Service difficulty report · Processor · Airbus A300F4605R

Difficulty date
March 14, 2015
Submitted
March 17, 2015
Operation
Air carrier
Aircraft
N681FE
Make and model
Airbus A300F4605R
Aircraft serial
799
Aircraft time
218 hours, 12,021 cycles
Part
Processor
Condition
Malfunctioned
Stage of operation
CR
How discovered
O
Nature of condition
J, G
Precautionary procedure
O

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

What was found

MULTIPLE FAILURES ON LIFT OFF, NR 1 ADC NR 1 FLIGHT DIRECTOR, NR 1 PITCH TRIM, AUTO FEED FAULT, TRIM TANK PUMPS FAIL, LT INNER TANK PUMP FAIL 2 FAIL, RT INNER TANK 1 FAIL, CAPTAIN`S ALPHA HEAT FAULT, CAPTAIN`S STAT HEAT FAULT, GROSS WT & CG FEEDBACK ON ECAM, SUSPECT FAULT WITH AIR GROUND SENSOR OR PROXIMITY DETECTOR BOX. CAPTAIN`S ADC & FD SWITCHING REGAINED DISPLAY ON CAPTAIN`S PFD, ON GROUND STAND BY PROBE OVERHEAT CAME ON. PERFORMED A DISPLAY TEST ON MTP PANEL & FOUND THE FOLLOWING 3 FAIL RECORDS, 1A 28 VDC POWER LOSS, 1B MTP FAIL, 2A FCC 1 FAIL, 2B FCC 2 FAIL & 3 FCU FAIL. FOUND DC ESSENTIAL ON BATTERY WARNING DISPLAY ON OVERHEAD & ON ECAM. PERFORMED BITE TEST ON PROX DET UNIT & FOUND ONLY ONE FAULT LOGGED, FAULT 70. SCANNED SENSORS & ALL COME UP GREEN. RESET BOX & DOWN POWERED ACFT, NO CHANGE IN THE MULTIPLE FAILURES IN COCKPIT. REMOVED AND REPLACED PROXIMITY DETECTOR PROCESSING UNIT (54GB) REF AMM32-31-71-04. BITE CHECK GOOD. AMM: SMP SEE WRI 24-30/3328 FOR ELECTRICAL PROBLEM S IGNOFF. PERFORMED ADJ/TEST AND OPS CHECKED ADC, NR 1 FLIGHT DIRECTOR, NR 1 PITCH TRIM, AUTO FUEL FEED SYSTEM, TRIM TANK PUMPS, LH INNER TANK PUMP NR 2, RT INNER TANK PUMP NR 1, CAPTAIN`S ALPHA HEAT, CAPTAINS STATIC HEAT AND CGCC SYTEMS.

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