Service difficulty report · Frame · Cndair CL6002C10

Difficulty date
December 11, 2015
Submitted
April 22, 2016
Operation
General aviation
Make and model
Cndair CL6002C10
Aircraft time
1 hours
Engine
Ge CF348C1
Part
Frame
Part number
SH67031357
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 CHECK CORROSION WAS FOUND IN AVIONICS BAY ON ATTACHED FLANGE OF 5EA FRAMES. REMOVAL OF CORROSION WAS PERFORMED IAW SRM 51-21-06, AFTER BLEND OUT NDT INSPECTION FOR CRACKS AND REMAINING THICKNESS WAS PERFORMED WITH NO FINDINGS. FOR DETAILS OF DAMAGE LOCATIONS AND THICKNESSES OF MULTIPLE LOCATIONS PLEASE SEE PHOTOS BELOW. ITEM MINIMUM THICKNESS IS LISTED IN TABLE (PAGE 2). AS PER SRM 53-21-06-101-006-A01 NO DAMAGE PERMITTED - DAMAGE IS NOT ALLOWED WITHIN A 2D RADIUS OF A FASTENER, WHERE D IS THE DIAMETER OF THE FASTENER.