Service difficulty report · Computer · Cndair CL6002B19

Difficulty date
December 30, 2002
Submitted
January 21, 2003
Operation
Air carrier
Make and model
Cndair CL6002B19
Engine
Ge CF343A1
Part
Computer
Condition
Malfunctioned
Location
Fuel Control
Stage of operation
CR
How discovered
O
Nature of condition
S
Precautionary procedure
E, A

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

What was found

(CAN) IN FLIGHT SHUTDOWN OF RT ENGINE DUE TO REOCCURANCE OF UNCONTROLLED FUEL IMBALANCE. CREW RECEIVED 'XFLOW/APU PUMP EICAS AMBER MESSAGE AFTER TAKEOFF, AFTER APU WAS SHUTDOWN'. ALSO HAD 'RT XFLOW SOV FAIL MESSAGE. REPLACEMENT OF : RT COMPENSATOR PROBE. RT CROSSFLOW SOV, APU NEG. GRAVITY RELIEF VALVE, AND APU/XFLOW FUEL PUMP CART. DURING ATTEMPTED FUNCTION CHECKS MAINT FOUND THE XFLOW/APU PUMP WAS ON BUT NO SHUTOFF VALVE WAS OPEN TO MOVE FUEL. LINE FROM PUMP ON FUEL PAGE WAS GREEN BUT ALL VALVES WERE CLOSED. FUEL COMPUTER WAS REPLACED. THIS UNIT WAS TRIED IN ANOTHER A/C AND PRODUCED THE SAME FAULTS. FUNCTION CHECKS FOR ALL REPLACED PARTS AND AFFECTED SYSTEMS WERE COMPLETED AND THE A/C RETURNED TO SERVICE.