Service difficulty report · Bulkhead Web · Cndair CL6002B19

Difficulty date
February 16, 2012
Submitted
September 14, 2015
Operation
General aviation
Make and model
Cndair CL6002B19
Part
Bulkhead Web
Condition
Cracked
Location
Bs 621
Stage of operation
NR
How discovered
9
Nature of condition
O
Precautionary procedure
O

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

(CAN) FUSELAGE BS 621 PRESSURE BULKHEAD WEB ASSY DURING INSPECTION IAW REF/C/MRM AND REF/D/AD AT THE LINE MAINTENANCE, FOUND 1 CRACK INDICATION. THE CRACK INDICATION IS DETECTED BY REF B, NDT METHOD, - D 0.008", L 0.680" + ALPHA, ALPHA MEANS THAT THE LOWER END OF THE CRACK IS UNABLE TO BE DETECTED DUE TO INTERFERENCE WITH EXISTING DOOR CAM TRACK. HOWEVER, THE CRACK INDICATION DID NOT PROPAGATE PORTION OF UNDERNEATH CAM TRACK. THE INDICATION EXCEEDED ALLOWABLE LIMIT. ACFT PERFORMED A FERRY FLIGHT TO REPAIR FACILITY.