Service difficulty report · Fitting · Cndair CL6002C10

Difficulty date
September 10, 2015
Submitted
April 22, 2016
Operation
General aviation
Make and model
Cndair CL6002C10
Engine
Lyc ALF502L2C
Part
Fitting
Condition
Corroded
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

(CAN) DURING INSPECTION OPERATOR FOUND CORRODED FRAME FOOT FROM FS295.00 TO FS333.00 BETWEEN STR 25L AND 25R. OPERATOR PERFORMED BLEND OUT OF CORRODED AREAS IAW SRM AND PERFORMED HFEC FOR CRACK IN BLENDED AREAS WITH NO FINDINGS. BLENDED AREAS AT: FS295.00, LOCATION A FS310.00 LOCATION A, B, C, FS333.00 LOCATION A, B, C, D, E ARE OUT OF ALLOWABLE LIMITS IAW SRM 53-21-06, PB 101.