Service difficulty report · Stiffener · Cndair CL6002B19

Difficulty date
January 14, 2004
Submitted
January 15, 2004
Operation
Air carrier
Aircraft
N952CA
Make and model
Cndair CL6002B19
Aircraft serial
7092
Aircraft time
20,590 hours, 18,683 cycles
Part
Stiffener
Part number
601R3220823
Condition
Cracked
Location
Fuselage
Part time
20,590 hours, 18,683 cycles
Stage of operation
IN
How discovered
9
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

VERTICAL BEAM CRACKED AT BL 0 BULKHEAD WEB AT FS 409+128 TOP RIVET LOCATION ON REINFORCING PLATE. PERFORMED A MAJOR REPAIR TO CRACKED VERTICAL BEAM, FS 409+128 BL 0 (TOP RIVET ON REINFORCING PLATE) BY TRIMMING OUT CRACKED PORTION OF STIFFENER, FABBING FILLER AND REPAIR ANGLE, AND INSTALLING PER WVAC EO 601R-53-4572 AS APPROVED BY FAA FORM 8110-3 DATED 1-12-2004.