Service difficulty report · Turbine Blades · Airbus A300*

Difficulty date
November 4, 2010
Submitted
December 13, 2010
Operation
Air carrier
Aircraft
N18315
Make and model
Airbus A300*
Aircraft serial
823
Aircraft time
13,780 hours, 3,800 cycles
Engine
Ge CF34*
Engine time
13,780 hours, 3,800 cycles
Part
Turbine Blades
Condition
Failed
Location
Nr 1
Stage of operation
CL
How discovered
O
Nature of condition
X, J
Precautionary procedure
A

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

What was found

(B-18315) DURING CLIMB TO 12,000 FT. A "BANG" SOUND WAS HEARD AND ENGINE 1 FAILED. CREW FOLLOWED QRH AND PERFORMED IFSD, THEN SHOWED MSGS: ENG 1 EGT EXCEEDED DURING AIR START; ADVISORY ENG1 N1 VIBRATION; ENG 1 EGT OVER LIMIT. ACFT AIR TURNED BACK. VISUAL INSP FOUND METAL CHIPS IN THE TAIL PIPE. REMOVED ENGINE IAW AMM 72-00-00. GE HAS BEEN ASSISTING IN THE INVESTIGATION FOR THE DAMAGE CAUSE, AND RECOMMENDED TO HAVE PROTECTIVE COATINGS APPLIED TO HPT BLADES WHEN ROUTED FOR REPAIR, OR REPLACED WITH COATED BLADES IF THE REMOVED BLADES ARE SCRAPPED. FURTHER RECOMMENDATIONS WILL BE PROVIDED ONCE THE ROOT CAUSE HAS BEEN VERIFIED.