Pratt & Whitney Canada PW306D1

Service difficulty reports · 107

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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 engine_model_key = 'PW306D1'
  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 DXTR2026101701Turbine Blades · cracked2ND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS IAW EMM 72-00-00. R & R ENGINE IAW AMM 72-00-05, OPS CHKD GOOD.Oct 17, 2026 · N597QS · Cessna 680A · Turbine SectionSDR 2026FA0000841Blades · crackedRIGHT ENGINE 200 HOUR BORESCOPE REINSPECT FINDS ONE HPT STAGE 2 BLADE OUT OF LIMITS AT .225" PER P&WC SI 33-2026R3 DATED OCT 09/2026 RESOLUTION: REMOVE UNSERVICEABLE ENGINE AND RETURN TO P&WC FOR REPAIR.Oct 16, 2026 · N597QS · Cessna 680A · Turbine Engine Compressor SectionSDR 2026FA0000794Compressor Blade · damagedWITHIN SECONDS OF THE TAKEOFF ROLL, FELT A SHORT “BUMP” AND ACCOMPANYING SOUND THAT WAS HARD TO DESCRIBE. IT APPEARED TO COME FROM THE RIGHT SIDE OF THE AIRPLANE, POSSIBLY AROUND THE GEAR AREA. ALL ENGINE INDICATIONS WERE NORMAL WITH NO ABNORMAL CAS MESSAGES OSep 28, 2026 · N859JC · Turbine Engine Compressor SectionSDR DXTR2026092701Compressor Blade · crackedRIGHT ENGINE, SECOND STAGE TURBINE BLADES FAILED BORESCOPE INSP, DUE TO CRACKS OUT OF LIMITS IAW EMM 72-00-00. R & R THE ENGINE IAW AMM 72-00-05, OPS CHKD GOOD.Sep 27, 2026 · N585QS · Cessna 680A · Turbine Engine Compressor SectionSDR DXTR2026091101Turbine Blades · cracked2ND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS PER EMM 72-00-00. CORRECTIVE ACTION: R&R ENGINE PER CE-680A AMM 72-00-05, OPS CHK GOOD.Sep 11, 2026 · N912QS · Cessna 680A · Turbine SectionSDR DXTR2026091102Turbine Blades · cracked2ND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS PER EMM 72-00-00. R&R ENGINE PER CE-680A AMM 72-00-05, OPS CHK GOOD.Sep 11, 2026 · N912QS · Cessna 680A · Turbine SectionSDR DXTR2026090302Blades · crackedBLADE S/N PMOXM75 SUCTION SIDE CRACK .155 INCH. PRESSURE SIDE CRACK .407 INCH (OPEN) THROUGH COOLING HOLE WITH CRACK PRESENT ON TOP OF COOLING HOLE R&R ENGINE.Sep 3, 2026 · N572QS · Cessna 680A · Turbine SectionSDR DXTR2026090303Turbine Blades · crackedSECOND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS IAW EMM 72-00-00.Sep 3, 2026 · N528QS · Cessna 680A · Turbine SectionSDR DXTR2026090304Turbine Blades · crackedSECOND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS IAW EMM 72-00-00. R&R ENGINE IAW AMM 72-00-05, OPS CHKD GOOD.Sep 3, 2026 · N528QS · Cessna 680A · Turbine SectionSDR DXTR2026090305Turbine Blades · crackedSECOND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS IAW EMM 72-00-00. R & R ENGINE IAW AMM 72-00-05, OPS CHKD GOOD.Sep 3, 2026 · Cessna 680A · Turbine SectionSDR DXTR2026090306Turbine Blades · crackedSECOND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS IAW EMM 72-00-00. R & R ENGINE IAW AMM 72-00-05, OPS CHKD GOOD.Sep 3, 2026 · N677QS · Cessna 680A · Turbine SectionSDR DXTR2026090307Turbine Blades · crackedSECOND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS