Service difficulty report · Compressor · Airbus A300F4605R

Difficulty date
March 17, 1998
Submitted
March 26, 2000
Operation
Air carrier
Aircraft
N654FE
Make and model
Airbus A300F4605R
Aircraft serial
738
Engine
Ge CF680C2A5
Part
Compressor
Condition
Burned
Location
Nr 2 Engine
Stage of operation
TO
Nature of condition
A, J
Precautionary procedure
C, F, D

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

What was found

REJECTED T/O AT APPROX 120 KTS, (18R MEM) DUE TO FIRE ON NR 2 ENGINE. AFTER BOTH BOTTLES WERE FIRED THE FIRE WENT OUT. A/C NOT EVACUATED EMERGENCY CREW CONFIRMED NO FURTHER SMOKE. FOUND HOLE BURNED THROUGH REAR COMPRESSOR STAGE AT 8 O'CLOCK FUEL NOZZLE POSITION. *S/D* INSPECTED WHEELS AS PER 32-41-00-6, NO DEFECTS NOTED SKS 197864. FOUND HOLE BURNED THROUGH REAR COMPRESSOR STAGE AT EIGHT O'CLOCK FUEL NOZZLE POSITION. JOB PROGRESS FORM STARTED. REMOVED AND REPLACED NR 2 ENG IAW W/C 64T0700. LEAK AND OPS CHECK GOOD IAW SNRD NR 390843. REMOVED AND REPLACED FAN AIR VALVE IAW M/M 36-11-16-4.

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