Service difficulty report · Blades · Cndair CL6002D24

Difficulty date
August 27, 2007
Submitted
October 24, 2007
Operation
General aviation
Make and model
Cndair CL6002D24
Aircraft time
5,525 hours
Engine
Ge CF34*
Part
Blades
Condition
Damaged
Location
Nr 1 Engine
Part time
6,692 hours
Stage of operation
TX
How discovered
O
Nature of condition
C
Precautionary procedure
O

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

(CAN) ON WALK AROUND ON THE RAMP, IT WAS DISCOVERED THAT NR 1 ENGINE HAD BLADE AND STATOR DAMAGE CAUSED BY UNKNOWN FOD. THE A/C WAS TAXIED TO THE HANGER FOR INSPECTION AND BOROSCOPE. THE INSPECTION REVEALED THAT NR 14 BLADE HAD A SMALL DENT, FURTHER INVESTIGATION REVEALED DAMAGE AT THE 1ST STAGE STATOR AT THE 5 O-CLOCK POSITION AND A PUNCTURE TO THE ENGINE LINER. (APPROX 1.4X1.0 HOLE JUST AFT THE NR1 FAN AND JUST FORWARD OF STATOR AT APPROX 4 O’CLOCK POSITION LOOKING AFT.) DUE TO THE SKIN CONTAINMENT DAMAGE 1 INCH X .40 , MM DOES NOT ALLOW FOR ANY DAMAGE IN THIS AREA. ENGINE CHANGE HAS BEEN C/O. PRESENT A/C HOURS:6692:52 AND CYCLES:3126.