PER EMM 72-00-00. R&R ENGINE IAW AMM 72-00-05, OPS CHKD GOOD.Sep 3, 2026 · N902QS · Cessna 680A · Turbine SectionSDR DXTR2026090308Turbine Blades · crackedSECOND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS IAW EMM 72-00-00. R & R ENGINE IAW AMM 72-00-05, OPS CHK GOOD.Sep 3, 2026 · N905QS · Cessna 680A · Turbine SectionSDR DXTR2026090310Turbine Blades · crackedSECOND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS IAW EMM 72-00-00. R & R ENGINE IAW AMM 72-00-05, OPS CHKD GOOD.Sep 3, 2026 · N916QS · Cessna 680A · Turbine SectionSDR DXTR2026090311Turbine Blades · crackedSECOND STAGE TURBINE BLADES FAILED BORESCOPE INSP DUE TO CRACKS OUT OF LIMITS IAW EMM 72-00-00. R & R ENGINE IAW AMM 72-00-05, OPS CHKD GOOD.Sep 3, 2026 · N916QS · Cessna 680A · Turbine SectionSDR DXTR2026090201Compressor Blade · crackedFAULT: DURING 100 HR 2ND STAGE HPT BORESCOPE RE-INSPECT OF ENGINE, FOUND PREVIOUS CRACK ON SUCTION SIDE OF BLADE HAS MIGRATED BEYOND LIMITS. RESOLUTION: REMOVED ENGINE UNSERVICEABLE & RETURNED TO PWC FOR REPAIR.Sep 2, 2026 · N572QS · Cessna 680A · Turbine Engine Compressor SectionSDR DXTA2026082809469Eec · faultedWHILE DESCENDING THRU FL350 ENG CNTRL FAULT L EICAS ILLUM IN VMC CONDITIONS. RAN CHKLST. AFTER PUTTING ANTI-ICE ON MESSAGE WENT OUT. AFTER TURNING ANTI-ICE OFF, MESSAGE CAME BACK ON FOR A FEW MINS. MANUFACTURER RESPONDED WITH ARES SHOWING L-A FADEC HAS THROWNAug 27, 2026 · N547QS · Cessna 680A · Fuel Controlling SystemSDR DXTA2026062208495Wire Harness · faultedWE RECIEVED AN ENG CNTRL FAULT R CAS MESSAGE DURING CRUISE. RAN THE QRH PROCEDURE BUT MESSAGE DID NOT CLEAR. POWERED UP ACFT VIA APU AND INTERROGATED CMC FOUND 2 FAULT CODES SA & SB. BOTH ISSUES HAPPENED AT CRUISE, CONTINUED. GAINED ACCESS TO DCU CONNECTOR INJun 17, 2026 · N620QS · Cessna 680A · Engine Fuel System WiringSDR DXTA2026061808455Diode · faultyRECEIVED AN AMBER ENG CNTRL FAULT R CAS MESSAGE DURING OUR CLIMB TO CRUISING ALTITUDE. WE RAN THE QRH PROCEDURE BUT THE MESSAGE DID NOT CLEAR. REMOVED PZ012 DIODE MODULE AND INSTALLED NEW DIODE MODULE. PERFORMED ENGINE RUN OF RT ENGINE WITH NO DEFECTS NOTED Jun 15, 2026 · N620QS · Cessna 680A · Fuel Controlling SystemSDR DXTA2026060108256Generator · faultedDURING CRUISE ENG CONTROL FAULT R CASS MESSAGE ILLUMINATED. RAN QRH AND MESSAGE CLEARED. WHEN STARTING DESCENT FELT A VIBRATION THAT CHANGED WITH POWER SETTING CHANGES. OBSERVED THAT THE RIGHT ENGINE POWER CHANGES LAGGED BEHIND THE LT ENGINE BY 2-5%. REMOVED May 28, 2026 · N591QS · Cessna 680A · Engine (Turbine/Turboprop)SDR DXTA2026050707950Anti-Ice Valve · faultedDURING DESCENT WE SELECTED ALL A/I SYSTEMS ON FOR ICING CONDITIONS. ALL SYSTEMS OPERATED NORMALLY. UPON EXITING ICING CONDITIONS AT FL270, SELECTED ALL A/I SYSTEMS OFF. ABOUT 3 MINUTES AFTER SELECTING ALL A/I OFF, WE RECEIVED A/I ENGINE HOT R. ACCOMPLISHEDMay 5, 2026 · N584QS · Cessna 680A · Engine Anti-Icing SystemSDR DXTA2026010806475Throttle · faultyLEFT ENGINE THROTTLE LEVER. UPON