Pratt & Whitney Canada PW306A
Service difficulty reports · 198
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 = 'PW306A' 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 = 'PW306A' 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 DXTA200802858Fuse · failedAPU FIRE CAS MESSAGE ILLUMINATED ALONG WITH FIRE BELL ENROUTE AT FL380. RT FIRE BOTTLE WAS DISCHARGED INTO APU. FIRE INDICATION REMAINED ON, DIVERTED. AFTER SHUTTING DOWN AND EXITING AC, NO SMOKE, FLAMES OR SOOT WERE VISIBLE IN THE AREA OF THE APU BUT THE APU SDR DXTA200802840Switch · inoperativeDURING T/O ROLL WITH THROTTLES AT T/O DETENT THE BLEED PRESS/TEMP HIGH MSG ILLUMINATED. THE T/O WAS ABORTED. M2B- REMOVED FWD OVERTEMP SWITCH P/N 641180-1 S/N 0245 AND INSTALLED NEW FWD OVERTEMP SWITCH P/N 641180-1 S/N 0368. REMOVED AFT OVERTEMP SWITCH P/N 641SDR DXTA200802800Control Unit · malfunctionedSLATS FAILED TO RETRACT, CAS MSG: SLAT UNBALANCED, SLAT FLAP MAINTAIN. FLAPS/SLATS FUNCTIONAL TEST GOOD. PERFORMED FSECU BITE CHECK. NO FAULTS FOUND.SDR DXTA200802776Connector · defectiveAFTER TAKEOFF AT MLG AMBER AND RED HASHES FLASHED ON AND OFF THRU ENTIRE FLIGHT. REPLACED RT MLG CONNECTOR 44G1 USING CONNECTOR P/N D38999/24WB98SN. BACKSHELL P/N TX1240AB90-1006A1 AND BOOT 202S132-25S. WORK IAW ENG ORDER DOC 4AS8104002 A013REV. PERFORMED RTSDR DXTA200802759Float Valve · failedIN CRUISE FLIGHT AT FL380 WE NOTICED FUEL LEAKING OUT OVER THE LT AILERON. REMOVED DEFECTIVE LEFT WING VENT FLOAT VALVE AND INSTALLED NEW VALVE PER G200 CMP 28501.SDR DXTA200802747Squat Switch · malfunctionedGROUND AIR BRAKES DEPLOYED ON FINAL APPROACH WHEN THE SWITCH WAS ARMED. R & R LT MLG WOW SWITCH AND HARNESS IAW AMM 32-60-05. OPERATIONAL & FUNCTIONAL CHECK GOOD WITH NO FURTHER DEFECTS NOTED.SDR DXTA200702677Control Valve · bypassingAC PULLS RT WITH NEUTRAL TILLER POSITION. NWS DISENGAGES WHEN ATTEMPTING FULL RT TURN. REMOVED AND REPLACED NOSEWHEEL STEERING CONTROL VALVE. AND ADJUSTED FEEDBACK MANIFOLD POTENTIOMETERS 1 AND 2 IAW GAC G200 AMM 32-50-00 AND 32-50-15.SDR CA071128015Valve · malfunctioned(CAN) PILOT REPORTED PARK BRAKE SET AND INDICATED ON EICAS. STARTED RT ENGINE WITH THE CHOCKS REMOVED, READY FOR DEPARTURE. THE AIRCRAFT ROLL FWD AFTER THE ENGINE WAS STARTED. PILOT CHECKED THE INDICATION ON EICAS AND THE INDICATION WAS STILL ON EICAS PARK BRASDR DXTA200702617Warning Light · illuminated"RT BLEED AIR LEAK" WOULD NOT EXTINGUISH INFLIGHT AND RT ENGINE SHUTDOWN INFLIGHT. "RT