Pratt & Whitney Canada PW207D
Service difficulty reports · 133
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 = 'PW207D' 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 = 'PW207D' 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 2A6R201411201572Elastomer · failedTR FLAPPING BEARING ELASTOMER FAILURE & DELAMINATION AT 1054.25 HOURS. SLL IS 15,000 HOURS.SDR CA141114011Wire Harness · faulty(CAN) DURING FERRY FLIGHT, ENGINE NR 2 OIL PRESSURE INDICATION DROPPED TO 0. HELICOPTER CHECKED IN BELL , OIL PRESSURE TRANSDUCER CHECKED WITH SERVICEABLE ONE AND FOUND OK. CONNECTORS ON ADIU REMOVED, CLEANED AND RECONNECTED, INDICATION CAME BACK. DURING WSDR CA141021010Bearing · damaged(CAN) DURING LONG FINALS AIRPORT, PILOT EXPERIENCED HEAVY VERTICAL VIBRATIONS, THIS WAS REPORTED TO THE MAINTENANCE CREW WHO STARTED INSPECTING THE HELICOPTER AND FOUND THAT ON THE ORANGE BLADE PITCH LINK ASSY, ROD END BEARING 429-010-433-101, THE CARTRIDGE 60SDR CA140903006Bearing · failed(CAN) PN 429-010-433-107, PRINTED ON BEARING. ALSO STAMPED ON BEARING, P/N 429-010-433-103. HAD PUT THIS BEARING ON BLUE BLADE ON APRIL 24, 2014 IT FAILED WITH 231.3 HOURS TT ON PART TODAY IS AUGUST 26, 2014. THE BEARING WAS INSPECTED 34.2 HOURS AGO, WITH SDR CA140903004Structure · loose(CAN) WHEN WE WERE PERFORMING SB FOR "FLAPPER VALVE", THIS PART WAS FOUND ON FUEL CELL INNER FLOOR OF MIDDLE CELL. FOUND PN FOR SELF DISASSEMLED ITEM, IT WAS STAINLESS STEEL STRUT-REINFORCEMENT INTERNAL HORIZONTAL. THE PART WAS RE-INSTALLED.SDR CA140908002Engine · power loss(CAN) PERFORMED A HARD LANDING WITH STRUCTURAL DAMAGED. NO INJURY REPORTED. THE PILOT WAS THE ONLY ONE ONBOARD. THE PILOT CLAIMED THERE WAS A LOSS OF ENGINE POWER. CSDR CA140903002Warning Message · illuminated(CAN) DURING TROUBLESHOOTING OF THE FUEL LL2 MAINTENANCE MESSAGE, ENGINEERS DECIDED TO EXPLORE THE SENSOR AND THE WIRING IN THE TANK. WHEN DRAINING THE FUEL, FOUND THAT THE MESSAGE DISAPPEARS WHEN THE AMOUNT OF FUEL LESS THAN 40 KG. NO FAULT FOUND. WHEN VSDR CA140718002Guard · damaged(CAN) WHILE CARRYING OUT PRE-FLIGHT FLOAT TEST SEQUENCE AS DESCRIBED IN THE FLIGHT MANUAL, THE FLOATS INFLATED WHEN THE ARMING SWITCH WAS SELECTED ON.SDR CA140613004Centering Mech · damaged(CAN) DEPARTED WITH THE NOSE WHEEL TURNED 180 DEGREES, BACKWARDS. THE NOSE WHEEL DID NOT RECENTER AFTER TAKEOFF. WHEN WE TRIED TO RETRACT THE GEAR IT BECAME STUCK AND DAMAGED SOME OF THE LANDING GEAR NOSE PANELS, NO STRUCTURAL DAMAGE OCCURED. WE HAD TO LAND SDR CA140428006Cradle · unsecure(CAN) SHORTLY AFTER DEPARTURE, A CLIMB WAS INITIATED FULLY COUPLED FROM 1500 FT -2400 FT. THE AIRCRAFT WAS UNABLE TO CLIMB AND WAS OBSERVED DESCENDING AT 200 FPM. RECEIVED SEVERAL CAS MESSAGES INDICATING BOTH AUTOPILOT CHANNELS WERE DEGRADED. REVERTED TO MSDR CA140415005Float · faulted(CAN) DURING THE PRESTART CHECKS AND FOLLOWING THE CHECK LIST PROCEDURES BELOW: (EXTRACT FROM RFM) INTERIOR AND PRESTART CHECK 2-4-A. PREFLIGHT FLOAT SYS CHECK EMERGENCY INFLATE SWITCH, PEDESTAL, SWITCH