RUNWAY LINE-UP, FIRST OFFICER ADVANCED THROTTLES, LEFT THROTTLE DID NOT ADVANCE BEYOND THE CONTROL LOCK POSITION. CONTROL LOCK WAS NOT ON, AND NO CAS MESSAGES WERE DISPLAYED. PERFORMED VOLTAGE AND RESIISTANCE CHECKS OF CONTROLJan 6, 2026 · N641QS · Cessna 680A · Power LeverSDR DXTA2026010506400Anti-Ice System · faultyCLIMBING OUT FLIGHT LEVEL 230 IN MCT STILL. IN ICING CONDITIONS ALL ANTI-ICE ON. AT APPROXIMATELY THREE MINUTES THE A/I ENGINE COLD L ILLUMINATED, AND DID NOT EXTINGUISH. WE INITIATED THE QRH AND ACCOMPLISH IT. THE LIGHT REMAIN ILLUMINATED THEN EXTINGUISH WJan 1, 2026 · N578QS · Cessna 680A · Engine Anti-Icing SystemSDR 2025FA0000834Hp Turbine · crackedRH ENGINE HAS EVIDENCE OF AXIAL CRACKING ON HPT STAGE 1 BLADES (4 TOTAL BLADES).Dec 19, 2025 · N694QS · Cessna 680A · Turbine SectionSDR DXTA2025060603762Engine · faultedIN FLIGHT ENGINE SHUTDOWN. AT APPROXIMATELY FL 330 ON DECENT WE NOTICED A SEVERE RUMBLE FROM THE RIGHT ENGINE, AND LOSS OF THRUST. WE ALSO NOTICED ITT RISE TO 900. THE THRUST WAS ERRATIC AND NOT USABLE. ACCOMPLISHED THE INFLIGHT ENGINE SHUTDOWN QRC AND PROJun 3, 2025 · N909QS · Cessna 680A · Engine (Turbine/Turboprop)SDR DXTA2025050203320Eec · faultedENG CNTRL FAULT L AMBER CAS: ON CLIMB OUT THE AMBER CAS ILLUMINATED PASSING THROUGH 38500 FEET, FOLLOWED BY A AMBER WOW MISCOMPARE. AT APPROXIMATELY 39700 FEET THE A/I STAB HOT AMBER CAS MESSAGE ILLUMINATED. QRH PROCEDURE COMPLETED AND THE ENG CONTROL FAULT L May 2, 2025 · N649QS · Cessna 680A · Fuel Controlling SystemSDR DXTA2025050203311Warning Message · illuminatedRECEIVED AMBER ENG CONTRL FAULT R IN CLIMB OUT. RAN QRH CHECKLIST. MESSAGE REMAINED FOR ENTIRETY OF FLIGHT. ARRIVED ON SITE AND GAINED ACCESS TO AIRCRAFT, PERFORMED ARES DOWNLOAD AND SENT TO TEXTRON FOR REVIEW. FOUND CAS MESSAGE TO BE RELATED TO THRUST REVERMay 1, 2025 · N584QS · Cessna 680A · Fuel Controlling SystemSDR DXTA2025032502777Engine · malfunctionedCLIMBING OUT OF KHPN ABOUT TO LEVEL AT 5000 FT WE RECIEVED A RIGHT RED ENGINE FIRE WARNING. BEFORE I COULD RUN THE CHECKLIST THE LIGHT AND WARNING EXTINGUISHED. I BELIEVE IT WAS FROM THE THEOTTLE RETARDING AT LEVEL OFF. NOTICED THE ITT ON THE RIGHT ENGINE WOMar 21, 2025 · N586QS · Cessna 680A · Fire DetectionSDR DXTA2025030602563Engine · bird ingestionWE FELT AND HEARD A VERY NOTICABLE "CLUNK" AT 200' AGL ON APPROACH. DURING POSTFLIGHT, FOUND EVIDENCE OF BIRD STRIKE ON RIGHT WING LEADING EDGE DIRECTLY IN FRONT OF ENGINE. LARGE BLOOD SPATTERS ON UNDERSIDE OF COWLING, AND BLOOD SCATTERED ON SPINNER AND INSIDEMar 2, 2025 · N697QS · Cessna 680A · Engine (Turbine/Turboprop)SDR DXTA2025030302524Engine · bird ingestionUNSCHEDULED MAINTENANCE: BIRD STRIKE RIGHT WING, MULTIPLE BIRD STRIKE RIGHT ENGINE INTAKE WITH FOD INGESTION WITH BURNING SMELL IN CABIN AFTER STRIKE. DECLARED EMERGENCY AND MADE EMERGENCY RETURN. AT A QUICK GLANCE ENGINE INIDICATIONS AND PARAMETERS WITHIN LIMFeb 27, 2025 · N962QS · Cessna 680A · Engine (Turbine/Turboprop)SDR 2025F00048Flange · chafedRH