Aerospatiale ATR 72-212A

Service difficulty reports · 695

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Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'ATR72212A'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR CA151007001Engine · power loss(CAN) THE PILOT REPORTED THAT DURING THE LAST STAGE OF CRUISE AND DURING DESCENT, THEY HAVE EXPERIENCED A REPETITIVE RAPID FLUCTUATION AND TORQUE DROP OF THE ENGINE INSTALLED ON THE LT POSITION WITH YAW MOVEMENT OF THE ACFT. UNEVENTFUL LANDING WAS MADE. TORQSep 26, 2015 · Aerosp ATR72212A · Engine (Turbine/Turboprop)SDR CA151006014Engine · leaking(CAN) OIL ODOR IN CABIN REPORTED DURING DESCENT PHASE OF THE FLIGHT. UNEVENTFUL LANDING COMPLETED. BOROSCOPE INSPECTIONS AFTER 3 ENGINE RUNS REVEALED FRESH AND COOKED OIL IN THE INTERMEDIATE COMPRESSOR CASE. THE OPERATOR WAITING RECOMMENDATION.Sep 24, 2015 · Aerosp ATR72212A · Engine (Turbine/Turboprop)SDR CA151007005Engine · power loss(CAN) CUSTOMER REPORTED THAT WHEN POWER LEVER IS AT TAKEOFF, RT ENGINE WAS UNABLE TO ACHIEVE TAKEOFF POWER WITH NO INCREASE IN TORQUE. FSR PROVIDED TROUBLESHOOTING RECOMMENDATIONS TO CUSTOMER.Sep 22, 2015 · Aerosp ATR72212A · Engine (Turbine/Turboprop)SDR CA150901002Eec · faulted(CAN) TAKEOFF WAS ABORTED DUE TO ELECTRONIC ENGINE CONTROL FAULT OCCURRENCE WHEN POWER LEVER WAS ADVANCED TO TAKEOFF NOTCH. CUSTOMER MONITORED THE SITUATION AND AS THERE WAS NO CHANGE IN ENGINE PERFORMANCE ASSOCIATED WITH THESE F/A, THE ACFT RETURNED TO SERVIAug 21, 2015 · Aerosp ATR72212A · Fuel Controlling SystemSDR CA150820002Engine · power loss(CAN) AT 800FT WITH POWER MNG ON T/O, NR 2 ENGINE SUFFERED A LOSS OF POWER WITH TORQUE INDICATION THAT WENT TO ZERO AND ENGINE NR 1 UPTRIM LIGHT CAME ON. AUTOFEATHER CONDITION HAS BEEN REGULARLY ACTIVATED BY THE ATPCS. EMERGENCY PROCEDURES IAW QRH ENGINE FAIAug 7, 2015 · Aerosp ATR72212A · Engine (Turbine/Turboprop)SDR CA150731002Blade · distressed(CAN) DURING PUSHBACK, AFTER RELEASE PROPELLER BRAKE, PILOT NOTICED ABNORMAL SOUND FROM RT ENGINE. ACFT RETURNED TO BAY AND ENGINE WAS SHUTDOWN. GROUND INSPECTION FOUND PT2 BLADE DISTRESS. THE CUSTOMER PLANS TO PERFORM A BORESCOPE INSPECTION TO DETERMINE THEJul 29, 2015 · Aerosp ATR72212A · Turbine SectionSDR CA150802001Engine · failed(CAN) ACFT WAS PERFORMING TAXIING WHEN PILOTS WERE NOTIFIED THAT FIRE WAS COMING OUT OF NR 2 ENGINE EXHAUST. THE CREW SHUTDOWN THE ENGINE AND ACTIVATED 1ST STAGE FIRE EXTINGUISHER