Service difficulty report · Frame · Cndair CL6002C10

Difficulty date
September 2, 2010
Submitted
September 7, 2010
Operation
Air carrier
Aircraft
N616QX
Make and model
Cndair CL6002C10
Aircraft serial
10128
Aircraft time
18,356 hours, 13,502 cycles
Engine
Ge CF34*
Part
Frame
Condition
Corroded
Location
Bs 349
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

C-CHECK - DURING INSP, FOUND CORROSION ON FRAME AT FS349 ON ATTACH ANGLE LOCATED JUST FWD OF ATTACHMENT ANGLE 26R. REMOVED RIVETS FROM ATTACH ANGLE IAW SRM 51-42-06-001-001-A01. BLENDED CORRODED AREAS ON WEB AND ATTACH FLANGE IAW SRM 51-21-06-001-001-A01. BLENDED AREA MEASURES 2.5"W 0.9"L .002"D, ORIGINAL THICKNESS IS 0.50", REMAINING MATERIAL ON WEB IS 0.48", WITHIN LIMITS OF SRM 53-21-06-101-006-A01. BLEND ON ATTACH FLANGE MEASURES 3.0"W 0.6"L .002"D, ORIGINAL THICKNESS IS 0.50", REMAINING MATERIAL IS 0.48", WITHIN LIMITS OF SRM 53-21-06-101-006-A01. TREATED, PRIMED AND PAINTED BLENDED AREAS IAW SRM51-21-11-001-001-A01, 51-21-06-001-001-A01 AND 51-25-16-001-001-A01. INSTALLED SOLID FASTENERS IAW SRM 51-42-06-001-001-A01. TOPCOATED AND APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-25-16-001-001-A01 AND 51-21-11-001-001-A01.