ENGINE BYPASS DUCT FLANGE FRETTING.Feb 21, 2025 · N936QS · Cessna 680A · Engine (Turbine/Turboprop)SDR DXTA2025020302178Compressor · stalledLEFT ENGINE ENGINE COMPRESSOR STALL: AFTER DEPARTURE AND DURING THE INITIAL CLIMB THROUGH APPROXIMATELY 5000 FEET. THE LEFT ENGINE HAD A SUDDEN LOUD BANG, FOLLOWED BY HEAVY VIBRATION IN THE LEFT ENGINE. NO INDICATION OF FIRE OR OTHER TYPE OF MALFUNCTION WAS PRJan 31, 2025 · N621QS · Cessna 680A · Turbine Engine Compressor SectionSDR 9JLA202501290001Anti-Ice Valve · failedLEFT ENGINE ANTI-ICE FAILED. CAS MESSAGE ILLUMINATED (COLD-R). FOLLOWED QRH PROCEDURE. CAS REMAINED ILLUMINATED.Jan 28, 2025 · N398C · Cessna 680A · Engine Anti-Icing SystemSDR DXTA2025011601954Engine · vibrationENGINE VIBRATION FELT BETWEEN APPROX. 10000 AND FL260 DURING CLIMB AND LEVEL FLIGHT SEGMENTS. TO A LESSOR EXTENT, THE VIBRATION IS FELT DURING THE DESCENT AT APPROX. THE SAME ALTITUDES. PERFORMED LH & RH ENGINE TRANSIENT VIBE SURVEY. NO DEFECTS NOTED. OPS CHECJan 13, 2025 · N652QS · Cessna 680A · Engine (Turbine/Turboprop)SDR DXTA2024121601533Warning Message · false activationENG CNTRL FAULT L AMBER CAS ILLUMINATED ON TAXI IN. ACCOMPLISHED QRH PROCEDURE AND MESSAGE REMAINED. GAINED ACCESS TO AIRCRAFT, POWERED UP APU, NOTED NO FAULTS DISPLAYED. INTERROGATED CDMS, AND FOUND ALERT ID CODE1610 WITH FAULT CODE TE, WHICH IS THRUST REVEDec 14, 2024 · N533QS · Cessna 680A · Fuel Controlling SystemSDR DXTA2024111501134Fault Message · false activationENG CNTRL FAULT L AMBER CAS: ENG CNTRL FAULT L AMBER CAS MESSAGE APPEARED AT THE END OF RUNWAY BEFORE TAKEOFF. RAN QRH PROCEDURE AND DID NOT CLEAR. ALSO NOTICED THE L ITT GAUGE WOULD INTERMITTENTLY GO TO AMBER DASHES AND THE TO CARROT ON THE L N1 GAUGE WOULD GNov 13, 2024 · N943QS · Cessna 680A · Fuel Controlling SystemSDR DXTA2024080500102Oil Filter · faultedDURING CLIMB TURN ON ANTI-ICE ON & SUPPLY BLEED LEAK R MESSAGE ILLUM, RAN CHKLIST & MESSAGE EXTINGUISH FOR A MIN & CAME BACK ON WITH WINDSHIELD HEAT INOP. R MESSAGE ENG CNTRL FAULT. R MESS ILLUM . RAN CHKLSTST. ENG FLAMED OUT CROSSING FL 390. RED OIL PRESAug 4, 2024 · N641QS · Cessna 680A · Turbine Engine Oil SystemSDR DXTA2024073100045Engine · bird ingestionRIGHT ENGINE BIRD STRIKE. 300 AGL. RIGHT ENGINE OVERTEMP AND SHUTDOWN AFTER STRIKE. RIGHT ENGINE FADEC AUTO RELIT AFTER 30 SECONDS AND ENGINE CONTINUED TO OPERATE UNTIL RETURN TO KSJC ACCOMPLISHED UNSCHEDULE BIRD STRIKE INSPECTION PER NJA CE-680A AAIP NJA05501Jul 29, 2024 · N934QS · Cessna 680A · Engine (Turbine/Turboprop)SDR DXTA2024071912401Hmu · defectiveFUEL PRESS LOW R AMBER CAS: AT FL 430, RECEIVED FUEL PRESS LOW R AMBER CAS MESSAGE. THAT WAS SHORTLY FOLLOWED BY A RIGHT FUEL BOOST PUMP ON AMBER CAS MESSAGE. THEN, SHORTLY AFTER THAT, THE RIGHT ENGINE DID AN UN-COMMANDED SHUT DOWN. A RE-START WAS NOT ATTEMJul 18, 2024 · N925QS · Cessna 680A · Fuel Controlling SystemSDR DXTA2024061112018Engine · bird ingestionINGESTED A SEAGULL AT ROTATION INTO THE LEFT ENGINE. THERE IS AT LEAST ONE