BLEED AIR LEAK" MESSAGE REMAINED ON AFTER ENGINE SHUTDOWN. R & R RT FWD & AFT LEAK DETECTION ELEMENTS IAW MM 21-61-60. OPS CHECKED SATISFACTORY.SDR DXTA200702614Skin · damagedDURING LANDING AND AFTER TOUCHDOWN, THE AIRCRAFT DEPARTED THE LT SIDE OF THE RUNWAY. DAMAGE NOTED ON THE LOWER IB SECTION OF THE RT WING, DAMAGE NOTED ON THE RT WING IB LEADING EDGE, AND DAMAGE NOTED ON THE RT KRUEGER FLAP.SDR DXTA200702588Starter Gen · inoperativeRT GENERATOR FAILED AFTER TAKEOFF POWER , R/T GEN WOULD NOT STAY RESET NOR HOLD AMP LOAD NOR VOLTS, TO ABORTED. REMOVED AND REPLACED RH STARTER GEN PER G200 MM 24-30-06. OPS CHECK GOOD PER G200 MM 24-30-00SDR DXTA200702570Thermal Switch · inoperativeJUST AFTER ENGINE RUN-UP GOT LINE PRESSURE HIGH/OVER TEMP WARNING ILLUMINATED. WHEN THROTTLES REDUCED TO IDLE, LIGHT WENT OUT. PERFORMED ENGINE RUN, NO DEFECTS NOTED. CHECKED HP PRSOV VALVES NR 1 & 2 ENGINE; PRESSURE FROM NR 1 ENG HP PRSOV VALVE 25 PSI AND NSDR DXTA200702555Brake · wornNORMAL BRAKES INEFFECTIVE ON LANDING ROLLOUT. FOUND NR 1 BRAKE ASSY WORN. REMOVED AND REPLACED NR 1 BRAKE ASSY WITH REPAIRED UNIT IAW G-200 CMP CARD NR: 324301. PERFORMED NORMAL BRAKE SYSTEM BLEEDING IAW G-200 MM CHAPTER 32-40-20. OPS CHECK AND LEAK CHECK SATSDR DXTA200702536Slat System · malfunctionedAFTER DEPARTURE AT APPROPRIATE SPEED, WE SELECTED SLATS UP, KRUEGERS RETRACTED SLATS WENT TO AN INTERMEDIATE POSITION. FLAP/SLAT OPS CHECK I/A/W G200 MM 27-51-45 NO DEFECTS NOTED.SDR DXTA200702431Sight Glass · crackedLT ENG OIL PRESS LOW EICAS MSG ON CLIMB OUT. (OIL PRESS 5 PSI INDICATED ON LT ENG) COMPLIED WITH QRH AND SECURED/SHUTDOWN ENG. REMOVED LT ENGINE UPPER AND LOWER COWLS. FOUND OIL FILLER NECK SIGHT GLASS LEAKING. REMOVED OIL FILLER NECK SIGHT P/N 30B6275-01 NSN SDR DXTA200702363Slat System · out of rigSLATS WOULD NOT RETRACT ALL THE WAY THEY ARE STUCK IN THE MIDDLE . SEVERAL FAULTS ON THE FSEU. [08-23-07] COMPLIED WITH RIGGING BOX FUNCTION CHECK AS OUTLINED IN GULFSTREAM G200 MM 27-50-05 & FOUND FLAP/SLAT SYSTEM TO FUNCTION NORMALLY ON GROUND AT THIS TIMSDR DXTA200702291Fire Loop · malfunctionedAPU FIRE INDICATION ON GROUND. BLEW BOTTLE INTO APU DURING CHECKLIST. RT FIRE BOTTLE IS EMPTY. [07-12-07] REMOVED TAIL CONE AND INSPECTED APU FOR DAMAGE. FOUND NO DAMAGE. REMOVED APU FIRE DETECT LOOP AND INSTALLED A NEW GAC FURNISHED BOTTLE. PERFORMED SATSDR DXTA200702207Unknown · unknownAIRCRAFT WOULD NOT ROTATE WITH STICK FULL AFT. (M2B) PERFORMED HIGH ENERGY