SYS. GROUND CREW CONFIRMED THE PROPELLER DOES NOT ROTATE FREELY AND ENGINE ANJul 28, 2015 · Aerosp ATR72212A · Engine (Turbine/Turboprop)SDR CA150727003Terminal Block · broken(CAN) TAKEOFF ABORTED DUE TO ENGINE NR 1 WARNING LIGHT AND ITT RISE TO 801 DEGREES CELSIUS. TROUBLESHOOTING REVEALED T6 BROKEN TERMINAL BLOCK. PARTS HAS BEEN REPLACED AND THE ACFT IS DECLARED SERVICEABLE POST ENGINE GROUND RUN AND ITT BEING WITHIN LIMITS.Jul 11, 2015 · Aerosp ATR72212A · Engine Indicating System WiringSDR CA150603005Engine · shutdown(CAN) WHILE CRUISING IN FLIGHT, LT ENGINE EXPERIENCED AN INFLIGHT SHUTDOWN. THE PILOT THEN CARRIED OUT THE SINGLE ENGINE OPERATION AND AFTER CONFIRMING NO DAMAGE, FIRE OR SMOKE FROM THE ENGINE, THE PILOT PROCEEDED TO RESTART THE ENGINE SUCCESSFULLY. THE ACFT CMay 21, 2015 · Aerosp ATR72212A · Engine (Turbine/Turboprop)SDR CA150512001Engine · malfunctioned(CAN) ON THE INCOMING FLIGHT, PILOT NOTICED NR 1 ENG WAS 30 DEG C HIGHER. DURING OUTGOING FLIGHT, AFTER POSITIVE LIFT & GEAR UP, APPROX AT 670 FT, LOW OIL PRESS LIGHT CAME ON. PILOT LOWERED THE POWER LEVER TO FLIGHT IDLE. OBSERVED SHARP DROP IN OIL PRESS & Apr 19, 2015 · Aerosp ATR72212A · Engine (Turbine/Turboprop)SDR CA150507004Engine · shutdown(CAN) IN FLIGHT SHUTDOWN OF NR 1 ENGINE WAS REPORTED DURING DESCENT. ACFT LANDED UNEVENTFULLY. NO ANOMALIES WERE FOUND DURING THE BORESCOPE INSPECTION. THE EEC & PEC SHOWED FAULT CODES. TROUBLESHOOTING IS ONGOING.Apr 14, 2015 · Aerosp ATR72212A · Engine (Turbine/Turboprop)SDR CA150410012Engine · fluctuates(CAN) DURING CLIMB, JUST AFTER THE BLEEDS WERE SELECTED ON, THE LT ENG TORQUE STARTED FLUCTUATING. THE PILOT THEN SHUT DOWN THE ENG IAW THE PILOT`S QUICK REFERENCE HANDBOOK & THE ACFT FLEW BACK TO THE AIRPORT & LANDED UNEVENTFULLY. AFTER GROUND INSPECTIONS WApr 9, 2015 · Aerosp ATR72212A · Engine (Turbine/Turboprop)SDR CA150410007Unknown · odor(CAN) REPORTED AN OIL ODOR IN CABIN AND COCKPIT ONLY AT LOW POWER SETTINGS. AFTER THE ACFT LANDED UNEVENTFULLY, THE SMOKE ALARM WAS ACTIVATED. TROUBLESHOOTING ON-GOING.Apr 6, 2015 · Aerosp ATR72212A · Air Distribution SystemSDR CA150325009Engine · power loss(CAN) DURING THE CLIMB PHASE, PASSING 10000FT, THE ENGINE NR 2 TORQUE DROPPED TO 60 PERCENT FROM 86 PERCENT, WITHOUT COMMAND. AFTER 10 SEC THE TORQUE HAS BEEN RESTORED TO NORMAL VALUE. YAW MOMENT PHYSICALLY PERCEIVED DURING THE TORQUE DROP. THE ACFT RETURNED Mar 10, 2015 · Aerosp ATR72212A · Engine (Turbine/Turboprop)SDR CA150306010Autofeather Sys · malfunctioned(CAN) THE AUTOMATIC TAKEOFF POWER CONFIGURATION SYSTEM, ATPCS, DID NOT ARM DURING LINING UP PRIOR TO TAKE OFF. THE TAKEOFF ROLL WAS ABORTED & THE AIRCRAFT RETURNED TO GATE. CUSTOMER INITIALLY ELECTED FOR MINIMUM EQUIPMENT LIST DISPATCHED UNDER ATPCS INOPERATMar 2, 2015 · Aerosp ATR72212A · Propeller Feathering/ReversingSDR CA150306012Eec · malfunctioned(CAN) THE AIRCRAFT TOOK OFF & JUST AFTER RETRACTING THE LANDING GEAR THE NR 2 ENGINE LOST POWER & UP TRIM OF ENGINE NR 1 WAS COMMANDED. AFTER SOMETIME THE ENGINE NR 2 RECOVERED THE POWER AUTOMATICALLY, WITHOUT ANY PILOT ACTION. AIRCRAFT RETURNED TO DEPARTURE Feb 21, 2015 · Aerosp ATR72212A · Fuel Control/Turbine EnginesSDR CA150224018Propeller · malfunctioned(CAN) DURING TAKEOFF, ENGINE NR 1 WENT INTO AN UNCOMMANDED AUTOFEATHER. THE FLIGHT CREW SELECTED POWER MANAGEMENT TO MAINTENANCE AND ENGINE NR 1 RETURNED TO NORMAL OPERATION. UNEVENTFUL LANDING WAS COMPLETED AT AIRPORT OF ORIGIN.Feb 21, 2015 · Aerosp ATR72212A · Propeller Feathering/ReversingSDR CA150224006Engine · malfunctioned(CAN) DURING CRUISE, FLUCTUATION OF TORQUE WAS WITHIN 5 PERCENT. AT TOP OF DESCENT ENGINE NR 2 TORQUE DROPPED TO ZERO AND ITT DROPPED BELOW 350, DEGREE C. THE PILOT COMPLETED IFSD PROCEDURES AND ACCOMPLISHED A SUCCESSFUL SINGLE ENGINE LANDING. MFCU AND FUELFeb 7, 2015 · Aerosp ATR72212A · Engine (Turbine/Turboprop)SDR CA150120018Engine · making metal(CAN) SHORTLY AFTER TAKE-OFF, WHILE GEARS WERE BEING RETRACTED, NR 2 ENGINE TORQUE WENT FROM 90 TO 70 PERCENT. APPROXIMATELY 5 SECONDS LATER, THE TORQUE DROPPED TO 40 PERCENT, THEN TO ZERO. FOLLOWED PROCEDURES AND SAFELY LANDED BACK AIRPORT OF ORIGIN. THE PRELJan 15, 2015 · Aerosp ATR72212A · Engine (Turbine/Turboprop)SDR CA150113002Engine · flamed out(CAN) THE PILOT REPORTED THE ENGINE NR 2 FLAME OUT WITH STRONG NOISE. DURING TROUBLESHOOTING THE MAINTENANCE PERFORMED THE ENGINE VISUAL INSPECTION AT THE POWER TURBINE AND FOUND METAL PARTICLES INSIDE EXHAUST AREA. MAINTENANCE ATTEMPTED TO ROTATE THE PROPELLDec 23, 2014 · Aerosp ATR72212A · Engine (Turbine/Turboprop)SDR CA141217001Oil System · low pressure(CAN) PILOT NOTICED LOW OIL PRESSURE WITH A LOW PRESSURE WARNING ON RT ENGINE DURING CLIMB. PILOT THEN PROCEEDED TO REDUCE POWER AND MAIN OIL PRESSURE STABILIZED AT JUST ABOVE 35 PSI. PILOT ELECTED TO RETURN TO ORIGIN AND AIRCRAFT LANDED UNEVENTFULLY. UPON