Pratt & Whitney Canada PW535E

Service difficulty reports · 50

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 = 'PW535E'
  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 DXTA2026101910207Engine · failedON APP FOR RUNWAY 27L INTO PHL, RECEIVED A CAS MSG WITH E1 FUEL FEED FAULT. THEN FOLLOWED WITH E1 FAIL. LOST THE LEFT ENGINE ON THE APPROACH RAN QRC AND LANDED UNEVENTFULLY. ONCE LANDED, SMELLED SMOKE, PERFORMED EVACUATION IAW QRC. CREW AND PAX ARE SAFE. CAOct 16, 2026 · N492QS · Emb EMB505 · Engine (Turbine/Turboprop)SDR DXTA2026052908243Engine · vibrationCLOSE TO V1 WE FELT A VIBRATION THAT RESULTED IN A BURNING SMELL. WHEN CLIMBING THROUGH 800 FT WE RECEIVED AND ENGINE 1 FAIL MESSAGE. COMPLETED CHECKLISTS AND LANDED SAFELY. REMOVED LT ENGINE AND INSTALLED IN SHOP STAND. REMOVED ACCESSORIES, HARNESSES, BRACKMay 27, 2026 · N457QS · Emb EMB505 · Engine (Turbine/Turboprop)SDR DXTA2026031907263Engine · failedDURING THE TAKE OFF ROLL AROUND 30 KNOTS WE EXPERIENCED A RIGHT ENGINE FAILURE. WE HEARD 4-5 COMPRESSOR STALLS. ENGINE SHUT DOWN ON ITS OWN. WE PULLED OFF THE RUNWAY AND HAD THE AIRCRAFT TOWED TO SIGNATURE. UPON VISUAL INSPECTION WE DID NOT NOTICE ANY ABNOMar 15, 2026 · N331QS · Emb EMB505 · Engine (Turbine/Turboprop)SDR DXTA2026010206358Engine · faultyUPON CLIMBING THROUGH APROX 2500', RECEIVED A E2 OIL LOW PRESSURE CAS MESSAGE. ADVISED NEEDED TO RETURN TO AIRPORT. ABOUT A MINUTE LATER DETECTED A BURNING ODOR WHICH WAS SHORTLY FOLLOWED BY SMOKE FILLING THE CABIN. DECLARED AN EMERGENCY & ADVISED RETURNING. RDec 29, 2025 · N390QS · Emb EMB505 · Engine (Turbine/Turboprop)SDR DXTA2025120205928Fuel Control · failedFUEL FEED 1 FAULT & FUEL FEED 2 FAULT MESSAGES DISPLAYED IN FLT, ACCOMPANIED WITH YELLOW XS OVER MOTIVE FLOW PUMPS ON FUEL SYNOPTIC PAGE. NR 1 MESSAGE APPEARED FIRST FOLLOWED BY NR 2 A FEW SECS LATER WHEN CLIMBING THROUGH APPROX FL280. ALL INDICATIONS REMAINEDec 1, 2025 · N331QS · Emb EMB505 · Fuel Control/Turbine EnginesSDR 2026FA0000083Hydraulic Line · failedHYDRAULIC SYSTEM FAILURE FOLLOWED BY NUMBER 2 ENGINE FAILURE. ROOT CAUSE DETERMINED TO BE FAILURE OF NUMBER 1 ENGINE HYDRAULIC PRESSURE LINE.Oct 19, 2025 · N29GS · Emb EMB505 · Hydraulic System, MainSDR DXTA2025051903504Engine · fodMOLD ODER IN COCKPIT, BOTH CREW MEMBERS EXPERIENCING SORE THROAT. FOUND UNKNOWN DEBRIS IN LH ENGINE DURING BOROSCOPE. ACCOMPLISHED COMPRESSOR WASH ·PERFORMANCE RECOVERY IAW PHENOM 300 AMM 71-00-00-160·806, NO ODOR PRESENT AT THIS TIME. (ORIGINAL SUBMISSION May 15, 2025 · N431QS · Emb