STOP INSPECTION REF MM 5-50-01, NO DEFECTS NOTED. MEASURED ELEVATOR UP AND DOWN TRAVEL, TRAVEL NORMAL. ELEVATORS MOVED WITH EASE. PERFORMED ELEVATOR CONTROL SYSTEM TRAVEL TEST AND FOUNDSDR DXTA200702191Wire · brokenRT MLG RED INDICATION IN FLIGHT W/GEAR NOT SELECTED DOWN. IT OCCURRED DESCENDING THROUGH 9000 FT. AT 250 KIAS. ACCOMPANIED BY RED GEAR SPEED LIMIT INDICATIONS. M2B- FOUND A BROKEN WIRE AND WATER IN THE BACKSHELL OF WHEEL WELL DISCONNECT 44GJ1. RE-PINNED CONNESDR DXTA200702149Monitor · inoperativeDURING POST FLIGHT, EVALUATING INOP VIDEO MONITOR SCREEN. SCREEN WAS MOVED TO VIP STATION TO DETERMINE IF MONITOR CONNECTOR WAS CONNECTED OR MONITOR ITSELF WAS INOPERATIVE. IMMEDIATELY AFTER MONITOR WAS PLUGGED IN AT VIP SEAT SMOKE WAS NOTED AT THE CONNECTIONSDR DXTA200702137Unknown · odorACRID ELECTRICAL BURNING SMELL EMINATING FROM BEHIND LT PILOT SEAT IN COCKPIT. CHECKED ALL CB'S, NOTHING FOUND (POPPED). [4-27-07] PERFORMED ENG RUN AND APCS RUNS FOR COCKPIT SMELLS, RUNS SATISFACTORY. ACCESSED L/R RELAY PANEL FOUND SATISFACTORY. ACCESSED FWSDR DXTA200702108Warning System · unknownLT ENG BLEED AIR LEAK, RED WARNING MESSAGES ILLUMINATED IN FLT-QUICK REF HANDBOOK PROCEDURES FOLLOWED IAW EH-3 BLEED AIR LEAK CHECKLIST. LT BLEED AIR LEAK REMAINED ON SO LT ENGINE SHUTDOWN IAW CHECKLIST. REMOVED DUCT COMING OFF PRSOU VALVE, REPLACED O-RINGS RESDR DXTA200702086Fire Warning · unknownAT FL-380 APU FIRE WARNING ILLUMINATED, RAN QRH CHECKLIST FIRED APU FIRE BOTTLE INDICATION DID NOT GO OUT. LANDED AT NEAREST AIRPORT. REPLACED APU FIRE DETECTOR P/N 3001-148-450-9, S/N 86516 WITH INSPECTED DETECTOR P/N 3001-148; S/N 87592 IAW G200 AMM SECTIONSDR DXTA200702061Actuator · intermittentSELECTED GEAR DOWN, THE RT MLG DID NOT SHOW DOWN & LOCKED WITH A RED INDICATION PRESENT. ON FINAL, CYCLED MLG 1 MORE TIME & INDICATION THE SAME. FLY BY TOWER & TOLD THAT THE MLG LOOKED TO BE NORMAL. ON DOWNWIND LEG AT 1500 FT AGL RED LIGHT WENT OUT & GREEN LISDR CA070514036Engine · noisy(CAN) IN CRUISE THE ENGINE EMITTED A NOISE ACCOMPANIED BY VIBRATION, A FADEC FAULT INDICATION AND FIRE WARNING INDICATION. THE ENGINE WAS SHUTDOWN IN FLIGHT. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070514036)SDR DXTA200702039Landing Gear · malfunctionedRT MAIN LANDING GEAR WOULD NOT RETRACT. HAD RED UNSAFE EICAS INDICATION. CONFIRMED DISCREPANCY. TROUBLESHOT AND DISCOVERED CONNECTOR 44G1J TO HAVE AMPLE AMOUNT OF WATER IN IT. CLEANED AND DRIED CONNECTOR AND RECONNECTED. SWUNG GEAR THROUGH SEVERAL CYCLES WITHSDR DXTA200702024Dcu · inoperativeRT MAIN LANDING GEAR WOULD NOT COME UP YELLOW INDICATOR THEN RED. CYCLED ONE TIME DID NOT CHANGE. DCU INOP. REMOVED DCU AND INSTALLED AN INSPECTED UNIT IAW CH 31-50-00 OF THE G-200 MM OPS CHECK GOOD.SDR DXTA200702020Trim System · unknownDURING CLIMB WITH THE AUTOPILOT ENGAGED THE AUTOPILOT DISENGAGED ALONG WITH ILLUMINATION OF THE A/P PITCH TRIM CAUTION MESSAGE 3 TIMES AFTER THE THIRD FAILURE THE PRIMARY PITCH TRIM WOULD NOT FUNCTION. PERFORMED HORIZONTAL TRIM SYSTEM FUNCTIONAL TEST AND RAN SDR DXTA200702005Unknown · unknown30 SECONDS AFTER TAKEOFF WE GOT STALL SYS FAIL ELEV FEEL AND STICK PUSHER FAIL, ALL CB,S WERE IN. REMOVED AND REPLACED THE SPQC WITH AN INSPECTED UNIT AND PERFORMED A COMPLETE FUNCTIONAL TEST I/A/W G200 MM 34-15-00. COMPLIED WITH CMP'S 341601 AND 2703030.SDR CA070314018Actuator · failed(CAN) ON APPLICATION OF POWER IN CLIMB, THE ENGINE EXPERIENCED A COMPRESSOR STALL ACCOMPANIED BY AN UNCOMMANDED POWER REDUCTION, PARAMETER FLUCTUATIONS AND A FADEC FAULT INDICATION. SUBSEQUENT INVESTIGATION LED TO REPLACEMENT OF THE ENGINE INLET GUIDE VANE ACSDR CA070220006Actuator · leaking(CAN) AC PERFORMED NORMALLY FOR THE TAKEOFF AND INITIAL CLIMB TO 5000 FEET. APPROX (2) MINUTES INTO THE FLIGHT AFTER CLEARANCE TO 17000 FT WITH CLIMB PWR REAPPLIED TO COMMENCE THE CLIMB, THE RT ENG EXPERIENCED A COMPRESSOR STALL. AFTER (2) OR (3) SURGES THE ENSDR DXTA200701920Control Unit · malfunctionedRT BLEED AIR LEAK CAME ON IN FLIGHT, WARNING MESSAGE STAYED ON DURING ALL PROCEDURES ON EH-3 OF THE QRH. ENGINE WAS SHUTDOWN INFLIGHT. NO SMOKE OR FIRE REPORTED BY FIRE DEPARTMENT. REMOVED AND INSTALLED NEW RT BLEED AIR CONTROL UNIT IAW G-200 MM / CH 21-61-00SDR DXTA200701915Motor · malfunctionedAUTO PILOT DISENGAGES ON APPROACH IN ALL MODES AND DURING TURNS. ALSO, IN STRAIGHT FLIGHT, YOKE JERKS RT AND LT ROUTINELY ABOVE MACH .78. FOUND THE RUDDER SERVO MOTOR, AUTOPILOT TO BE FAULTY. REMOVED AND REPLACED THE AUTOPILOT RUDDER SERVO MOTOR WITH AN OVERSDR DXTA200701896Unknown · unknownELEVATOR FEEL FAIL LIGHT CAME ON IN CLIMBOUT. REMAINED ON, THE ENTIRE FLIGHT. UPON A/C ARRIVAL VERIFIED DISCREPANCY AND NOTED THAT THE SPQC WAS NOT FULLY INSTALLED IN RACK, RERACKED SPQC AND MESSAGE EXTINGUISHED. PERFORMED A SPQC DOWNLOAD AND OPS CHECK WITHSDR DXTA200802817Ecu · inoperativeDURING APU SHUTDOWN FLAMES WERE COMING OUT OF EXHAUST, NO FIRE WARNING LIGHTS