Service difficulty report · Drag Angle · Cndair CL6002C10

Difficulty date
February 28, 2011
Submitted
March 4, 2011
Operation
Air carrier
Aircraft
N754EV
Make and model
Cndair CL6002C10
Aircraft serial
10173
Aircraft time
16,727 hours, 11,555 cycles
Part
Drag Angle
Condition
Cracked
Location
Vertical Stab
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

LEFT VERTICAL STAB DRAG ANGLE CRACKED AT AFT END. PERFORMED EDDY CURRENT INSP ON LT SIDE FWD VERTICAL STAB DRAG ANGLE IAW NDT INSP PROCEDURES ET-2. VERIFIED DRAG ANGLE IS CRACKED AT AFT ENG. CRACK IS .65IN IN LENGTH. CUT AND REMOVED DAMAGE AT LT VERTICAL STAB DRAG ANGLE AND REMOVED BURRS IAW STEPS 1 AND 2 OF REO 670-55-31-018. PERFORMED EDDY CURRENT INSP, STEP (3) OF REO 670-55-31-018 IAW NDTM PT 1, 51-20-006-250-A01. NO CRACK NOTED AT THIS TIME. FABRICATED REPAIR DOUBLER AND FILLER, CORROSION TREAT AND PRIMER IAW REO670-55-31-018. FABRICATED A REPAIR DOUBLER AND FILLER, CORROSION TREATED AND PRIMED IAW REO 670-55-31-018. INSTALLED REPAIR IAW REO 620-55-31-018.