Pratt & Whitney Canada PW206B2
Service difficulty reports · 110
Newest first. General aviation reporting is voluntary.
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 engine_model_key = 'PW206B2' 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.
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 engine_model_key = 'PW206B2' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR M3XA2016100508Bypass Valve · defectiveDURING APPROACH, PILOT ENCOUNTERED A NR 1 ENGINE OIL TEMPERATURE INDICATION. A PRECAUTIONARY LANDING WAS MADE. MECHANIC DISCOVERED THAT THE NR 1 ENGINE OIL BYPASS VALVE WAS DEFECTIVE. A NEW VALVE WAS INSTALLED PROVIDING A RTS FOR THE AIRCRAFTSDR HDNA201660823008Thermal Bypass · failedTHERMAL BYPASS VALVE FAILED IN CLOSED POSITION NOT ALLOWING OIL TO OIL COOLER.SDR HDNA 20160725211Engine · making metalNR 2 ENGINE CHIP INDICATION IN FLIGHT. PILOT REDUCED ENGINE FROM FLIGHT TO FLIGHT IDLE AND RETURNED TO BASE UNEVENTFUL. MAINTENANCE DISCOVERED HAIRLIKE SLIVER OF METAL ON CHIP DETECTOR.SDR QMLA2016032416029Rod End · wornPILOT REPORTED, HOPPING VIBRATION, IN-FLIGHT WHILE EN-ROUTE TO HOSPITAL. DURING POST FLIGHT CHECK, DISCOVERED THE RED MAIN ROTOR BLADE PITCH LINK UPPER ROD END TO HAVE LATERAL PLAY.SDR QMLA201601816011Unknown · odorPILOT CALLED & STATED STRANGE SMELL IN CABIN & FLIGHT DECK. THIS WAS A STRANGE ODOR TO THE CREW, NOT A BURNING SMELL & NO SMOKE. INSPECTED THE ENGS, TRANSMISSION, BLEED AIR SYS AVIONICS BAY & INTERIOR OF CABIN & FLIGHT DECK. OPERATED ENGS AT FLY FOR SEVERALSDR CA160203008Engine · malfunctioned(CAN) AT 50 FEET, DURING TAKE-OFF, THE PILOT ABORTED AS A PRECAUTION DUE TO A POPPING NOISE OF UNDETERMINED ORIGIN. THE AIRCRAFT LANDED SAFELY. TROUBLESHOOTING IS ON-GOINGSDR CA151215005Engine · cracked(CAN) DURING A CT DISK REPLACEMENT DUE TO LCF NEARING EXPIRY AT 9841 CYCLES, A CRACK WAS FOUND AT THE FLANGE LEADING TO 2 RIVET HOLES. SERVICE INVESTIGATION REQUESTED THE PART FOR FURTHER ANALYSIS.SDR QMLA2015081515074Fan · unserviceableHIGH ENG OIL TEMP ON BOTH ENGS. TROUBLE SHOT BY INSPECTION OF OIL COOLERS, BYPASS VLVS & ENG OIL INDICATING TEMP PROBES. REMOVED OIL COOLERS FOR CLEANING PROCEDURE IAW AMM 79-22-00. WHEN THE BLOWER BAN WAS REMOVED FROM NR 2 SIDE IT WAS DISCOVERED THE BLOWERSDR QMLA2015072115061Engine · making metalTHE PILOT HAD JUST DEPARTED HOSPITAL WITH PATIENT ON BOARD FOR TRANSFER TO ANOTHER HOSPITAL. APPROX 9 MINUTES INTO THE FLIGHT, THE PILOT & CREW EXPERIENCED A VIOLENT YAWING, JOSTLING & HEARD A LOUD THUD FROM THE BACK OF THE ACFT. ALL ENG INDICATIONS WERE NORSDR CA150728005Engine · making metal(CAN) DURING REVENUE FLIGHT, IN CRUISE FLIGHT, THE PILOT REPORTED