LANov 30, 2014 · Aerosp ATR72212A · Turbine Engine Oil SystemSDR CA141217003Bearing · damaged(CAN) DURING DECENT, ENGINE NUMBER TWO EXPERIENCED SMALL VIBRATION WHICH INCREASED IN AMPLITUDE UNTIL THE PILOT DECIDED TO SHUT DOWN THE ENGINE. AN UNEVENTFUL LANDING WAS COMPLETED. NO INJURIES REPORTED. UPON INSPECTION AFTER LANDING, PROPELLER BLADE BEARINGS Nov 29, 2014 · Aerosp ATR72212A · Propeller AssemblySDR CA141105003Engine · power loss(CAN) DURING DESCENT FROM FL150 TO FL090 THE NR 2 ENGINE TORQUE DROPPED TO ZERO AND NP DROPPED TO 04 %, THE CREW REDUCED POWER LEVER TO FLIGHT IDLE AND ALL PARAMETERS BECAME NORMAL.Oct 29, 2014 · Aerosp ATR72212A · Engine (Turbine/Turboprop)SDR CA141027005Engine · fire(CAN) AFTER FUEL NOZZLES REPLACEMENT, THE ENGINE SUSTAINED A FIRE EXTERNAL TO THE ENGINE CASING DURING THE FINAL STAGE OF ENGINE RUN. THE RT ENGINE NACELLE COWL WAS OPENED AND THE EXTINGUISHING AGENT WAS DIRECTED TO THE FUEL NOZZLES AREA, TWICE, WITH A VERY LOct 19, 2014 · Aerosp ATR72212A · Engine (Turbine/Turboprop)SDR CA141025007Warning Message · false activation(CAN) AIRCRAFT WAS EN ROUTE WHEN ENGINE FIRE WARNING ON NR 1 ENGINE ILLUMINATED. FLIGHT CREW SHUT DOWN THE ENGINE AND DISCHARGED THE FIRE EXTINGUISHER OF NR 1 ENGINE. AIRCRAFT MADE AN UNEVENTFUL LANDING. CUSTOMER REPORTING NO EVIDENCE OF EXTERNAL FIRE IN THE NOct 14, 2014 · Aerosp ATR72212A · Fire DetectionSDR CA141024005Oil System · leaking(CAN) AFTER TAKEOFF, ENGINE NR 1 OIL ON CAP ILLUMINATED. ENGINE NR 1 OIL PANEL FLUCTUATING BETWEEN YELLOW AND RED BAND. AFTER SELECTING POWER MANAGEMENT TO CLIMB DURING SEQUENCE PROCEDURE, ENGINE NR 1 OIL INCREASED BACK TO GREEN BAND. VISUAL INSPECTION ON NRSep 30, 2014 · Aerosp ATR72212A · Turbine Engine Oil SystemSDR CA141010008Engine · fire(CAN) ON A REVENUE FLIGHT, PILOTS NOTICED A FIRE WARNING FROM NR 1 ENGINE. BOTH FIRE BOTTLES WERE RELEASED AND THE ENGINE WAS SHUTDOWN. THE ACFT WAS DIVERTED BACK TO RAMP AND THE LANDING WAS UNEVENTFUL. DURING THE TROUBLESHOOTING, MECHANICS CONFIRMED THAT TSep 28, 2014 · Aerosp ATR72212A · Engine (Turbine/Turboprop)SDR CA141008004Engine · malfunctioned(CAN) JUST AFTER TAKEOFF, ENGINE NR 1 PRESSURE WARNING CAME ON DURING FLIGHT AND ALL ENGINE PARAMETERS WERE FLUCTUATING. PILOT DID NOT SHUTDOWN THE ENGINE, AND MADE AN UNEVENTFUL LANDING. TROUBLESHOOTING ONGOING.Sep 16, 2014 · Aerosp ATR72212A · Engine (Turbine/Turboprop)SDR CA141006012Turbine · damaged(CAN) IT IS