VISIBLY DAMAGED FAN BLADE. COMPLIED WITH BORESCOPE INSPECTION AND FOUND EVIDENCE OF BIRD INGESTION THROUGH THE CORE OF THE ENGINE; SIX DAMAGED FAN BLADES REMOVED LT ENGINE. INSTALLED RJun 10, 2024 · N626QS · Cessna 680A · Engine (Turbine/Turboprop)SDR DXTA2024042911615Seal · leakingIN THE DESCENT THROUGH 10,000 FT, BOTH CREW NOTICED LT OIL PRESSURE INDICATOR TURNED AMBER AS OIL PRESSURE DECREASED. RAN THE CHECKLISTS, OIL PRESSURE CONTINUED TO DECREASE UNTIL TURNING RED & RED OIL PRESSURE LOW L CAS MESSAGE APPEARED. DID A PRECAUTIONARY EApr 27, 2024 · N621QS · Cessna 680A · Engine Oil PressureSDR 2023F00257Boss · detachedCOMBUSTION CHAMBER DRAIN BOSS DETACHED WHILE FUEL DRAIN VALVE WAS REMOVED ON LH ENGINE. P&WC DEVIATION LETTER WAS ACCOMPLISHED DEVIATION LETTER DAA2023-1044-PW306D1-CN0086, CRM CASE: PWC-285022-Z8X0 DATED AUGUST 23, 2023. DEVIATION LETTER FOR ENGINE MODEL PW30Aug 26, 2023 · N550QS · Cessna 680A · Nacelle/Pylon StructureSDR DXTA2022112174440Warning Message · pilot errorRIGHT THRUST REVERSER WOULD NOT INITIALLY DEPLOY DESPITE SEVERAL ATTEMTPS. LEVER SEEMED JAMMED. MADE NUMEROUS ATTEMPTS WHERE IT WOULD DEPLOY AND THEN NOT DEPLOY. INITIALLY RECEIVED R-L ENGINE CONTROL FAULT CAS MESSAGE.LEFT ENGINE CONTROL FAULT CLEARED. IT LONov 21, 2022 · N521QS · Cessna 680A · Engine Thrust ReverserSDR DXTA2022072566540Transmitter · defectiveRIGHT ENGINE ZERO OIL PRESSURE INFLIGHT 70 MINUTES INTO FLIGHT AT FL410. RED OIL PRESSURE LOW R CAS. SHUTDOWN ENGINE PER CHECKLIST (J2) AND LANDED UNEVENTFULLY. RIGHT OIL AFTER LANDING SHOWED 3/8 INCH ABOVE ZERO, JUST BELOW MIN. OIL CAP SECURED. // SIGNOFF /Jul 22, 2022 · N502QS · Cessna 680A · Engine Oil Indicating SystemSDR 2022F00270Engine · shearedUPPER RH ENGINE BORESCOPE BLANKING PLUG BOLT PN MS9696-07 SHEARED OFF.Jun 27, 2022 · N569QS · Cessna 680A · Engine (Turbine/Turboprop)SDR 2022F00228Engine · corrodedLH ENGINE AGB AFT COVER IS CORRODING.May 16, 2022 · N512QS · Cessna 680A · Accessory GearboxesSDR 2022F00229Engine · corrodedRH ENGINE AGB AFT COVER IS CORRODING.May 16, 2022 · N512QS · Cessna 680A · Accessory GearboxesSDR 2022FA0000206Thrust Reverser · corrodedUPON REMOVAL OF RH ENGINE, FOUND RH LOWER BOTTOM THRUST REVERSER FLANGE CORRODED C/T ENGINE OUTER BYPASS. REFERENCE TEXTRON AVIATION LETTER FF220401 DATED APRIL 1, 2022.Apr 12, 2022 · N544QS · Gulstm 680 · Engine Thrust ReverserSDR 2022F00169Cowling · erodedLH ENGINE LOWER COWL HAS AN AREA DELAMINATED ALONG THE LEADING EDGE. THE REPAIR WAS DEEMED MINOR IN SCOPE. REPAIRED PER TEXTRON AVIATION ENGINEERING MEMO DQ34060M1 DATED MAR 21, 2022.Mar 26, 2022 · N562QS · Cessna 680A · Engine Cowling SystemSDR 2022F00151None · gougedL/H UPPER COWL GOUGED BY O/B BLEED AIR CLAMP AT AFT BLEED AIR COUPLING. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ34079M1, DATED. MARCH 22,2022. 680A-0138 (N582QS) ENGINE UPPER COWL (LEFT AND RIGHT) DAMAGE (GOUGE).Mar 23, 2022 · N582QS · Cessna 680A · Engine Cowling System
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