Service difficulty report · Angle · Cndair CL2151A10

Difficulty date
September 14, 1998
Submitted
March 26, 2000
Operation
General aviation
Make and model
Cndair CL2151A10
Part
Angle
Part number
21531033800
Condition
Cracked
Location
Rt Wing
Part time
2,750 hours
Stage of operation
IN
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

(CAN) WHILE DOING AD CF-97-07 OF WING-TO-FUSELAGE FITTINGS, A CRACK WAS FOUND ON THE RIGHT HAND FORWARD OUTBOARD ANGLE AT THE LOWER 3 FASTENER HOLE LOCATION. THE CRACK WAS VISIBLE TO THE NAKED EYE. CRACK EXTENDED FROM THE CENTER OF FASTENER HOLE TO WITHIN .50 INCH FROM THE ANGLE EDGE, AND .1250 INCH THROUGH THE OTHER SIDE OF FASTENER HOLE. AIRCRAFT HAD 375 HOURS SINCE LAST INSPECTION OF THIS AD.