Pratt & Whitney Canada PW206A
Service difficulty reports · 136
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 = 'PW206A' 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 = 'PW206A' 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 QMLA2024062820076Valve · abnormalNO 1 ENGINE FUEL VALVE' CAUTION LIGHT ILLUMINATED 3 MINUTES AFTER TAKEOFF. LIGHT WENT OUT AND THEN CYCLED ON AND OFF FOR THE DURATION OF THE FLIGHT AS A PRECAUTIONARY LANDING WAS MADE WITH NO OTHER INDICATIONS OF IMMINENT ENGINE FAILURE. DISCONNECTED, CLEANED,SDR UG8A2018072601Engine · failedDUAL ENGINE FAILURE REQUIRING AUTOROTATION AND EMERGENCY LANDING, RESULTING IN SUBSTANTIAL DAMAGE TO THE AIRCRAFT AND INJURIES TO PILOT AND PASSENGERS. NTSB INVESTIGATION IS CURRENTLY IN PROCESS.SDR QMLA2017060217057Wire · damagedWHEN PILOT PULLED AIRCRAFT INTO HOVER, THE NR 1 ENGINE SHUT DOWN. UPON INSPECTION, FOUND TWO WIRES THAT HAD PULLED OUT OF THERE SPLICES. THIS WAS A REPEAT OF SAME PROBLEM THE DAY BEFORE. HAD FOUND MULTIPLE WIRES CHAFED AND TWO BROKEN WIRES. REPAIRED WIRES AS NSDR QMLA2017011817011Warning Light · illuminatedNR 1 ENGINE, OIL CHIP WARNING LIGHT ILLUMINATED IN FLIGHT.SDR M3XA2016110410Oil System · overtempDURING CRUISE ALTITUDE, ENCOUNTERED A NR 1 ENGINE HIGH OIL TEMPERATURE OF 145C. IMMEDIATELY MADE A PRECAUTIONARY LANDING.SDR HDNA20160304001Frame · crackedFRAME 5 HAS ONE INCH CRACK & A MAJOR REPAIR IS REQUIRED.SDR CA150901001Engine · power loss(CAN) DURING TAKE-OFF THE EEC WARNING LIGHT CAME ON FOR A SHORT TIME AND ENGINE NR 1 DID NOT ACCELERATE. AFTER ANOTHER TAKE-OFF ATTEMPT THE ENGINE SPOOLED DOWN AND WENT OFF. THE PILOT TRIED TO RESET THE EEC BUT WITH NO SUCCESS. FIELD SERVICE REP. WILL GO ON SISDR CA141014021Drive Ring · cracked(CAN) WHILE STATIC WITH BLADES UNTIED THE AIRCRAFT WAS SUBJECTED TO ROTOR WASH FROM A HEAVY HELICOPTER. A PREFLIGHT INSPECTION THE FOLLOWING DAY REVEALED THE MAIN ROTOR DRIVE RING WAS CRACKED.SDR CA140224011Connector · contaminated(CAN) DURING FINAL APPROACH, THE MAIN GEARBOX FIRE INDICATION AND AUDIO WARNING WERE ACTIVATED ACCOMPANIED BY A STRONG BURNING ODOR AND SMALL AMOUNT OF SMOKE IN THE CABIN. THE CREW REQUESTED FIRE BRIGADE UPON LANDING. ENGINES WERE SHUTDOWN ON THE GROUND. POSDR CA121120005Hub · cracked(CAN) AD 2012-21-01 WAS CARRIED OUT IAW SB900-117. AN EDDY CURRENT INSPECTION WAS CARRIED OUT BY NDT AND WAS DETERMINED TO HAVE AN.1250" ANOMOLY. THE LOWER HUB WAS THEN REPLACED WITH A NEW ASSY WHICH DID NOT REQUIRE AD 2012-21-01 TO BE CARRIED