EMB505 · Engine (Turbine/Turboprop)SDR DXTA2025040702972Warning Message · false indicationAIR INTAKE ANTI-ICE / DE-ICE: A-I E1 FAIL AND A-I E2 FAIL CAS MESSAGE DISPLAYED DURING THE APPROACH PHASE. WE WERE OPERATING IN INSTRUMENT CONDITIONS AND THE TAT WAS 8C. CYCLING THE ENG1 AND ENG2 SWITCHES OFF AND BACK ON AGAIN CLEARED THE MESSAGE. CORRECTIVE AApr 6, 2025 · N371QS · Emb EMB505 · Engine Anti-Icing SystemSDR DXTA2025012702092Exciter · defectiveLEFT ENGINE HUNG START: 80-10-06-01 WHEN STARTING ENGINE 1 OBSERVED IGNITION B FUEL FLOW, AND N1 HANG AT 4% ABORTED THE START, RAN THE ENGINE START MALFUNCTION QRC CONTACTED MCC. CORRECTIVE ACTION: REPLACED ENGINE IGNITION EXCITER. OPS CHECK GOOD. IAW P-300 EMJan 23, 2025 · N330QS · Emb EMB505 · ExciterSDR DXTA2024121601482Oil System · leakingON DEPARTURE ENG NO TO DATA ILLUM AFTER TAKEOFF & GEAR RETRACT. FOLLOWED BY A YELLOW X OVER NR 2 ENG OIL PRESSURE. SMOKE IN CABIN & DONED O2 MASKS. CLIMBED THROUGH 2000FT E2 OIL LO PRESS RED CAS APPEARED. PERFORMED ENG SHUTDOWN & RETURNED TO FIELD. OIL DRIPDec 11, 2024 · N439QS · Emb EMB505 · Turbine Engine Oil SystemSDR DXTA2024081900263Engine · failedLEFT ENGINE FAILURE DEPARTING SFO AT 1000' MSL. 2-3 BANGS THEN ENGINE FAILURE. NOT ASSOCIATED WITH ANY CAS MESSAGES. SHUT LEFT ENGINE DOWN & BURNED OFF FUEL & RETURNED TO SFO. ACCOMPLISHED THE REMOVAL OF THE LT ENGINE AND INSTALLED A RENTAL INSPECTED ENGINE. Aug 17, 2024 · N337QS · Emb EMB505 · Engine (Turbine/Turboprop)SDR DXTA2023071090720Engine · failedENGINE FLAMEOUT: LEFT ENGINE FAILED INFLIGHT AT FL250. PAX AND PILOTS FELT SIGNIFICANT VIBRATIONS/BUMPS FOLLOWED BY WIND DOWN AMID FAILURE INDICATION ON ENGINE SYNOPTIC. RESOLUTION: REMOVED LH ENGINE PN: 3072913-01 SN: PCE·DG0528 FROM AIRCRAFT N438QS SN: 50500Jul 9, 2023 · N438QS · Emb EMB505 · Engine (Turbine/Turboprop)SDR DXTA2022120175210Engine · power lossWHEN ADDING POWER FOR CLIMB OUT OF 3000 FT, 4 LOUD BANGS HEARD & LT ENG ROLLED BACK TO WINDMILLING RPM. APPEARED TO BE A FADEC COMMANDED ENG SHUTDOWN. NO ABNORMAL INDS PRIOR SHUTDOWN, & EICAS MESSAGES WERE EXPECTED FOR CONDITION AFTER SHUTDOWN. POST FLT INSP,Nov 30, 2022 · N383QS · Emb EMB505 · Engine (Turbine/Turboprop)SDR DXTA2022040659730None · noneRIGHT ENGINE ENGINE FAN BLADE: DURING TAKEOFF ROLL AT ROTATION, WE HAD A VERY LARGE BIRD STRIKE WITH INGESTION IN THE RIGHT ENGINE.Apr 5, 2022 · N353QS · Emb EMB110* · Turbine Engine Reduction GearSDR 2021FA0000315Starter Gen · defectiveTHE OPERATOR STATED THAT AFTER TAKEOFF THE FLIGHT CREW EXPERIENCED HIGH