REPORTED THAT DAMAGES WERE OBSERVED ON POWER TURBINE.Sep 14, 2014 · Aerosp ATR72212A · Turbine SectionSDR CA140908013Engine · power loss(CAN) THE OPERATOR HAS INFORMED THAT THE SUBJECT ENGINE LOST POWER AFTER LOUD BANG AND SUBSEQUENTLY THE PILOT SHUTDOWN THE ENGINE. THE CREW PERFORMED UNEVENTFUL LANDING AT ORIGINAL AIRPORT. THE CUSTOMER WILL REPLACE ENGINE.Aug 28, 2014 · Aerosp ATR72212A · Engine (Turbine/Turboprop)SDR CA140908004Engine · power loss(CAN) DURING CLIMB AT 6000 FT APPROXIMATELY, ENGINE NR 2 EXPERIENCED SUDDEN LOSS OF POWER, WITH ENGINE PARAMETERS DECREASE, TQ/ITT/NP FOR THE NH UP TO 68 PERCENT, LEADING TO THE ACFT, VEERING TO THE RT. 15-20 SECONDS LATER, ENGINE NR 2 PARAMETERS CAME BACK TOAug 22, 2014 · Aerosp ATR72212A · Engine (Turbine/Turboprop)SDR CA140721015Line · loose(CAN) ABORTED TAKEOFF. DFDR REVEALED ENGINE ITT AT 804C AND NH 104 PERCENT. TROUBLESHOOTING FOUND BLEED LEAK AT HBOV DUE TO A LOOSE HBOV LINE. REPAIR IN PROGRESS. AWAITING FEEDBACK. IF PAC IS GOOD AC WILL BE RTS TONIGHT.Jul 15, 2014 · Aerosp ATR72212A · Compressor Bleed ControlSDR CA140721013Engine · malfunctioned(CAN) DURING CRUISE, THE PILOT HEARD A LOUD NOISE FROM THE 2 ENGINE FOLLOWED BY WARNING/CAUTION LIGHT FOR OIL INDICATION AND IN-FLIGHT SHUTDOWN. ACFT WAS DIVERTED.Jul 10, 2014 · Aerosp ATR72212A · Engine (Turbine/Turboprop)SDR CA140630019Engine · shutdown(CAN) THE PILOT REPORTED THAT DURING TAKEOFF, THE RT ENGINE NR 2 SHUTDOWN BETWEEN 500 AND 1000 FT. THE ACFT RETURNED TO BASE AND LANDED UNEVENTFULLY. THE PILOT WAS ABLE TO RELIGHT ENGINE PRIOR TO LANDING. THE ENGINE DATA WAS SENT IN TO MFG FOR REVIEW.Jun 20, 2014 · Aerosp ATR72212A · Engine (Turbine/Turboprop)SDR CA140620006Engine · power loss(CAN) DURING START ON GROUND, ON SELECT CONDITION LEVER TO AUTO, COMPRESSOR SPEED (NP) REMAINED AT 56%. THE START WAS ABORTED. DURING THE ENGINE INSPECTION, ONE OF PT2 BLADE WAS FOUND BROKEN. ENGINE WILL BE REMOVED FOR INVESTIGATION AND REPAIR.Jun 11, 2014 · Aerosp ATR72212A · Engine (Turbine/Turboprop)SDR CA140602007Engine · power loss(CAN) ENGINE NR 1 ANALOG TORQUE DROPPED DURING INITIAL TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND UNABLE TO CONFIRM IF UNCOMMANDED AUTOFEATHER TOOK PLACE. ENGINE NR 1 AUTOFEATHER UNIT AND AUTOMATIC TAKEOFF POWER CONTROL SYSTEM, ATPCS, WERE ISOLATED IAW MINIMUApr 29, 2014 · Aerosp ATR72212A · Engine (Turbine/Turboprop)SDR CA140314006Engine · faultedDURING FLIGHT, THE PILOT