A LOUD POP SOUND, FOLLOWED BY SEVERE VIBRATION. THE PILOT IMMEDIATELY TOOK PRECAUTIONS TO LAND ON A PRIVATE FIELD. THEY LANDED SAFELY, SHUTDOWN THE ENGINE WHEN ON THE GROUND. NO INJURIES REPORTSDR CA150629008Engine · shutdown(CAN) DURING A REPOSITIONING FLIGHT ON CLIMB OUT, AFTER REFUELING, THERE WAS A CHIP LIGHT INDICATION FOLLOWED BY AN UN-COMMANDED ENG SHUTDOWN. THE ACFT LANDED SINGLE ENG WITHOUT INCIDENT. AWAITING FOR THE CUSTOMER TO PERFORM THE POST FLIGHT INSPECTION. MFG SDR QMLA2015060815048Switch · faultyAPPROXIMATELY 10 MINUTES INTO FLIGHT ENROUTE, NO PATIENT ON BOARD, THE NR 2 GEN OVHT CAUTION LIGHT ILLUMINATED. IMMEDIATELY RETURNED TO THERMAL BASE. EXECUTED EMER CHECKLIST & SHUTDOWN THE NR 2 GEN. LANDED AT BASE UNEVENTFUL. AFTER VISUAL INSPECTION OF THESDR CA150511003Engine · power loss(CAN) DURING ANNUAL INSPECTION FLIGHT TEST PILOT OBSERVED MAIN ROTOR SPEED DROP, WARNING LIGHT ILLUMINATED AND BOTH ENGINE TORQUE INDICATIONS BETWEEN 0 TO 1 PERCENT DURING DESCENT. PILOT DECLARED EMERGENCY LANDING AND ACFT LANDED UNEVENTFULLY IN AN OPEN FIELSDR M3XA2015031111Panel · dislodgedDURING FLIGHT INTERIOR CABIN ROOF PANEL, TRIM, DISLODGED. ACFT MADE A SAFE LANDING, SECURED THE PANEL, NO OTHER ISSUES REPORTED.SDR M3XA2015031112Panel · departedDURING FLIGHT EXTERIOR COVER PANEL FOR THE WINDOW EMER RELEASE DEPARTED THE ACFT. ACFT MADE A SAFE LANDING, REQUESTED FERRY PERMIT TO RETURN TO BASE. COVER PANEL WAS REPLACED & ACFT WAS RETURNED TO SERVICE. NO OTHER ISSUES REPORTED.SDR HDNA2015F00039Electrical Box · failedNR 1 ENGINE WOULD NOT START OR VENT DUE TO NO DC POWER RUNNING THROUGH THE ELECTRICAL MASTER BOX (EMB). THE EMB HAD 27 HOURS SINCE INSTALLED ON THE ACFT.SDR HEER20141211553Bypass Valve · inoperativeWHILE FLYING BETWEEN EW921 AND SS246, SAW THE NR 1 ENGINE TEMPERATURE IN THE RED. REDUCED POWER TO OEI LEVELS AND LOOKED FOR SECONDARY INDICATIONS AND SAW NONE. CONSULTED CHECKLIST AND PERFORMED A SINGLE ENGINE SHUTDOWN. CONTACTED COM CENTER AND WAS ADVISEDSDR CA140623024Switch · intermittentON SHIP BATTERY POWER UP AND FADEC NR 1 POWER UP. FADEC SELF TEST WOULD NOT TEST AND ACFT INDICATED ENGINE NR 1 WAS AT IDLE. THE ENGINE WAS NOT RUNNING AND COULD NOT BE STARTED WITHOUT FADEC SELF TEST. POWER WAS REMOVED AND NR 1 ENGINE SWITCH WAS CYCLED SEVSDR 7AJA20140613003Engine · making metalDURING CRUISE FLIGHT THERE WAS AN ENG CHIP CAUTION ILLUMINATED ON CAD, CAUTION ADVISORY PANEL, FOR THE NR 1 ENG. UPON INSPECTION OF CHIP DETECTOR FOUND MANY LARGE SHINY CHIPS OF MAGNETIC MATERIAL APPEARING TO BE BEARING MATERIAL. ACFT DEEMED UN-AIRWORTHY UNTSDR CA140623023Switch · intermittent(CAN) ON SHIP BATTERY POWER UP AND