ENGINE VIBRATIONS WITH THE LEFT ENGINE. THEY'RE CHECKLIST LED THEM TO DO AN ENGINE SHUTDOWN AND THEY RETURNED TO EVANSVILLE (EVV). THEY TROUBLESHOT THE HIGH VIBES WITH EMBRAER AND PRATT Nov 8, 2021 · Emb EMB505 · Starter-GeneratorSDR 3WTR20210726Control Cable · frayedFOUND BROKEN AILERON CABLE STRANDS ON LH AND RH WING CABLES, 2EA P/N 505-15135-405 WHILE PERFORMING DVI INSPECTION ON TASK CODE 27-11-02-002 FOR A 3200 HR/60 MONTH INSPECTION. THE CABLES HAVE NO INDICATION OF WEAR AND HAVE MULTIPLE STRANDS BROKEN ON THE UPPER Jul 14, 2021 · N304GV · Emb EMB505 · Aileron Control SystemSDR XMXR202104230004Shutoff Valve · failedBLEED 2 OVERPRESSURE FOLLOWED BY A BLEED 2 FAILApr 1, 2021 · N335AS · Emb EMB505 · Engine Bleed Air SystemSDR 3WTR20210317Control Cable · brokenFOUND BROKEN AILERON CABLE STRANDS ON LH AND RH WING CABLES, 2EA P/N 505-15135-405 WHILE PERFORMING DVI INSPECTION ON TASK CODE 27-11-02-002 FOR A 3200 HR/60 MONTH INSPECTION. THE CABLES HAVE NO INDICATION OF WEAR AND HAVE MULTIPLE STRANDS BROKEN ON THE UPPER Mar 15, 2021 · N300GV · Emb EMB505 · Aileron Control SystemSDR 2021FA0000077Control Cable · brokenFOUND BROKEN AILERON STRANDS ON L/H AND R/H WING CABLES 2EA P/N: 505-15135-405 WHILE DOING DVI INSPECTION ON TASK CODE 27-11-02-002 FOR A 3200/60 MONTH. THE CABLES HAVE NO INDICATION OF WEAR AND HAVE MULTIPLE STANDS BROKEN ON THE UPPER SIDE OF THE CABLE LOCATEMar 9, 2021 · N300GV · Emb EMB505 · Aileron Control SystemSDR XMXR202107220004Shutoff Valve · failedBLEED 2 PRSOV FAILFeb 17, 2021 · N697AS · Emb EMB505 · Compressor Bleed ValveSDR XMXR202010220001Precooler · crackedCRACKED INTERNAL SUPPORT STRUT.Oct 22, 2020 · N346AS · Emb EMB505 · Engine Bleed Air SystemSDR DXTA2020090918041Starter Gen · defectiveAFTER TAKEOFF, NOTED LOW FREQUENCY RUMBLE ASSOCIATED WITH RIGHT THROTTLE MOVEMENT. THEN GOT GEN 2 OFF BUS CAS MESSAGE. RIGHT ENGINE SHUT DOWN IAW QRH. SIGNIFICANT CARBON VISIBLE ON BOTTOM OF RIGHT ENGINE ON POST FLIGHT. SIGN OFF. PERFORMED GVI OF RT ENGINSep 18, 2020 · N379QS · Emb EMB505 · Starter-GeneratorSDR 2PJA2020032000000Tire · blownWHILE DEPARTING RWY 33 AT MARTIN STATE (MTN) FOR CLEVELAND INTL (CLE), WE EXPERIENCED A TIRE BLOWOUT JUST PRIOR TO V1 RESULTING IN A HIGH-SPEED ABORTED TAKE-OFF. ALL PRE-FLIGHT CHECKS WERE COMPLETED AND SATISFACTORY. INSPECTION OF THE TIRES AND LANDING GEAR DIMar 19, 2020 · N185P · Emb EMB505 · TireSDR 2020FA0000190Brake Sys · contaminatedTHE LEFT AND RIGHT MAIN LANDING GEAR WHEEL BRAKES WERE REPLACED WITH OVERHAULED UNITS AND THE AIRCRAFT WAS