Service difficulty report · Line · Cndair CL6002C10

Difficulty date
August 19, 2002
Submitted
August 30, 2002
Operation
Air carrier
Make and model
Cndair CL6002C10
Engine
Ge CF348C1
Part
Line
Part number
CN6272003001
Condition
Cracked
Location
Hyd System
Stage of operation
CR
How discovered
O
Nature of condition
K, J
Precautionary procedure
O

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

What was found

(CAN) DURNING FLIGHT, PILOT REPORTED A HYD. SYSTEM NR 1 FAILURE. FLUID AND PRESSURE WENT TO ZERO. AFTER FURTHER INVESTIGATION IT WAS DISCOVERED THAT THE PRESSURE LINE FROM THE EDP WAS THE CAUSE OF THE LOSS OF FLUID. A/C TAT IS 2,110.6 AND TAC IS 1,809.HYD. LINE LOOKS TO BE IN GOOD CONDITION BUT WAS STATED THAT THE FLUID WAS LEAKING OUT FROM THE WELDED AREA ON THE END OF THE LINE. ALSO STATED THAT IT JUST WASN`T LEAKING AT ONE POINT BUT AROUND THE WHOLE WELDED AREA.