FADEC NR 2 POWER UP, FADEC SELF TEST WOULD NOT TEST AND ACFT INDICATION ENGINE NR 2 WAS AT IDLE. THE ENGINE WAS NOT RUNNING AND COULD NOT BE STARTED WITHOUT FADEC SELF TEST. POWER WAS REMOVED FROM ACFT AND NR 2 ENGINE SWITCSDR CA140616001Engine · making metal(CAN) DURING FLIGHT, THE CREW RECEIVED A CHIP DETECTOR WARNING ON NR 2 ENGINE. POWER WAS SET TO IDLE FOR THE REMAINDER OF THE FLIGHT BUT AS POWER WAS INCREASED ON APPROACH, THE FADEC SHOWED AN EXCEEDANCE MESSAGE AND UNABLE TO CLEAR. POST FLIGHT INSPECTION FOSDR 7AJA20140530001Engine · making metalNUMBER 2 ENG CHIP DETECTOR WARNING ILLUMINATED. ACFT RETURNED TO BASE.SDR CA140602021Engine · overheated(CAN) THE PILOT SHUTDOWN NR 1 ENGINE FOR HIGH OIL TEMPERATURE AND THEN THE NR 2 ENGINE RUN IN OEI. THE ON GROUND PRELIMINARY FINDINGS FROM THE TROUBLESHOOTING REVEALED THAT NR 1 ENGINE OIL TEMPERATURE PEAKED AT 132.375 OC AND WAS ABOVE 130OC FOR 2 MINUTES 41 SDR CA140505005Eec · warning light(CAN) DURING REVENUE FLIGHT, THE ELECTRONIC ENGINE CONTROL LIGHT ILLUMINATED. THE CREW REDUCED POWER ON THE AFFECTED ENGINE AND ELECTED TO RETURN TO BASE, WHERE AN UNEVENTFUL LANDING WAS ACCOMPLISHED. TROUBLESHOOTING IS ON-GOING AND ENGINE DOWNLOAD DATA UNDERSDR STRA2014FA0000162Heater · contaminatedSHORTLY AFTER TAKEOFF, PILOT TURNED ON CABIN HEATER AND ALMOST IMMEDIATELY, A FOUL ODOR WAS DETECTED BY ALL CREW MEMBERS, SMELLED LIKE SOMETHING BURNING. A HAZE OF WHAT APPEARED TO BE SMOKE WAS EXPERIENCED IN CABIN AREA. AN IMMEDIATE RETURN TO DEPARTURE INISDR QMLA2013081313115Warning Light · illuminatedNR 2 ENGINE CHIP LIGHT ILLUMINATED. USED BURNER ONCE AND LIGHT WENT OUT. CONTINUED FLIGHT AND APPROXIMATELY ONE MINUTE LATER, THE SAME NR 2 ENGINE CHIP LIGHT ILLUMINATED AGAIN. SECURED NR 2 ENGINE AND DECLARED AN EMERGENCY. LANDED BACK AT THE AIRPORT WITSDR QMLA2013071613100Pivot · corrodedTHE PILOT REPORTED THAT ON FINAL APPROACH, THE LT TAIL ROTOR PEDAL BECAME STUCK, AND THE ACFT BEGAN FLYING TO THE RIGHT. DECIDED TO ABORT APPROACH, COULD NOT GAIN CONTROL TO LAND AT DESTINATION. DECLARED AN EMERGENCY, AND AFTER 20 SECONDS, PEDAL MOVEMENT RSDR QMLA2013071213099Bearing · making metalTHE PILOT WAS REPOSITIONING THE ACFT FOR FUEL WHEN ON SHORT FINAL TO THE HELIPAD, THE MASTER CAUTION ILLUMINATED ALONG WITH THE NR 1 ENGINE CHIP LIGHT ANNUNCIATION ON CAD. IAW THE EMERGENCY PROCEDURES, ATTEMPTED TO BURN CHIP WHILE STILL IN FLIGHT. ENG CHIP SDR 2013FA0000377Warning Message · false activationAT 7,000-FT, IFR AND IMC, IN LEVEL FLIGHT AT 115 KNOTS, ENROUTE, ACTUATION ILLUMINATED AND PITCH MODE FAILED. MAINTAINED CONTROL OF ACFT PITCH CHANNEL AND ALLOWED NAV MODE TO CONTINUE NAVIGATION. FAILURE