RELEASED TO SERVICE ON 2/26/2020. THE AIRCRAFT OWNER/OPERATOR FLEW ON MARCH 1 2020 AND REPORTED AFTER THE SECOND LANDING INTO KDAL LOVE FIELD THAT THE LEMar 1, 2020 · N636SD · Emb EMB500 · Landing Gear Brake SystemSDR XMXR20200211001Starter Gen · failedGEN OFFLINE CASS AND PRECAUTIONARY ENGINE SHUTDOWN DUE TO VIBRATION.Feb 11, 2020 · N359AS · Emb EMB505 · Starter-GeneratorSDR DXTA2020020603417Garlock Seal · leakingRIGHT ENGINE - UPON DECENT A E2 OIL LO PRESS ILLUMINATED, WITH ASSOCIATED ENGINE PRESSURE INDICATION SHOWING 28 AND FALLING. THUS DIRECTING US TOWARD THE NAP 1-16 ENGINE SHUTDOWN PROCEDURE WHICH WE ACCOMPLISHED AND LANDED IN MSP. ///SIGN-OFF/// EVALUATED ANFeb 5, 2020 · N404QS · Emb EMB505 · Engine Oil Indicating SystemSDR 2PJA202002050001Flap System · failedON JANUARY 3, 2020, N654SR WAS CRUISING AT FL400 FROM SARATOGA COUNTY (5B2) WITH TWO PASSENGERS DESTINATION LEXINGTON KENTUCKY (KLEX). FIRST INDICATION OF A PROBLEM WAS THE AMBER SWPS FAIL ANNUNCIATOR FOLLOWED BY THE WHITE ADVISORY SPOILER FAIL INDICATION. PMFeb 3, 2020 · N654SR · Emb EMB505 · Trailing Edge Flap Control SystemSDR E07A201912020009Diverter · crackedCRACKED LH PRECOOLER INLET DIVERTER WELDS FOUND DURING INSPECTION IAW SERVICE LETTER 505-36-0003. REPLACED WITH OVERHAULED UNIT.Oct 10, 2019 · N301AS · Emb EMB505 · Engine Bleed Air SystemSDR E07A201912020010Diverter · crackedCRACKED RH PRECOOLER INLET DIVERTER WELDS FOUND DURING INSPECTION IAW SERVICE LETTER 505-36-0003. REPLACED WITH OVERHAULED UNIT.Oct 10, 2019 · N301AS · Emb EMB505 · Engine Bleed Air SystemSDR E07A201912020012Diverter · crackedCRACKED RH PRECOOLER INLET DIVERTER WELDS FOUND DURING INSPECTION IAW SERVICE LETTER 505-36-0003. REPLACED WITH OVERHAULED UNIT.Oct 9, 2019 · N335AS · Emb EMB505 · Engine Bleed Air SystemSDR 2019FA0000186Wire Harness · brokenCABIN DOOR INDICATION HARNESS BINDS, STRESSES AND BENDS SEVERELY UNDER TOP STEP (FUSELAGE TO CABIN DOOR HINGING STEP) WHEN CABIN DOOR IS CLOSED CAUSING INDICATION HARNESS TO BREAK AND ILLUMINATING A FALSE WARNING ON CAS.Jun 19, 2019 · N60NF · Emb EMB505 · Door System WiringSDR CA190604003Engine · unknown(CAN) DURING TAKEOFF, HSDB FAULT AND ENG NO DISPATCH CAS MESSAGE ILLUMINATED. ENGINE INSTRUMENTS DISPLAYED YELLOW X FOR FEW SECONDS. CREW ABORTED THE TAKE-OFF BEFORE REACHING 30 KNOTS. TROUBLESHOOTING IS GOING ON.May 20, 2019 · Emb EMB505 · Engine (Turbine/Turboprop)SDR 2019F00212Starter Gen · failedAT CRUISE, INDICATION OF LOSS OF ELECTRICAL POWER OF THE #2 DC STARTER/GENERATOR. CREW ELECTED TO MAKE AN