GUARD SECURED IN OFF POSITION. BATTERY SWITCH "ON". SDR CA140206003Throttle Cable · frozen(CAN) AN OPERATOR REPORTED TO MFG SEVERAL OCCURRENCES OF THROTTLE CABLE FREEZE WHEN OAT IS APPROXIMATELY -4 TO -6 DEG C OR BELOW. THE EXACT CIRCUMSTANCES WERE NOT REPORTED. ALL BUT ONE OCCURRENCES WERE ON ENGINE NR 2 ONLY.SDR CA140120016Shaft · failed(CAN) ACFT WAS ENROUTE TO AN OFFSHORE PLATFORM WHEN THE NR 2 ENGINE CHIP LIGHT CAME ON AND THE CABIN BEGAN TO FILL WITH SMOKE. PILOT SHUTOFF THE VENT SYSTEM WHICH CLEARED THE SMOKE AND ROLLED NR 2 TO IDLE. ACFT RETURNED AND SHUTDOWN. INVESTIGATION FOUND THE SDR CA131218005Lock · missing(CAN) ON RETURN FROM FLIGHT, IT WAS NOTICED THAT THE LOCK BARREL WAS MISSING FROM CARGO DOOR LOCK SET.SDR CA140108014Connector · unsecure(CAN) DURING FERRY FLIGHT, PILOT EXPERIENCED VERY HIGH FUEL CONSUMPTION, ELECTED TO MAKE A PRECAUTIONARY LANDING WITH ONLY 60 POUNDS OF FUEL REMAINING. HE WOULD NOT HAVE MADE THE REMAINING 60+NM. AFTER LANDING, THE PILOT DISCOVERED FUEL LEAKING DOES THE SIDESDR CA131126012Connector · corroded(CAN) ACFT WAS EXPERIENCING HEADING MISCOMPARE IN EXCESS OF 20 DEGREES. ADAHRS EVENT CODE DOWN LOADED DURING TROUBLESHOOTING. CORROSION WAS FOUND ON CHANNEL A CONNECTOR. A MAGNETO METER CONTINUITY CHECK REPORTED OK.SDR AC2A201311060001Collective Stick · bindingDURING FINAL APPROACH, COLLECTIVE CONTROL BOUND OR FROZE AT APPROXIMATELY 30 PERCENT POWER WHEN POWER WAS REDUCED. A SIGNIFICANT AMOUNT OF FORCE WAS REQUIRED TO PUSH THROUGH THE CONTROL BINDING TO CONTINUE WITH THE APPROACH. ONCE POWER WAS REAPPLIED TO ARRESDR CA131031008Case · cracked(CAN) AN OIL LEAK HAD DEVELOPED ON THE LT SIDE OF THE UPPER TRANSMISSION DECK. IT WAS OBSERVED THAT THE OIL LEAK WAS ORIGINATING FROM A CRACK IN THE RADII TRANSITION AREA OF THE CASE BETWEEN THE LT MAIN INPUT AND PORTION OF THE LOWER CASE.SDR QMLA2013082513121Blade · crackedON 50 HR INSPECTION FOUND CRACK ON BLUE BLADE A-1847 ON L/E ABRASION STRIP 30.25" FROM TIP.SDR QMLA2013072913105Blade · crackedDURING AWC CK FOUND GREEN MAIN ROTOR BLADE, HAS CRACK ON L/E OF ABRASION STRIP AT SCARF JOINT OF BLADE & TIP CAP. CRACK IS .3750" LONG.SDR CA130605006Engine · making metal(CAN) ACFT IS AOG DUE TO ENGINE METAL PARTICLES. FIRST ENGINE CHIP LIGHT REPORTED 16 MAR 2013 AT 94.7 HOURS. SMALL AMOUNT OF VERY FINE PARTICLES AND SEDIMENT FOUND ON THE CHIP PLUGS. PROCEDURES FOLLOWED IAW THE MANUAL AND ACFT RETURNED TO SERVICE. ON 03 APSDR CA130321001Restraint · damaged(CAN) UPON INITIAL LIFT OF THE ACFT, A LOUD METALLIC SOUNDING NOISE WAS HEARD, COMING FROM THE LT SIDE. THE ACFT WAS IMMEDIATELY SET BACK ON THE GROUND. UPON INSPECTION THE LT FORE/AFT TRANSMISSION RESTRAINT WAS IDENTIFIED AS DEFECTIVE, DEBONDED.SDR CA130328005Bearing · debonded(CAN) MAIN ROTOR SHEAR BEARING WAS FOUND TO BE DEBONDED AT THE SPINDLE SHAFT.SDR CA130215012Connector · disconnected(CAN) MIDWAY THROUGH NEW SHIP DELIVERY PROCESS, TECHS REMOVED THE AFT EXHAUST FAIRING PN 429-061-601-103, DESIGNATOR NR 700H, AND