Service difficulty report · Drag Angle · Cndair CL6002B19

Difficulty date
December 1, 2010
Submitted
December 3, 2010
Operation
Air carrier
Aircraft
N878AS
Make and model
Cndair CL6002B19
Aircraft serial
7590
Aircraft time
20,873 hours, 17,955 cycles
Engine
Ge CF34*
Part
Drag Angle
Condition
Cracked
Location
Airstair Door
Stage of operation
IN
How discovered
E
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

ASD HAS A SUSPECT CRACK ON THE AFT UPPER DRAG ANGLE. FILL STOP DRILL HOLE WITH SEALANT IAW SRM 51-12-00. EVALUATED CRACK TO AFT DRAG ANGLE AND FOUND TO BE OUT OF LIMITS. SUBMITTED DAMAGE REPORT TO STS ENGINEERING FOR DISPOSITION. COMPLIED WITH NDT IAW NDTM 51-20-06, PART 1. CONFIRMED DRAG ANGLE IS CRACKED AND MARKED LOCATION FOR MEASUREMENT. JOB COMPLETE. STOP DRILLED CRACK IAW SRM 51-12-00 AND TREAT IAW SRM 51-21-16, EA 1-2010-206, MIL-STD-6866 IAW EA 1-2020-206, CRACK HAS BEEN CONTAINED. FILL STOP DRILL HOLE WITH SEALANT IAW SRM 51-12-00.