UNSCHEDULED PRECAUTIONARY LANDING AT KATL. UPON INSPECTION, THE STARTER GENERATOR WAS DISCOVERED TO BE INTERNALLY FAILED, AND HAD SHEARED ITS DESIGNED DRIMay 4, 2019 · N301AZ · Emb EMB505 · Starter-GeneratorSDR CA190426014O-Ring · failed(CAN) DURING FLIGHT, THE LEFT HAND ENGINE OIL PRESSURE WENT INTO YELLOW ZONE AND THE PILOT PULLED BACK POWER WHERE THE OIL PRESSURE WENT BACK TO GREEN. AIRCRAFT CONTINUED WITH THE LANDING AND LANDED UNEVENTFULLY. AFTER LANDING AND DURING TAXIING, THE OIL PRESSApr 20, 2019 · Emb EMB505 · Turbine Engine Oil SystemSDR E07A201912020011Precooler · crackedCRACKED LH PRECOOLER INLET DIVERTER WELDS FOUND DURING INSPECTION IAW SERVICE LETTER 505-36-0003. REPLACED WITH OVERHAULED UNIT.Apr 2, 2019 · N346AS · Emb EMB505 · Engine Cooling SystemSDR 4NSA2019FA0000067Starter Gen · shortedDURING CRUISE, FLIGHT CREW NOTICED A MODERATE VIBRATION COMING FROM THE BACK OF THE AIRCRAFT. AFTER FURTHER INVESTIGATION, THE CREW DETERMINED THAT THE VIBRATION WAS COMING FROM THE RT NACELLE. SHORTLY AFTER, THE CREW RECEIVED A RT GEN FAIL CASS MESSAGE AND THMar 13, 2019 · N516N · Emb EMB505 · Starter-GeneratorSDR E07A201912020013Diverter · crackedCRACKED LH PRECOOLER INLET DIVERTER WELDS FOUND DURING INSPECTION IAW SERVICE LETTER 505-36-0003. REPLACED WITH OVERHAULED UNIT.Mar 8, 2019 · N340AS · Emb EMB505 · Engine Bleed Air SystemSDR E07A20191202014Diverter · crackedCRACKED RH PRECOOLER INLET DIVERTER WELDS FOUND DURING INSPECTION IAW SERVICE LETTER 505-36-0003. REPLACED WITH OVERHAULED UNIT.Mar 8, 2019 · N340AS · Emb EMB505 · Engine Bleed Air SystemSDR E07A201912020007Precooler · crackedCRACKED LH PRECOOLER INLET DIVERTER WELDS FOUND DURING INSPECTION IAW SERVICE LETTER 505-36-0003. REPLACED WITH OVERHAULED UNIT.Mar 1, 2019 · N361AS · Emb EMB505 · Engine Cooling SystemSDR 2019F00130Warning Message · false activationAIRCRAFT DURING REQUESTED DESCENT HAD SWPS FAULT ANNUNCIATOR ILLUMINATED, ALONG WITH THE MAX SPEED FLAG AT THE TOP OF THE AIRSPEED TAPE. AIRCRAFT DESCENT IN EMERGENCY. AIRCRAFT LANDED SAFELY. ON GROUND WEST STAR TECHNICIANS PERFORMED SWPS STALL TEST SWITCH (PRFeb 15, 2019 · N858EE · Emb EMB505 · Stall Warning SystemSDR 2018FA0000491Control Cable · chafedDURING INSPECTION IT WAS FOUND THAT THE LH AND RH AFT UPPER SECTION OF RUDDER CABLES WERE CHAFED BEYOND LIMITS. IT WAS NOTED THAT THE CHAFING IS HAPPENING AT THE FAIRLEADS/CABLE SUPPORTS. THE CABLE TENSION IS 5 LBS SO THE CABLES LAY ON THE FAIRLEADS, THEREFORENov 27, 2018 · N367QS · Emb EMB505 · Rudder Control SystemSDR