REPORTED AN ELECTRONIC ENGINE CONTROL FAULT. THE ENGINE WAS FLOWN IN MANUAL MODE AND SUBSEQUENT INTERMITTENT FIRE ALARMS OCCURRED. THE ACFT LANDED SAFELY. POST FLIGHT INSPECTION FOUND EVIDENCE OF BURNING ON THE ENGINE.Mar 8, 2014 · Aerosp ATR72212A · Engine (Turbine/Turboprop)SDR CA140326010Eec · faulted(CAN) DURING FLIGHT, THE PILOT REPORTED AN EEC FAULT. THE ENGINE WAS FLOWN IN MANUAL MODE AND SUBSEQUENT INTERMITTENT FIRE ALARMS OCCURRED. THE ACFT LANDED SAFELY. POST FLIGHT INSPECTION FOUND EVIDENCE OF BURNING ON THE ENGINE. THE ENGINE WILL BE REMOVED AND SMar 4, 2014 · Aerosp ATR72212A · Fuel Controlling SystemSDR CA140312004Engine · unknownTHE PILOT REPORTED NP STAYED AT 100.5 PERCENT DURING INITIAL CLIMB, JUST AFTER TAKEOFF. THE PILOT ELECTED TO SHUTDOWN ENGINE NR 2 AND LANDED SAFELY. NO EEC NOR PEC FAULTS WERE DETECTED. PROPELLER INTERFACE UNIT (PIU) WERE SWAPPED FROM ENGINE NR 1 AND NR 2 FOFeb 22, 2014 · Aerosp ATR72212A · Engine (Turbine/Turboprop)SDR CA140224008Engine · making metal(CAN) DURING FLIGHT, AT APPROXIMATELY 6500 FT, THE PILOT REPORTED A LOUD RUMBLING SOUND FROM NR 2 ENGINE. THE CREW REPORTED FIRE COMING OUT FROM NR 2 ENGINE EXHAUST. THE ENGINE WAS SHUTDOWN AND AN UNEVENTFUL SINGLE ENGINE LANDING WAS PERFORMED AT THE AIRPORT OFeb 15, 2014 · Aerosp ATR72212A · Engine (Turbine/Turboprop)SDR CA140203008Engine · power loss(CAN) DURING GROUND RUN AFTER PERFORMING A FUEL NOZZLE REPLACEMENT, LT ENGINE WAS SET TO TAKEOFF POWER AND PARAMETERS WERE COLLECTED. AFTER REDUCING THE ENGINE NR 1 POWER WHILE IN PREPARATION TO INCREASE POWER ON ENGINE NR 2, THE TECH HEARD A LOUD BANG AND NOJan 27, 2014 · Aerosp ATR72212A · Engine (Turbine/Turboprop)SDR CA140203005Fuel Control · malfunctioned(CAN) AT THE TOP OF DESCENT, THE CREW OBSERVED INCREASING TORQUE, TEMPERATURE AND COMPRESSOR SPEED FLUCTUATIONS. THEY ELECTED TO SHUT THE ENGINE DOWN BEFORE A SINGLE ENGINE LANDING WAS MADE ON THE 2ND ATTEMPT. POST FLIGHT TROUBLESHOOTING LED TO THE REPLACEMENJan 14, 2014 · Aerosp ATR72212A · Fuel Control/Turbine EnginesSDR CA140224002Pcu · failed(CAN) TAKEOFF WAS ABORTED DUE TO FAULT CODE ALARM FROM THE PROPELLER ELECTRONIC CONTROLLER. DURING THE ON GROUND TROUBLESHOOTING, THE PROPELLER VALVE MODULE, THE OVERSPEED GOVERNER AND THE OIL PUMP WERE REPLACED AND THE ALL FAULTS DISAPPEARED. THE ACFT RETURJan 9, 2014 · Aerosp ATR72212A · Propeller Controlling SystemSDR CA140119002Engine · power loss(CAN) DURING A