Service difficulty report · Ecu · Airbus A300B4605R

Difficulty date
August 29, 2008
Submitted
September 4, 2008
Operation
Air carrier
Aircraft
N681FE
Make and model
Airbus A300B4605R
Aircraft serial
799
Aircraft time
13,647 hours, 7,422 cycles
Engine
Ge CF680
Part
Ecu
Part number
1820M99P08
Part serial
LMDD7467
Condition
Failed
Location
Nr 2 Engine
Stage of operation
CL
How discovered
O
Nature of condition
G, 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. FOLLOWING NR 2 ENG FADEC BITE DISPLAY: BITE CHA CHB 270 84120 84120 271 99080 99080 272 20000 20000 273 274 ON 350-354. FADEC GROUND 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 & 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.

More about the Airbus A300 B4-605R