OCCURRED IN RELATIVELY SMOOTH CLOUD FORMATIONS AT 7,000SDR CA130701006Engine · surges(CAN) THE PILOT ABORTED TAKEOFF DUE TO ENGINE SURGE. INVESTIGATION ONGOING.SDR CA130613005Sleeve · loose(CAN) RUBBER SLEEVE BECAME LOOSE ON THE SHAFT.SDR CA130416002Engine · malfunctioned(CAN) DURING LANDING ON THE OIL RIG, PILOT REPORTED THAT BOTH ENGINE`S CAUTION LIGHTS CAME ON FOR ENGINE MANUAL, TWIST GRIP AND ENGINE EXCEED ALONG WITH INCREASING NR AND NF. TROUBLESHOOTING ONGOING. MFG WILL INVESTIGATE TO ESTABLISH ROOT CAUSE AND SUPPLEMENTSDR CA130207005Sensor · defective(CAN) ON START-UP THE INLET BARRIER FILTER SYS WOULD NOT TEST ON THE LT SIDE. A FAULT WAS INDICATED ON THE CONTROL PANEL FOR IBF. THROUGH TROUBLESHOOTING IT WAS DISCOVERED 1 OF THE 2 DIFFERENTIAL PRESSURE SENSOR WAS DEFECTIVE. THE PART WAS REPLACED WITH NEWSDR QMLA2012082712139Connector · burnedCREW NOTICED ODOR AND FUMES IN ACFT DURING FLIGHT, FOUND CONNECTOR BURNED IN BELLY BY AIR CONDITIONER BLOWER MOTOR FOR SB EC135-8010. THIS IS PART OF THE CONDENSOR BLOWER MOTOR WIRING HARNESS.SDR QMLA2012082412137Gearbox · making metalDURING FLT, TRANSMISSION CHIP LIGHT CAME ON. POWER WAS IMMEDATELY REDUCED, EMERGENCY LANDING WAS MADE. DISCOVERED A LARGE CHUNCK OF METAL ON THE CHIP DETECTOR. TRANSMISSION FLUID WAS FLUSHED AND FILLED, FILTER REPLACED, AND A FIFTEEN MINUTE PENALTY RUN ACCSDR CA120827009Engine · power loss(CAN) LIFTING FROM NICE AIRPORT BACK TO THE YACHT, THE PILOT GOT A DOUBLE FADEC MNR ON BOTH ENGINES AT THE SAME TIME. THIS HAPPENED WHEN THE PILOT WAS ACCELERATING OUT OF THE AIRPORT AND CROSSING THE SHORELINE OUT OVER THE OCEAN. HE IMMEDIATELY HAD A DECREASSDR CA120827006Engine · malfunctioned(CAN) UPON TAKEOFF AND BEFORE REACHING 40 KTS WHILE AT 30 FT HEIGHT, NR 2 ENGINE TOT, TORQUE AND N1 OSCILLATES BETWEEN 8-11 FLI, FLIGHT LIMIT INDICATOR, WITH A GONG SOUND AND NR LIGHT COMES ON AND OFF. NR 1 ENGINE TOT, TORQUE AND N1 DECREASES. THE PILOT LANSDR QMLA2012073012121Circuit Card · failedDURING TAKEOFF, THE PILOT AND MEDICAL CREW ALL DETECTED AN ODOR OF BURNING METAL AND RUBBER. PILOT IMMEDIATELY RETURNED TO THE AIRPORT AND SHUTDOWN AIRCRAFT. FOUND THAT THE Z300 CARD IN THE BATTERY MASTER BOX HAD FAILED. OPENSDR CA120319009Mount · failed(CAN) PART INSTALLED WITH 819.6 HRS TSN AND FRESH OUT OF REPAIR. AFTER INSTALL OF 25.7 HRS THE TRANSMISSION SUFFERED A COMPLETE FAILURE AND LOST ALL ITS DAMPING FLUID.SDR CA120208002Mount · failed(CAN) ACFT WAS REPORTED ROUGH IN FLIGHT 35 HRS AFTER MAINTENANCE INSPECTION. DYNAMIC BALANCE EQUIPMENT WAS INSTALLED AND ACFT WAS FOUND TO BE WITHIN LIMITS BUT FURTHER ADJUSTMENTS COULD BE CARRIED OUT. OVER THE 7 ACFT RUNS, THE