Service difficulty report · Line · Cndair CL6012A12

Difficulty date
March 23, 2007
Submitted
May 1, 2007
Operation
General aviation
Make and model
Cndair CL6012A12
Aircraft time
14,929 hours
Engine
Ge CF348E5A1
Part
Line
Part number
600752406
Condition
Failed
Location
Hyd System
Part time
15,054 hours
Stage of operation
IN
How discovered
V
Nature of condition
K
Precautionary procedure
K

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

What was found

(CAN) DURING ROUTINE SERVICING AFTER A/C ARRIVAL, HYD FLUID WAS NOTICED LEAKING OUT OF THE BOTTOM OF THE RUDDER AND RUNNING DOWN THE TAILCONE AND TO THE GROUND. PANELS WERE REMOVED TO LOCATE THE LEAK, FIGURING THAT THERE WAS A BAD RUDDER PCU LEAKING. WHAT WAS FOUND IT WAS THE NR 3 HYDRAULIC RETURN SYSTEM LINE P/N 600-75240-6 CHAFED THREW AT THE BOTTOM OF THE HORIZONTAL STAB REAR SPAR. 3 MONTH PREVIOUS A 15,000 HOUR INSP WAS C/O AND THE CENTER BOTTOM HINGE BEARING WAS FOUND WORN OUT, SO THE HOLE BRACKET ASSY WAS REPLACED. TO REPLACED THIS BRACKET THE HYD LINE OF THE NR 3 RETURN SYSTEM HAD TO BE DISASSEMBLE TO GAIN ACCESS TO THE BRACKET. WHEN THE RUDDER WAS REMOVED TO DO THE REPAIR, AS THIS LINE IS ON THE REAR SP