Service difficulty report · Ecu · Airbus A300F4605R

Difficulty date
August 29, 2008
Submitted
February 3, 2009
Operation
Air carrier
Aircraft
N681FE
Make and model
Airbus A300F4605R
Aircraft serial
799
Aircraft time
13,647 hours, 7,422 cycles
Engine
Ge CF680C2A5F
Part
Ecu
Part number
1820M99P08
Part serial
LMDD7467
Condition
Failed
Location
Nr 2
Part time
13,041 hours, 7,109 cycles
Stage of operation
CL
How discovered
O
Nature of condition
J
Precautionary procedure
A

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

What was found

DURING CLIMB NR 2 ENG N1, FF, EGT BECAME UNSTABLE, ASSOCIATED WITH ENGINE SURGING. FADEC GRD TEST, FOUND FAULT CODE 352-21 ON CH A. N1 SPEED SENSOR PERFORMED TSM PROCEDURE 73-21-30 352-21 FIG 102 SHEET 28. CHECKED BOTH CH A AND B SYS GOOD. SPEED SENSOR IS 116 OHMS AT THE HARNESS. THE ECU CHECKED BAD PER STEP 12. REMOVED AND REPLACED ECU IAW AMM 73-21-01-4 05. ENGINE RUN AT HIGH POWER IAW JRH. ALL INDICATIONS STABLE. NO FAULT CODES AFTER RUN. ITEM CLEARED

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