OUT.SDR CA111125008Bearing · separated(CAN) ON INSPECTION, ELASTOMERICS OF BEARING FOUND SEPARATED FROM THE CENTER MOUNT. BEARING WAS COMPLETELY UNSERVICEABLE.SDR CA111125009Blade · cracked(CAN) UPON DAILY INSPECTION, IT WAS DISCOVERED THAT THE OTBD L/E ABRASION STRIP WAS CRACKED BEYOND LIMITS. THE M/R BLADE WAS R & R WITH A RENTAL UNIT. THE BLADE IS CURRENTLY OUT FOR REPAIR.SDR QMLA2011081511085Fuel Cap · leakingUPON DEPARTURE AND CLIMBOUT, THE PILOT AND CREW SMELLED A RAW FUEL ODOR THROUGHOUT THE ACFT. THE PILOT IMMEDIATELY ABORTED THE MISSION AND RETURNED TO THE BASE. THE MECHANIC ARRIVED AND PERFORMED BOTH VISUAL AND OPS CHECKS OF THE FUELS SYS. IT WAS REVEALED SDR QMLA2010070710031Switch · dislodgedDURING CRUISE FLIGHT, ABOUT 5 MINUTES FROM DESTINATION THE ENGINE CONTROL SWITCH TO THE NR 1 ENGINE WAS EITHER BUMPED OR IT SLIPPED ON ITS OWN TO THE IDLE POSITION. THE PILOT HAD THE MASTER CAUTION FOR THE ENG GOING TO IDLE AND GOT A LT YAW AS WELL. THE PILOT SDR RMXA021620100070Blade · delaminatedDURING A DAILY INSPECTION, THE TECH DISCOVERED A 'L' SHAPED DELAMINATION ON 1 MAIN ROTOR BLADE UPPER SKIN NEAR THE BLADE ROOT OR 'CUFF'. THE DELAMINATION MEASURES 18MM L X 8MM W. MAIN ROTOR BLADE IS BEING REPLACED & DEFECTIVE BLADE BEING SENT BACK TO MFG FOR RSDR 2009FA0000674Fire Detector · false indicationFIRE WARNING LIGHT ILLUMINATED IN FLIGHT. THIS WAS A FALSE INDICATION GIVEN BY THE FIRE CONTROL BOX.SDR CA090219014Wire Harness · damaged(CAN) SHORTLY AFTER T/O, THE ENGINE SUFFERED AN UNCOMMANDED DECREASE IN POWER. THE FLIGHT WAS ABORTED AND THE AIRCRAFT RETURNED TO BASE WITHOUT INCIDENT. THE DECREASE IN POWER WAS COMPENSATED BY THE OTHER ENGINE AND AT NO TIME DID THE ENGINE REVERT TO MANUAL NSDR QML2008F00005Housing · crackedON STARTUP AND PRIOR TO TAKEOFF, PILOT NOTICED SX-5 SEARCHLIGHT SEEMED TO BE VIBRATING EXCESSIVELY. SHUTDOWN AIRCRAFT TO INVESTIGATE AND FOUND BRACKET HOLDING RT SIDE OF LIGHT, BROKEN COMPLETELY THROUGH. THE RT SIDE WELDED MOUNT FITTING OF THE SEARCHLIGHT HOSDR 492AE0278Engine · malfunctionedAFTER A NORMAL SHUT DOWN NR 1 ENGINE RESTARTED ON ITS OWN AFTER ALL POWER AND SWITCHES WERE IN THE OFF POSITION. AFTER INSPECTING THE ENGINE, FOUND MANY POWER TURBINE BLADES MELTED. THIS ENGINE JUST CAME BACK 30.4 HOURS AGO AT OVERHAUL FACILITY. THE ENGINE SDR DXTA200802844Air Duct · contaminatedWITH THE APU ON THE COCKPIT FILLED WITH JET FUEL FUMES STRONG ENOUGH TO BURN YOUR EYES. FOUND AIR COND. DUCTS UNDER CABIN FLOOR TO BE FUEL SOAKED. REMOVED FUEL SOAKED DUCTS