295+4. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON FUSELAGE SKIN UNDER TCAS ANTENNA IN 4 EA LOCATIONS (P1) FS 295 +4 STR 0+1.165 (P2) FS 295+4 STR 0-1.765 (P3) FS 295+10.394 AND STR 0+1.394 438?L X .08?W (P4) FS 295 +10.394 AND STR 0 1.394 .634L X 0.6?W, REF CRJ 200 SRM 51-21-06, REV 38. PERFORMED HFEC INSPECTION ON FUSELAGE SKIN BENEATH UPPER TCAS ANTENNA AT 4EA LOCATIONS (P1) FS 295 +4 STR 0+1.165 (P2) FS 295+4 STR 0-1.765 (P3) FS 295+10.394 AND STR 0+1.394 438?L X .08?W (P4) FS 295 +10.394 AND STR 0 1.394 .634?L X 0.6?W, REF CRJ 200 NDTM PART 1 REV 41 51-20-06, NO INDICATIONS NOTED. EDDY-CURRENT TESTER S/N 200051301 CAL DUE: 01/24/21. PERFORMED UT THICKNESS INSPECTION ON FUSELAGE SKIN BENEATH UPPER TCAS ANTENNA AT 4EA LOCATIONS. (P1) FS 295 +4 STR 0+1.165 (P2) FS 295+4 STR 0-1.765 (P3) FS 295+10.394 AND STR 0+1.394 438?L X .08?W (P4) FS 295 +10.394 AND STR 0 1.394 .634?L X 0.6?W. (P1) THICKNESS .050", (P2) THICKNESS .054", (P3) THICKNESS .053" AND (P4) THICKNESS .051" WITHIN LIMITS, REF AWAC SUPPLEMENT NO: 16-122B REV-B DATED: 10/24/2017 AND CRJ 200 NDTM PART 4 REV 41 51-00-001. UT THICKNESS GAUGE S/N 151136107 CAL DUE: 09/16/2021.