Service difficulty report · Valve · Urocop EC120B

Difficulty date
September 15, 2009
Submitted
October 23, 2009
Operation
General aviation
Make and model
Urocop EC120B
Aircraft time
1,440 hours
Engine
Tmeca ARRIU2F
Part
Valve
Part number
EVP310
Condition
Sticking
Location
Servo Control
Component
Servo · Samm
Component part number
SC50911
Stage of operation
NR
How discovered
C
Nature of condition
L
Precautionary procedure
O

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

What was found

(CAN) SERVO CONTROL ISSUES HAVE BEEN RECURRING ON ALL THREE EC120S IN OUR FLEET. THE MOST COMMON PROBLEM OCCURS AFTER INITIAL START UP OF THE DAY WHEN THE PILOT DOES THE HYDRAULIC CUT OFF CHECK (THE SWITCH ON THE COLLECTIVE STICK). THE CYCLIC GOES HARD TO THE LEFT OR RIGHT, DEPENDING ON WHICH SERVO MALFUNCTIONS. WE SUSPECT IT’S A STICKY SOLENOID VALVE ON ONE OF THE LATERAL SERVOS. IT ALSO HAPPENS ON THE FWD SERVO, IN WHICH CASE, THE FORE AND AFT MOVEMENT DOES NOT GET STIFF (AS IT SHOULD) BECAUSE THE SOLENOID VALVE DOES NOT CUT OFF ITS HYDRAULIC PRESSURE. IN ALMOST ALL CASES, ALL THE PILOT HAS TO DO IS LET THE AIRCRAFT WARM UP FOR 10-15 MIN AND CYCLE THE SWITCH A DOZEN TIMES UNTIL THE SYSTEM IS BACK TO NORMAL. ON THE 15 SEPT. 2009, THE PILOT COMPLAINED THAT THE CYCLIC WAS GOING HARD LEFT DURING THE “CUT OFF CHECK”. THE “SWITCH CYCLING” TECHNIQUE WOULDN’T WORK SO THE HELICOPTER WAS GROUNDED UNTIL AN ENGINEER COULD BE DISPATCHED TO ASSESS THE SITUATION. ONE OF THE SERVO SOLENOID VALVES WAS REPLACED WITH NO CHANGE IN SYMPTOMS (DIDN’T KNOW IF IT WAS THE LEFT OR RIGHT SO HE JUST PICKED ONE). WHILE THE AIRCRAFT WAS STILL RUNNING, HE TAPPED THE SOLENOID VALVES AND THE SYSTEM IMMEDIATELY STARTED TO FUNCTION PROPERLY. THE SYSTEM WAS TESTED NUMEROUS TIMES AFTERWARD AND FUNCTIONED PROPERLY. (TC# 20090918001)

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