Service difficulty report · Thermocouple · Airbus A319132

Difficulty date
April 14, 2003
Submitted
April 23, 2003
Operation
Air carrier
Aircraft
N820AW
Make and model
Airbus A319132
Aircraft serial
1397
Aircraft time
8,450 hours, 3,269 cycles
Engine
Iae V2500A1
Part
Thermocouple
Part number
HAD22308
Condition
Defective
Location
Nr 2 Engine
Stage of operation
DE
How discovered
O
Nature of condition
S
Precautionary procedure
O

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

What was found

ON DESCENT WITH AUTO THROTTLE ON 11,000 FT, NR 2 ENGINE SPOOLED NORMALLY TO MAINTAIN MANAGED SPEED, NR 1 ENGINE DID NOT SPOOL FOR 3 TO 4 SECONDS. NR 1 ENGINE WENT TO CLIMB THRUST RESULTING IN SUBSTANTIAL YAW (3 TO 5 DEG) ROLL OF 2 TO 3. ON IDLE DESCENT 6000 FT NR 1 ENGINE FUEL FLOW 800, NR 2 ENGINE 1450 WITH HIGH N1, N2 & EPR. TURNED OFF AUTO THROTTLES, APPROACH & LANDING NORMAL. MX TROUBLESHOT SYS USING TSM 73-00-00-810-877 AND FOUND NR 2 ENGINE IDLING HIGH. MX FOUND FADEC NR 2 A & B FAULTS FOR FUEL TEMP SENSOR (4017KS). REMOVE & REPLACED NR 2 ENGINE FUEL TEMP SENSOR. OPS & LEAK CHECK GOOD. AUTO FLT SYS & FADEC INDICATE NO FAULTS. PERFORMED HIGH POWER ASSURANCE TEST, OPS NORMAL & ALL PARAMETERS MATCH.

More about the Airbus A319-132