Service difficulty report · Web · Cndair CL6002C10

Difficulty date
April 2, 2010
Submitted
April 6, 2010
Operation
Air carrier
Aircraft
N355CA
Make and model
Cndair CL6002C10
Aircraft serial
10067
Aircraft time
19,090 hours, 13,933 cycles
Engine
Ge CF348C1
Part
Web
Condition
Corroded
Location
Bs 280
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

CORROSION FOUND ON LT LOWER WEB AT FS 280 BETWEEN LBL 10 & LBL 13. REMOVED CORROSION FOUND ON LT LOWER WEB. ALL WORK DONE IAW SRM 53-11-10-201-003-A01. THICKNESS CHECK REQUIRED TO ENSURE THAT MIN WEB THICKNESS OF .0035" WAS NOT EXCEEDED. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA ON LT LOWER WEB IAW MAC NDT INSP PROCEDURE UT-3 MINIMUM MATERIAL REMAINING IS .035" LT LOWER WEB IS IN SERVICEABLE CONDITION WITH TO NR REMAINING THICKNESS OF 0.035" IAW SRM 53-11-10-201-003-A01. APPLIED A023 PROTECTIVE COATING TO REWORKED AREA IAW SRM 53-11-10-201-003-A01 AND ARM 51-21-16-001-001.