SDR SA06072

Service difficulty report · Engine · Airbus A321211

Difficulty date
September 14, 2006
Submitted
September 15, 2006
Operation
Air carrier
Aircraft
N185UW
Make and model
Airbus A321211
Aircraft serial
1666
Engine
Ge CFM56*
Engine time
16,947 hours, 6,310 cycles
Part
Engine
Condition
Shutdown
Location
Nr 2
Stage of operation
CR
How discovered
O
Nature of condition
Y, J
Precautionary procedure
A

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

What was found

FLT1408 - DURING CRUISE, EN ROUTE FROM SFO TO CLT, CREW RECEIVED ECAM MESSAGE "ENG 2 HI TEMP FADEC OVHT" AND "ENG 2 FADEC B FAULT" ALONG WITH OTHER ASSOCIATED FAULT MESSAGES. CIRCUIT BREAKER FOR ENG 2 FADEC TRIPPED, AND MOMENTS LATER, THE NR 2 ENGINE AUTOMATICALLY SHUTDOWN. CREW DECLARED AN EMERGENCY, ADVISED ATC OF SITUATION AND RECEIVED CLEARANCE TO LAS. FLIGHT DIVERTED TO LAS AND LANDED WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS 35 MINUTES. MX FOUND THE NUMBER TWO ENGINE COWL ANTI ICE VALVE CLAMP DISCONNECTED, WITH OBVIOUS HEAT DAMAGE TO THE ECU AND J6 HARNESSES. MAINTENANCE REPLACED THE HARNESSES, AND THE ECU (PRECAUTIONARY). OPERATIONALLY CHECKS OK.

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