FOUND THAT THE ELT COAX CONNECTOR AND GROUND LANYARD WERE NOT CONNECTED AND WERE LAYING ON AND CONTACTING THE TAIL ROTOR DRIVE SHASDR CA121214008Nut Plate · cracked(CAN) A BROKEN TAILBOOM ATTACHMENT NUTPLATE WAS FOUND CRACKED. DURING THE 400 HR TORQUE CHECK ON THE UPPER LT AREA OF THE TAILBOOM ATTACHMENT POINT. A SB IS IN WORK ON THIS SUBJECT.SDR CA121017004Tape · departed(CAN) THE FOLLOWING WAS REPORTED TO MFG: DURING A FLIGHT THE 3M TAPE DEPARTED FROM THE RT EXHAUST EJECTOR AND WRAPPED ITSELF AROUND THE RT HORIZONTAL STABILIZER IN FLIGHT. THE CUSTOMER APPLIED SEVERAL TIME THIS TAPE IAW ASB 429-11-04 AND IT CONTINUES TO COMESDR CA120913007Scoop · separated(CAN) IT WAS REPORTED THAT ACFT HAD THE NR 1 STARTER GENERATOR SCOOP DEPART IN FLIGHT AT 185.0 HOURS TT. THE SCOOP WENT THROUGH THE TAIL ROTOR AND MARKED 2 OF THE T/R BLADES, THE DAMAGE TO THE BLADES WAS MINOR AND WITHIN THE CRITERIA OF THE MM.SDR CA120914008Shaft · sheared(CAN) OPERATOR INFORMED MFG THEY HAD TO MAKE AN EMERGENCY LANDING DUE TO AN ENGINE CHIP LIGHT ON 57004. THE CHIP DETECTOR HAD SLUDGE ON IT. THEY CLEANED IT, REINSTALLED, AND DURING START ATTEMPT THE PILOT HEARD A GRINDING NOISE. THE STARTER-GENERATOR SHEARESDR CA120723003Oil System · low pressure(CAN) DURING RETURN FROM AIRSHOW, ABOUT 2 HOURS INTO THE FLIGHT, PILOTS OBSERVED A LOUD GRINDING NOISE FROM ONE OF THE ENGINES. THIS WAS QUICKLY FOLLOWED BY A CHIP INDICATION AND THE OIL PRESSURE DROPPED TO ZERO. THE ENGINE WAS SHUTDOWN AND THE ACFT LANDED. SDR CA120816001Engine · making metal(CAN) WHILE ENROUTE, HAD TO SHUTDOWN ENGINE 2. WERE CRUISING AT 9500 AND HEARD 2 AUDIBLE GRINDING NOISES FROM THE REAR OF THE ACFT. ALMOST IMMEDIATELY WE RECEIVED A NR 2 ENGINE CHIP LIGHT. AT THAT TIME THE ENGINE 2 OIL PRESSURE ALSO INDICATED IN THE RED. WESDR CA120907007Nozzle · failed(CAN) PLEASE BE INFORMED THAT B429 IS EXPERIENCING NR 1 ENGINE STARTING PROBLEM, FOLLOWING WAS REPORTED BY CUSTOMER: BOTH NR 1 AND NR 2 FUEL FILTER CAUTION LIGHT WERE ON, FUEL FILTERS WERE REPLACED, NO REPORT OF DEBRIS IN THE FILTERS. AFTER FUEL FILTERS REPLSDR QMLA2012061212097Blade · crackedDURING SCHUDULED INSPECTION, FOUND A CRACK AND VOID ON L/E AT STA 125.5" FROM MAST CENTER ON PN 429-015-100-123, A-527 MAIN ROTOR BLADE.SDR CA120529004Reinforcement · detached(CAN) THE STAINLESS STEEL REINFORCEMENT ROD SHOULD BE RETAINED WITHIN 2 CARBON FIBER TUBES. DURING INSPECTION THE STAINLESS STEEL REINFORCEMENT ROD WAS FOUND LOOSE IN THE FUEL CELL.SDR CA120417003Barrel Nut · misinstalled(CAN) DURING A SCHEDULED MAINTENANCE FOR C OF A RENEWAL INSPECTION THE BARREL NUTS, EIGHT OF THEM ON ALL FOUR OF THE MAIN ROTOR GRIP ASSY, WERE FOUND INSTALLED BACKWARD.SDR CA120206009Manifold · damaged(CAN) THE BORE OF THE MANIFOLD WAS NOT PROPERLY DEBURED DURING MANUFACTURING, LEAVING THE POSSIBILITY OF BURRS IN THE BORE FOR THE SEQUENCE VALVE ASSEMBLY.SDR GAKA2012F00040Caliper · out of adjustMADE AN UNSCHEDULED LANDING AFTER DEPARTURE, PILOT NOTICED A CAS MESSAGE "ROTOR BRAKE". THERE WERE