Service difficulty reports · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR QMLA2013021313034Fuel Control · malfunctionedAT APPROX 1030 AM WHILE STARTING AN APPROACH INTO THE HOSPITAL. HAD A PRONOUNCED YAW FOLLOWED BY THE NR 2 ENGINE LOW LIGHT COMING ON, OBSERVED THE ENGINE RPM CLIMB TO 110 PERCENT AND DROP OFF, ENGINE RPM FELL BELOW 20 PERCENT AS WELL. AUDIBLE WARNING WAS GOISDR QMLA2013021313027Engine · failedAT START OF APPROACH, HAD A PROUNOUNCED YAW FOLLOWED BY NR 2 ENGINE LOW LIGHT COMING ON, OBSERVED ENGINE RPM CLIMB TO 110 PERCENT AND DROP OFF, ENGINE RPM FELL BELOW 20 PERCENT AS WELL. AUDIBLE WARNING ACTIVATED, LOST NR 2 ENGINE. DIVERTED TO AIRPORT AND EXECSDR QMLA2012051312078Unknown · odorROLL CSAS LIGHT ILLUMINATED AND AN ACRID ODOR FOLLOWED. ROLL CSAS CIRCUIT WAS DISENGAGED AND THE ODOR WAS NO LONGER PRESENT. RETURNED TO BASE. TROUBLESHOOTING FOUND NO DISCREPANCIES WITH ACFT, GROUND TURNED ACFT AND THEN A MX TEST FLIGHT WAS ACCOMPLISHED WITSDR QMLA2011010911004Starter Gen · defectiveNR2 STARTER/GENERATOR CAUSING IRREGULAR AMPERAGE SPIKES ON AMMETER DURING NORMAL FLIGHT. MOMENTARILY KICKED OFF NR1 GENERATOR. FOUND FAULTY STARTER/GENERATOR UPON EXAMINATION. STARTER BRUSHES WERE WORN BEYOND SERVICEABLE LIMITS AND IRREGULAR BRUSH WEAR NOTEDSDR QMLA2010110810074Sliding Sleeve · debondedUPON AIRWORTHINESS INSPECTION IN THE MORNING, THE MECHANIC FOUND THAT THE MAIN ROTOR SWASHPLATE SLIDING SLEEVE TEFLON BUSHING HAD TEFLON LINER DEBONDED FROM BUSHING AND WAS WORKING ITS WAY OUT OF THE LOWER PORTION OF THE SLIDING SLEEVE ASSEMBLY AND THUS AFFECTSDR QML2ML00281Skin · dentedDAMAGE FOUND NEAR THE RT REAR JACK POINT STA 5000MM AND DAMAGE LT OF CTR LINE APPROX 370MM AT STA 4750 MM.SDR 720110122007Starter Gen · out of adjustEXTREMELY FAINT ELECTRICAL BURNING ODOR DETECTED. ASKED TRANSPORT TEAM IF THEY DETECTED ODOR AND THEY INDICATED THAT THEY DID NOT. PILOT NOTICED NR 2 GENERATOR AMP GAUGE INDICATING APPROXIMATELY 50 AMPS WHILE NR 1 GENERATOR AMP GAUGE INDICATED APPROXIMATELY 10SDR 7201Fitting · crackedWHILE PERFORMING A LIFENET AAIP INSPECTION, THE MECHANIC FOUND A .7500 INCH (APPROX) CRACK EXTENDING FROM THE UPPER LEFT HAND T/R GEARBOX MOUNT HOLE INBOARD THROUGH AN ADJACENT RIVET HOLE TERMINATING AT A CORNER FILLET, ON THE MOUNT FITTING FOR THE TAIL ROTOR SDR A1U2003F00001Structure · crackedWHILE PERFORMING A DAILY INSP, MECHANIC FOUND A .5000 INCH CRACK EXTENDING PAST THE LEADING EDGE FAIRING FOR THE HORIZONTAL STABILIZER, THE CRACK WAS IN THE TAILBOOM OF THE AIRCRAFT, AFTER REMOVING THE FAIRING FOR FURTHER INSPECTION, IT WAS DETERMNED THAT CRACSDR A1U2002F00001Pump · failedAFTER TAKEOFF, AFT FUEL TRANSFER PUMP LIGHT ILLUMINATED. CIRCUIT BREAKER WAS PULLED AND RESET. SWITCH WAS CYCLED. PROBABLE CAUSE, BEARINGS SEIZED.SDR A1UR135HGovernor · failedPILOT REPORTED ENROUTE TORQUE SPLITS BETWEEN ENGINE. AC MADE SCHEDULED LANDING AT HOSPITAL. PILOT ATTEMPTED TO START NR 2 ENGINE, ENG WOULD NOT ACCELERATE BEYOND 42% NG SPEED. UPON INSP OF ENGINE AND COMPONENTS, TECH DISCOVERED NP GOVERNOR SHAFT SEIZED, REPSDR 99ZZZX1542Frame · crackedDURING ROUTINE TAIL BOOM INSPECTION, FOUND FRAME 10L CRACKED ALL THE WAY THROUGH. REPORTED DISCREPANCY TO AMERICAN EUROCOPTER. AMERICAN EUROCOPTER SENT TECH REP TO REMOVE FRAME 10L AND INSTALL NEW FRAME.
Other aircraft with N211SL · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. N211SL is registered now to the first aircraft listed.