Service difficulty report · Resolver · Airbus A320231

Difficulty date
February 8, 2001
Submitted
February 12, 2001
Operation
Air carrier
Aircraft
N645AW
Make and model
Airbus A320231
Aircraft serial
238
Aircraft time
28,348 hours, 12,978 cycles
Engine
Iae V2500A1
Engine time
32,386 hours, 14,953 cycles
Part
Resolver
Condition
Malfunctioned
Location
Fuel Flow
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

MAINTENANCE TROUBLESHOT IAW TSR 73-22-00-810-851 AND IAE TELEX; CELL CODE FAULT OF 59 ON FMU/HC/EEC 1 MESSAGE; (WFXCF) FUEL FLOW RESOLVER FAULT; CH B ON CONNECTOR J8 HAD HIGH RESISTANCE OF 104 OHMS BETWEEN PINS I & J (NORM: 15-78 OHMS); WIRING CHECKED GOOD; RANG OUT FMU RESOLVER ON CHANNEL B; (CONNECTOR 4000KC-C) AND RESOLVER WAS READING 82 OHMS; FOUND TCA VLV/HC/EECI MESSAGE IN GROUND SCANNING FADEC TEST; BLEED SYSTEM TESTS WERE PERFORMED - CHECKED GOOD. THE FOLLOWING COMPONENTS WERE REPLACED DUE TO TROUBLESHOOTING PROCEDURES IN ADDITION TO THE FMU: NR 1 ENG EEC P/N 798300-15-052 S/N 25000156 - HAMILTON STANDARD - TT 23201, TC 10818, TSR 2807 NR 1 ENG TCA.

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