NO ADVERSE INDICATIONS THAT THE ROTOR BRAKE HAD ACTUALLY INADVERTANTLY ENGAGED. MX INSPECTED THE ROTOR BRAKE SYS AND MADE ADJUSTMENTS TO THE SENSOR THAT CALCSDR CA111109011Blanket · separated(CAN) NR 2 ENGINE EXHAUST EJECTOR INSULATING BLANKET SEPARATED AND WAS PULLED INTO THE TAIL ROTOR DRIVETRAIN. DAMAGED COMPONENTS INCLUDE: FANSHAFT ASSY, FWD OIL COOLER BLOWER, AFT OIL COOLER BLOWER, OIL COOLER ASSY, AND AFT SEGMENTED TAIL ROTOR DRIVESHAFT. NSDR CA111103011Bonding Wire · broken(CAN) DURING ROUTINE POST FLIGHT INSPECTION, DISCOVERED THE BONDING WIRE, 1 OF 4 ON THE TAIL ROTOR, WAS MISSING. THE CAB HAD BROKEN OFF AT THE 2 TERMINALS ON THE TAIL ROTOR.SDR CA110830017Engine · flamed out(CAN) DURING A TRAINING FLIGHT WITH THE MFG TEST PILOT, THE CREW OF THE NEW ACFTWERE ON DECENT FOR LANDING. AT APPROXIMATELY 150 FT ABOVE GROUND THE CREW NOTICED A "LOW FUEL PRESSURE" INDICATION. BEFORE THEY COULD REACT THE NR 1 ENGINE FLAMED-OUT. THE LANDISDR CA110519005Bolt · cracked(CAN) DURING ROUTINE INSPECTION, IT WAS NOTICE THE EXPANDABLE BLADE BOLT EXHIBIT "CRACK LIKE" INDICATIONS. INDICATIONS WERE NOTICED ON THE CAM HANDLE DUE TO CONTACT WITH CENTER SHAFT WHEN IN FULL OPENNED POSITION.SDR CA110308009Extinguisher · contaminated(CAN) DURING A PREFLIGHT INSPECTION, THE ENGINE FIRE EXTINGUISHER WAS FOUND WITH ZERO PRESSURE. DURING REMOVAL OF THE EXTINGUISHER, WATER WAS FOUND IN THE MANIFOLD.SDR CA110215003Door · openLEFT PAX SLIDING DOOR CAME OPEN AND SLID FULLY AFT. IN FLIGHT, AFTER APPOX 10 MINUTES AT 110 KNOTS.SDR QMLA2010121810083Bearing · wornPILOT NOTICED IN FLIGHT, UPON VISUAL INSP OF MAIN ROTOR AND MAIN ROTOR CONTROLS FOUND GREEN PC LINK UPPER BEARING OUT OF LIMITS.SDR AC2A685K001Warning Light · illuminatedHAD JUST LEFT, ENROUTE, FOR AN ACFT SWAP WHEN A TRANSMISSION CHIP LT LIGHT ILLUMINATED. FOLLOWED EMERGENCY PROCEDURES AND LANDED AS SOON AS POSSIBLE AT SHIPPING PAD.SDR AC2A2009081282853Bolt · brokenDURING PRE-FLIGHT INSP, PIC FOUND THE VERTICAL STABILIZER TO HAVE UP AND DOWN PLAY.SDR CA090901007Bolt · brokenONE OF THE 4 VERTICAL FIN ATTACHMENT (NAS6604-30) BOLTS FOUND BROKEN (BOTTOM AFT BOLT). REMAINING 3 BOLTS WERE NOT FINGER LOOSE, BUT WERE NOT AT MAXIMUM TORQUE. THE NUTS WERE NOT BOTTOMED ON THE SHANK OF THE BOLTS. FRETTING DAMAGE TO TAIL FIN FLANGE BUSHINGSSDR CA090121007Beam · chafedDURING ANNUAL INSPECTION, FRETTING RESIDUE WAS NOTED ON BOTTOM OF LEFT HAND PYLON BEAM ASSEMBLY 427-010-201-107. FURTHER INVESTIGATION AND SUBSEQUENT REMOVAL OF THE BEAM REVEALED CHAFING DAMAGE TO PYLON BEAM 427-010-201-107, ADAPTER 427-010-206-101 AND HOSE 4SDR AC2A2009010180117Switch · failedTRIPLE SWITCH FAILED.SDR CA080710002Cable · broken(CAN) MANUAL RELEASE CABLE BROKE AT CARGO HOOK FITTING CAUSING HOOK TO RELEASE INFLIGHT.SDR CA080528007Shroud · chafed(CAN) OPERATOR REPORTED A MAIN ROTOR TRANSMISSION OIL LINE FAILURE. INSP REVEALED CHAFING DAMAGE TO THE OIL-LINE SHROUD ASSY FROM THE FIREWALL CLOSEOUT METAL EDGE.
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