ACFT WAS NOTICEABLE ROUGHER. TSDR ALGA2012011400001Support · brokenWHILE PERFORMING ANNUAL INSPECTION, PREFORMED SECTION 2, FOUND NR 5 TAIL ROTOR DRIVE SHAFT BEARING SUPPORT BROKEN WHERE T/R CONTROL CABLEMOUNTS TO BRACKET.SDR CA111214003Autopilot Sys · malfunctioned(CAN) AFTER PASSING TURBULENT CONDITIONS OVER MOUNTAINS AND APPROACHING DESTINATION, DURING CRUISE AT FL30, THE PILOT ENGAGED THE ALT AND HDG UPPER MODES AND APPROXIMATELY 2 MIN. LATER IN CALM CONDITIONS, THE HELO ABRUPTLY ROLLED RT AT 90 FOLLOWED BY A DIVE SDR RMXA DMR369596Connector · meltedON FINAL TO BASE, A SLIGHT ELECTRICAL ODOR WAS NOTED TO BE COMING FROM THE AIRCRAFT VENT/AIR CONDITIONING SYSTEM. ACFT HAS AIR CONDITIONING SYSTEM STC SR00565DE INSTALLED. TECH DISCOVERED EVIDENCE OF OVERHEATING ON THE CONNECTOR ON WIRE HARNESS PN EC-135-8010SDR CA110614005Engine · power loss(CAN) POWER ROLLBACK/IFSD IT WAS REPORTED THAT DURING CRUISE, THE NR 2 ENGINE ROLLED BACK THEN SHUTDOWN. AN UNEVENTFUL SINGLE-ENGINE LANDING WAS CARRIED OUT. NO PASSENGERS WERE ON BOARD, CREW ONLY. TROUBLESHOOTING IS ON-GOING.SDR HEEA130955Baffle · damagedENGINE REMOVED DUE TO N2 LOCKUP. INSP REVEALED SHEARED RIVETS ON BAFFLE OF EXHAUST NOZZLE AND DAMAGE TO PT BLADES. ENGINE LOOSELY ASSEMBLED FOR SHIPMENT TO MFG.SDR CA110413007Engine · shutdown(CAN) UNCOMMANDED ENGINE SHUTDOWN DURING ENGINE START RT ENGINE SHUTDOWN BY ITSELF. WHITE SMOKE FROM EXHAUST WAS OBSERVED. THE EVENT OCCURRED WHEN ENGINES CONTROL SWITCHES WERE SWITCHED FROM IDLE TO FLIGHT MODE. TROUBLESHOOTING IS ONGOING.SDR QMLA2011021811027Wire · chafedPILOT EXPERIENCED AN IN FLT FADEC FAILURE/ENGINE MANUAL INDICATION. PILOT PERFORMED EMERGENCY PROCEDURES. ON GROUND AND SHUTDOWN, POWER WAS RE-APPLIED TO SYS & NO FAULTS INDICATED. PERFORMED DIAGNOSTICS WITH MANUFACTURER SOFTWARE. DOWNLOADED DATA FROM DCUSDR QMLA2011021211025Fadec · false indicationTHE PILOT HAD JUST DEPARTED A SCENE WITH A PATIENT ON BOARD WHEN THE HELICOPTER EXPERIENCED A FAILURE OF THE NR1 ENGINE FADEC SYS. THE PILOT IMMEDIATELY TURNED THE ACFT AROUND, AND BEGAN HEADING TOWARDS THE CLOSEST AIRPORT WITH EMERGENCY FACILITIES. THE PILSDR HEEA129960Inverter · smokeNR1 INVERTER CAUTION ILLUMINATED. EMERGENCY CHECKLIST FOLLOWED. APPROX 10 MINS LATER SMELLED SMOKE. LANDED IN FIELD AND CONTACTED MX. CAUSE OF PROBLEM INVERTER.SDR RMXA102820100706Structure · crackedDURING SCHEDULED INSP, A 1.5" LONG CRACK WAS DISCOVERED ON THE COMPOSITE LT CLAMSHELL DOOR. THE CRACK IS AT THE OPENING FOR THE LOCKING PIN TO SECURE THE DOORS TOGETHER NEXT TO THE UPPER LATCH ASSY, TERMED ALIGNMENT CONE BY THE MFG. THE DAMAGED AREA WAS SANDE
Back to Pratt & Whitney Canada PW206B2