AND INSTALLED INSPECTED DUCTS, LEAK AND OPS CHECKED OK. IAW G200 MM 25-00-00. NO ODOR SDR CA071016007Bearing · failed(CAN) THE ENGINE CHIP DETECTOR ACTIVATED, ACCOMPANIED BY VIBRATION AND A TEMPERATURE INCREASE, AND THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INVESTIGATION REVEALED A DAMAGED NR3 BEARING AND RESULTANT TURBOMACHINERY DAMAGE. (TC NR 20071016007)SDR BAQA200600004Bonding Strap · brokenDURING AN AIRFRAME INSPECTION, FOUND 4 BONDING STRAPS THAT GROUND THE HELIPILOT COMPUTERS TO THE AIRFRAME BROKEN. THESE BONDING STRAPS ARE INSTALLED UNDER BT 109EP-51 DATED 2-9-2005 THESE STRAPS ARE THE GROUNDING POINTS FOR THE HELIPILOT SYSTEM. IT IS AN ON SDR HEEA109637Indicator · malfunctionedNR 1 AND 2 N2 NEEDLES WENT TO THE PARK POSITION IN FLIGHT, NR STILL READ CORRECTLY. ALL OTHER INDICATIONS WERE NORMAL. DIVERTED WITH LANDING AT HOSPITAL TO DROP OFF PATIENT TO LANDING AT GLS AIRPORT. REMOVED INSTRUMENT, DETERMINED IT WAS HOT, ALLOWED IT TOSDR BAQ2006F00000Selector Valve · brokenDURING APPROACH FOR LANDING PILOT TRIED TO SELECT GEAR DOWN DURING LANDING PILOT PULLED ON HANDLE TO SELECT GEAR DOWN BUT COULD NOT GET HANDLE TO MOVE. PILOT TRIED SEVERAL TIMES BEFORE THE HANDLE COULD BE MOVED TO THE DOWN POSITION. DURING THE INSPECTION AFTSDR EGRR101267Damper · deterioratedDURING AIRCRAFT INSPECTION, FOUND LT ENGINE EXHAUST SADDLE CHAFING ON ENGINE FIRE EXTINGUISHER BOTTLE UPPER ACTIVATION CARTRIDGE ELECTRICAL WIRE CONNECTING POINT. THE RUBBER NIPPLE WAS CHAFED THROUGH AND THE SADDLE WAS SITTING DIRECTLY ON THE STUD. REPLACED 2SDR BAQ2004F12345Bracket · crackedNR 1 ENGINE LT OB FORWARD ENGINE SUPPORT BRACKET FOUND CANCELLED DURING ROUTINE MAINTENANCE. PART IS VISABLE AFTER INSPECTION PANEL IS REMOVED INSIDE ENGINE COMPARTMENT. PANEL NR 109-0322-10-527.SDR GAKA144ETransmission · contaminatedWHILE IN CRUISE FLIGHT, MAIN ROTOR TRANSMISSION OIL PRESSURE FLUCTUATION OCCURRED RESULTING IN A FLUCTUATION BETWEEN 65-80 PSI., WITH AN ILLUMINATION OF THE LOW OIL PRESSURE WARNING LIGHT. PILOT LANDED IMMEDIATELY AT HELIPAD. TWO QUARTS OF TRANSMISSION OIL WSDR BAQA094260Indicator · inoperativeINDICATOR LIGHTING DIM. REPLACED WITH SERVICABLE UNIT. 05/05/2004SDR BAQA094139Cdu · erraticDISPLAY SCREEN ON CDU IS ERRATIC (FLICKERING, LIGHT TO DARK, ON AND OFF). REPLACED WITH SERVICABLE UNIT, 04/13/2004.SDR BAQA093756Mount · leakingGEARBOX MOUNT IS LEAKING EXCESSIVLEY (FLAT). REPLACED WITH SERVICABLE UNIT FROM AEC, 04/19/2004SDR BAQA094061Pump · failedFUEL PUMP FAILED OUT OF BOX (TSI 4.3 HOURS), RUNS FOR APPROX. 