Service difficulty report · Attach Angle · Cndair CL6002C10

Difficulty date
March 19, 2008
Submitted
April 1, 2008
Operation
Air carrier
Aircraft
N355CA
Make and model
Cndair CL6002C10
Aircraft serial
10067
Aircraft time
14,111 hours, 10,220 cycles
Part
Attach Angle
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

SUSPECTED CRACK AT RIGHT SIDE BASE OF VERTICAL STAB AT FS 1181. WORK COMPLETED IN ACCORDANCE WITH: PERFORMED EDDY CURRENT INSPECTION OF RIGHT SIDE BASE OF VERTICAL STAB AT FS 1181 IAW CRJ700 NDTM 51-20-006. AREA IS CONFIRMED CRACKED AND MARKED. 03/19/08 VTJ7010159. REMOVED DAMAGE PER REO 670-55-31-018. PERFORMED EDDY CURRENT INSPECTION OF CUT LINE ON RIGHT DRAG ANGLE IAW REO 670-55-31-018 PER CRJ 700 NDTM 51-20-006. NO DEFECTS NOTED. 03/20/08 VTJ7010159. STARTED FABRICATING 670-55-31-018-3 DOUBLER AND -4 FILLER FROM 2024T3 .090" PO# TO3606 RT SIDE V/STAB TO FUSELAGE ATTACH ANGLE PER REO 670-55-31-018. FINISHED FABRICATING DOUBLER -3 AND FILLER -4 PER REO 670-55-31-018. INSTALLED FILLER AND DOUBLER IAW REO670-55-31-018 DB 7020877. APPLIED TOPCOAT FINISH TO REPAIR AREA LOCATED ON RT BASE OF VERTICAL STAB AT FS 1181 PER CRJ 700 SRM 51-21-16. JOB COMPLETE. SUPPLEMENTAL SDR CLOSED 3/31/08.