Service difficulty report · Pump · Cndair CL6002D24

Difficulty date
November 2, 2003
Submitted
January 5, 2004
Operation
General aviation
Make and model
Cndair CL6002D24
Engine
Ge CF343B1
Part
Pump
Part number
N6521123
Condition
Failed
Location
Hyd System
Stage of operation
CR
How discovered
O
Nature of condition
K, M, J
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) AFTER T/O, CREW NOTICED ENG NOISES WERE ROUGH. AUDIO CK AT AFT BLKHD IND RT ENG. NO ABNORMAL IND, AT 15,000 FT DURING PRESS CHECKS, HYD 2LO PRESS AMBER MSG POSTED ON AND OFF. ENG FLOW LINE WAS GREEN/AMBER ON AND OFF, 2800 PSI. QTY WAS NML, TEMP OF 47 DEG C, HYD NR 1 TEMP WAS AT 11 DEGREES C. THRUST WAS REDUCED TO IDLE ON RT ENG, HYD PRESS DROPPING TO 2600 PSI, TEMP INCREASING. CREW PERFORMED ENG SHUT DOWN, QTY DROPPED TO ZERO, ROUGH ENG NOISE DISAPPEARED. A/C LANDED W/O INCIDENT. HYD FLUID WAS LEAKING FROM BELLY NEAR AFT EQUIP BAY. FOUND PRES LINE FROM ENG DRIVEN PUMP WITH CRACK INSIDE ELBOW WHICH CAUSED IND AND DEPLETED SYS OF FLUID. INDICATES PUMP IS AT FAULT AND CAUSED VIB CRACKING LINE.