Service difficulty report · Angle · Cndair CL6002C10

Difficulty date
April 19, 2009
Submitted
April 20, 2009
Operation
Air carrier
Aircraft
N601QX
Make and model
Cndair CL6002C10
Aircraft serial
10009
Aircraft time
19,374 hours, 14,397 cycles
Part
Angle
Condition
Cracked
Location
Vertical Stab
Stage of operation
IN
How discovered
9
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

THE AFT CONNECTING ANGLE ON THE LT SIDE FOR THE VERT STAB TO THE FUSELAGE IS CRACKED AT THE FWD END APPROX. .75 INCH AT VERTICAL STAB STRINGER DATUM 67.5 PERCENT. HFEC IAW NDTM PART 1, 51-20-006 CONFIRMED AND MARKED CRACK. MAPPED AREA FOR ENGINEERING. REMOVED FASTENERS FROM AFFECTED AREA AND COMPLIED WITH REO 670-53-84-094 NOTE 1,2. HFEC CUT LINE EDGES AND UNDERLYING STRUCTURES IAW REO 670-53-84-094 NOTE 3, NO CRACKS NOTED. FABRICATED REPAIR DOUBLER AND FILLER ANGLES AS PER REO 670-53-84-094 SHEET 2 STEPS 4-7. HFEC IAW NDTM PART 1, 51-20-006 AT RADIUS NO CRACKS NOTED. INSTALLED DOUBLER AND FILLER ANGLE IAW REO 670-53-84-094 AND CRJ SRM 51-25-01.