Service difficulty report · Frame · Cndair CL6002B19

Difficulty date
April 23, 2004
Submitted
June 4, 2004
Operation
General aviation
Make and model
Cndair CL6002B19
Aircraft time
10,579 hours, 8,503 cycles
Engine
Ge CF343B1
Part
Frame
Part number
601360012930
Condition
Cracked
Location
Fuselage
Part time
10,579 hours
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 COMPLETION OF AD CF-2003-12/A DVI OF AFT FUSELAGE AND REINFORCING ANGLE AT FS640 ON BOTH LT AND RT SIDES BETWEEN STRINGERS 9 AND 12 IAW PART A OF MFG SB601-53-061, RT SIDE REINFORCEMENTS PLATE WAS FOUND CRACKED APPROX .8750 INCH LONG AND CORRESPONDING CRACK WAS FOUND ON THE FRAME AT THE UPPER CORNER OF THE ENGINE SUPPORT BEAM APPROX. .6875 INCH LONG. IAW SB601R-53-061 WORK PROGRESSED TO PART B STEP E ITEM NR 4. EDDY CURRENT HAS BEEN PERFORMED WITH NO CRACKS FOUND ON SKIN DOUBLER. WORK IS CONTINUING IAW SB AND WILL BE REPORTED AS SOON AS MORE INFORMATION BECOMES AVAILABLE .