E07A201912020006Precooler · crackedCRACKED LH PRECOOLER INLET DIVERTER WELDS FOUND DURING INSPECTION IAW SERVICE LETTER 505-36-0003. REPLACED WITH OVERHAULED UNIT.Nov 20, 2018 · N361AS · Emb EMB505 · Engine Bleed Air SystemSDR CGHR201809191000Pump · failedFLIGHT DATE 8/22/2018. DURING CRUISE PILOTS REPORTED "WHINING" NOISE FROM NR 1 ENGINE FOLLOWED BY CAS MESSAGE "HYDRAULIC FAULT." SYSTEM INDICATED HYDRAULIC PRESSURE FLUCTUATIONS. CREW CLOSED SHUT OFF VALVE ON NR 1 ENGINE. AFTER MULTIPLE FAILED ATTEMPTS TO PUTSep 19, 2018 · N65KZ · Emb EMB505 · Hydraulic Pump (Electric/Engine), MainSDR E07A201912020003Precooler · crackedCRACKED RT PRECOOLER INLET DIVERTER WELDS, FOUND DURING INSPECTION. REPLACED WITH OVERHAULED UNIT.Jun 15, 2018 · N359AS · Emb EMB505 · Engine Bleed Air SystemSDR E07A201912020004Precooler · crackedCRACKED RH PRECOOLER INLET DIVERTER WELDS FOUND DURING INSPECTION IAW SERVICE LETTER 505-36-0003. REPLACED WITH OVERHAULED UNIT.Jun 13, 2018 · N368AS · Emb EMB505 · Engine Bleed Air SystemSDR DXTA2018031900726Interface Unit · faultedMULTIPLE AIRFRAME AND ENGINE CAS MESSAGES IN-FLIGHT INCLUDING, LG LEVER DISAG, E1 TTO HTR FAIL, PRESN AUTO FAIL, OXY LOW PRES, A-I E2 ON, A-I E1 ON, SWPS ICE SPEED, A-I WINGSTB ON, ADS 2 SLIP FAIL, ADS 1 SLIP FAIL, AND ENG NO DISPATCH. REMOVED AND REPLACED Mar 16, 2018 · N395QS · Emb EMB505 · Engine Fuel and ControlSDR E07A201802230001Precooler · damagedBLEED 1/2 FAILED IAW SIL505-36-0003. INSPECTED RT ENGINE PRECOOLER PER SIL505-36-0003 REV 2 AS PART OF A VOLUNTARY EXECUTIVE AIRSHARE FLEET CAMPAIGN. FOUND BOTH PRECOOLER DIVERTER VANES CRACKED AND BROKEN OFF. DIVERTER VANES FOUND LAYING ON TOP OF PRECOOLER EFeb 23, 2018 · N301AS · Emb EMB505 · Engine Oil CoolerSDR E07A201912020001Precooler · crackedCRACKED RH ENGINE PRECOOLER INLET DIVERTER WELDS FOUND DURING INSPECTION. REPLACED WITH OVERHAULED UNIT.Feb 23, 2018 · N359AS · Emb EMB505 · Engine Bleed Air SystemSDR E07A201912020002Precooler · crackedCRACKED LH ENGINE PRECOOLER INLET DIVERTER WELDS FOUND DURING INSPECTION. REPLACED WITH OVERHAULED UNIT.Feb 23, 2018 · N359AS · Emb EMB505 · Engine Bleed Air SystemSDR 9JLA2017051804389Ignition Lead · defectiveTHE CREW REPORTED A FAULT WITH THE NR 1 ENGINE IGNITION CHANNEL A. TROUBLESHOOTING DISCOVERED A DISCREPANCY WITH THE IGNITION LEADS. COMPLIED WITH THE SERVICE BULLETIN PW500-72-30529 TO REPLACE THE IGNITION LEADS ON BOTH ENGINES. FT WAS SATISFACTORY AND THE AIApr 26, 2017 · N732AC · Emb EMB505 · Ignition Harness (Distribution)
Back to Pratt & Whitney Canada PW535E