30 SECONDS THEN POPS CIRCUIT BREAKER. A REPLACMENT FOR THIS PUMP WAS ORDERED. REPLACED WITH SERVICABLE UNIT.SDR BAQA094196Pump · intermittentFUEL PUMP HAS INTERMITTENT OPERATION, POPPING CIRCUIT BREAKER. REPLACED WITH SERVICEABLE UNIT FROM AEC, 04/19/2004SDR BAQA094251Master Switch · inoperativeWARRANTY. NR 2 BUS TIE OPEN ON UNIT. THIS UNIT WAS INSTALLED BY HDS AT 11.4 HRS. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 04/26/2004SDR BAQA093968Indicator · burned outINSTRUMENT LIGHTING IS BURNED OUT. REPLACED WITH SERVICABLE UNIT.SDR BAQA093299Indicator · failedSELF-TEST ON POWER UP FAILED MULTIPLE TIMES. REPLACED WITH SERVICABLE UNIT. 03/01/2004SDR BAQA093336Actuator · unserviceableACTUATION LIGHT AMBER LETTER Y ILLUMINATE ON DFD. UNIT WAS CANNED FROM A/C S/N 0132. HARDCARD ENCLOSED REPLACED WITH SERVICABLE UNIT. 02/27/2004SDR BAQA092604Brake Disc · chatteringBRAKE DISC PRODUCING EXCESSIVE CHATTER WHILE BRAKE APPLIED. REPLACED WITH SERVICABLE UNIT. 02/16/2004SDR BAQA093656Pickup · inoperativeNO GAGE INDICATION. REPLACED WITH SERVICABLE ASSET UNIT. 03/10/2004SDR BAQA092485Display · intermittentCENTRAL DISPLAY UNIT INTERMITTENTLY BLACKS OUT WHEN POWER TURNED ON. REPLACED WITH SERVICABLE UNIT. 02/13/2004SDR I05R092764Mount · failedMAIN ROTOR GEARBOX MOUNT FAILED. REPLACED MOUNT.SDR I05R092765Mount · failedMAIN ROTOR GEARBOX MOUNT FAILED. REPLACED MOUNT.SDR BAQA091980Exciter · intermittentEXCITER INTERMITTENT DURING STARTS CAUSING TORCHING DURING STARTS. REPLACED WITH SERVICEABLE UNIT 01/14/2004SDR BAQA091938Pump · malfunctionedPUMP MAKING AIRCRAFT SLOW TO START WITH EXCESSIVE FLAME AND SMOKE OUT OF EXHAUST DURING START SEQUENCE. PART REPLACED WITH SERVICABLE UNIT 01/12/2004SDR BAQA091597Valve · stuckWILL NOT BLOW HOT AIR, VALVE STUCK. PART REPLACED WITH SERVICABLE UNIT. 12/30/2003SDR BAQA092582Blade · contaminatedWATER IN BLADE. REPLACEMENT FOR BLADE NOT RECEIVED YET. BEING REPLACED WITH SERVICABLE UNIT. 02/09/2004SDR BAQA091570Bearing · wornMAIN ROTOR CONTROL ROD BEARINGS WORN.SDR BAQA091574Bearing · wornBEARINGS WORN. REPLACED WITH SERVICEABLE UNIT.SDR BAQA091477Bearing · wornBEARINGS AND BUSHINGS WORN. REPLACED WITH SERVICEABLE UNIT.SDR BAQA091571Bearing · wornBEARINGS AND BUSHINGS WORN. REPLACED WITH SERVICEABLE UNIT.SDR BAQA091670Ecu · inoperativeWARRANTY. NR 1 ENGINE WON'T START. UNIT WAS INSTALLED AT A/CTT 16.6. HARDCARDS ENCLOSED. REPLACED WITH SERVICABLE UNIT. 02/17/2004
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