ROUTINE FLIGHT THE PILOT REPORTED A TORQUE DROP TWICE ON RT ENGINE. THE FIRST WAS A SUDDEN TORQUE DROP FROM 90 PERCENT TO 0 PERCENT. THE PILOT MANAGED TO BRING THE TORQUE BACK TO 90 PERCENT FOR A WHILE BEFORE IT DROPPED AGAIN TO 20 PERCENT IN 2 Jan 4, 2014 · Aerosp ATR72212A · Engine (Turbine/Turboprop)SDR CA131215005Blade · failed(CAN) DURING START NR 2 ENGINE MADE A LOUD NOISE. THE PILOT STOPPED THE STARTING ATTEMPT AND SECURED THE ENGINE. THE GROUND CREWS FOUND THE PROPELLER WAS DIFFICULT TO ROTATE. THE INSPECTION REVEALED 2 DAMAGE PT1 BLADES. THE ENGINE WAS CHANGED AND ACFT RETURNov 16, 2013 · Aerosp ATR72212A · Turbine SectionSDR CA131118005Engine · failed(CAN) EVENT OCCURRED DURING A REVENUE FLIGHT. AT 900FT THE CAPTAIN NOTICED THE UP-TRIM LIGHT FOR THE NR 2 ENGINE ILLUMINATED, THE F/O THEN NOTICED THE PARAMETERS TQ AND NP FOR THE NR 1 ENGINE WERE AT 0 PERCENT. THERE WAS A SLIGHT YAW FELT ON THE ACFT BY 2 ENGNov 5, 2013 · Aerosp ATR72212A · Engine (Turbine/Turboprop)SDR CA131117004Oil System · low pressure(CAN) AFTER TAKEOFF, THE PILOT NOTICED A LOW OIL PRESSURE WARNING ON ENGINE NR 1. THE PILOT SHUTDOWN AND SECURED ENGINE AND RETURNED TO ORIGIN AIRPORT WHERE A SINGLE ENGINE LANDING WAS PERFORMED. 8 QUARTS WERE REQUIRED TO RESTORE ENGINE OIL LEVEL, AN INSPECTOct 27, 2013 · Aerosp ATR72212A · Engine Oil PressureSDR CA131021017Autofeather Sys · malfunctioned(CAN) DURING CLIMB THROUGH FL123, THE ENGINE TORQUE SUDDENLY DROPPED TO ZERO WITHOUT THE OTHER ENGINE PARAMETERS DROPPING DOWN TO ZERO. NO WARNINGS OR FAULT MESSAGES ILLUMINATED IN THE COCKPIT. THE ENGINE WAS SHUTDOWN AND SUCCESSFULLY RE-STARTED AND IT WAS COct 16, 2013 · Aerosp ATR72212A · Propeller Feathering/ReversingSDR CA131021003Oil System · low pressure(CAN) DURING FLIGHT AT FL210, A LOW OIL PRESSURE ALARM, PRESSURE BELOW 40 PSI OCCURRED. THE CREW ELECTED TO SHUTDOWN THE ENGINE AND AN UNEVENTFUL SINGLE ENGINE LANDING WAS PERFORMED. ALL OTHER ENGINE PARAMETERS WERE REPORTED NORMAL.Oct 4, 2013 · Aerosp ATR72212A · Engine Oil Indicating SystemSDR CA131104023Oil System · low pressure(CAN) DURING CLIMB, THE PILOT NOTICED A LOW OIL PRESSURE WARNING ON ENGINE NR 2, CONFIRMED WITH LOW OIL PRESSURE READING ON INDICATOR. THE PILOT ELECTED TO SHUTDOWN THE ENGINE AND RETURNED TO ORIGIN WHERE A SINGLE ENGINE LANDING WAS PERFORMED. MAINTENANCE COOct 1, 2013 · Aerosp ATR72212A · Engine Oil Pressure
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