Service difficulty report · Drag Angle · Cndair CL6002C10

Difficulty date
January 19, 2009
Submitted
January 23, 2009
Operation
Air carrier
Aircraft
N717EV
Make and model
Cndair CL6002C10
Aircraft serial
10088
Aircraft time
15,421 hours, 10,325 cycles
Part
Drag Angle
Condition
Cracked
Location
Fuselage
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

RT DRAG ANGLE (VERTICAL - FUSELAGE) APPEARS CRACKED. PERFORMED REPAIR TO CRACKED LT DRAG ANGLE (VERTICAL FUSELAGE) AS PER REO 670-55-31-018 STEPS 1-5. PERFORMED EDDY CURRENT INSPECTION DRAG ANGLE IAW NDTM 51-20-006. ANGLE IS CONFIRMED CRACKED AND MARKED. CUT OUT DAMAGED AREA. COMPLIED WITH NDT OF CUTLINE PER STEP 3 OF REO 670-53-31-018. FABRICATED DOUBLER AND FILLER FOR LT DRAG ANGLE REPAIR IAW REO 670-55-31-018. INSTALLED ALL REPAIR PARTS AND FASTENERS EXCEPT 2 EA FASTENERS ON FWD EDGE OF BOTTOM LEG OF DRAG ANGLE.