OR MSG OF ANY KIND. OPENED UP APU FIRE SWITCH AND DISCHARGED RT FIRE BOTTLE INTO APU, FIRE EXTINGUISHED. M2B- INSPECTED APU AND TAIL CONE AREA FOR DAMAGE NONE NOTED. PERFORMED ALERSDR DXTA200701876Warning System · activatedL BLEED AIR MESSAGE ILLUMINATED IN FLIGHT AS DIRECTED BY THE CHECKLIST THE LT ENGINE WAS SHUTDOWN BY CREW BECAUSE THE MESSAGE REMAINED ON AFTER X-LIST ITEMS WERE COMPLETED SIDE NOTE ENGINE EVENT BUTTONS WERE PRESSED ABOUT 45 SECONDS AFTER MESSAGE ILLUMINATED. SDR DXTA200701874Trim System · failedAUTOPILOT PITCH TRIM FAILED AFTER TAKEOFF WE WERE UNABLE TO CONTROL TRIM W/YOKE THUMB SELECTOR AUTOPILOT WAS FUNCTIONAL AFTER WE TRIMMED AIRCRAFT IN SECONDARY DISCONNECT POSITION TRIM BECAME SEMI FUNCTIONAL UPON ARRIVAL. TROUBLESHOT SYSTEM AND DETERMINED THATSDR DXTA200701853Float Valve · leakingINFLIGHT NOTICED FLUID TRAILING OFF OF THE RT AILERON. ON THE GROUND THE VISIBLE TRAIL DISAPPEARED BUT THERE IS RESIDUAL FUEL POCKET ON THE RT AILERON. REMOVED FUEL PANELS 640NT, 640MB. REMOVED FLOAT VALVE P/N D25W652004-507 S/N 214. INSTALLED NEW FLOAT VASDR DXTA200701850Fire Loop · failedRT ENG FIRE DETECT CAS MSG ILLUMINATED RT AFTER ENGINE START. REPLACED RIGHT ENGINE ZONE 2 DETECTOR & FIRE LOOP CMP 261102 W/O REF FL008823SDR DXTA200601822Transfer Pump · inoperativeCROSS FEED (ON) IN AIR (2 OCCASIONS). CROSS FEED VALVES FAILED TO OPEN, BOTH FUEL BOOST PUMPS (LOW PRESS) CAME ON. EICAS MESSAGES APPROPRIATE AMBER FUEL PRESS LOW L-R ON. TROUBLESHOT PROBLEM TO LT BOOST PUMP. REMOVED FAILED BOOST PUMP AND INSTALLED A NEW BOOSDR DXTA200601798Handle · lack of lubeEMERGENCY EXIT EICAS MESSAGE CAME ON CLIMBING THROUGH 10,000 FT AND WENT OUT DESCENDING THROUGH 4,000. FOUND EMERGENCY EXIT HANDLE OUT OF ADJUSTMENT. READJUSTED E-EXIT HANDLE AND LUBED HANDLE IAW G200 MM 52-20-00. OPS CHECKED GOODSDR DXTA200601794Bleed Valve · stuckAT 4000 FT AND 250 KTS AT APPROXIMATELY 75% NI WE HEARD A BANG FROM THE REAR OF THE AIRCRAFT .ADDITIONALLY THE LEFT ENG VIBRATION GAGE INDICATION SIGNIFICANTLY HIGHER THAN THE RIGHT ENG. AFTER LANDING WE NOTED EXCESSIVE OIL ON THE LEFT WING. INSTALLED (1) 2.5SDR CA070103007Pump · malfunctioned(CAN) ENGINE OIL PRESSURE WAS REPORTED TO GRADUALLY DECREASE AND THE ENGINE WAS SHUTDOWN IN FLIGHT. THE AIRCRAFT DIVERTED FOR AN UNSCHEDULED LANDING. THE ENGINE OIL PRESSURE PUMP WAS SUBSEQUENTLY REPLACED. (TC NR 20070103007)SDR DXTA200601753Control Cable · lack of lubeGEAR HANDLE IS VERY HARD TO MOVE UP OR DOWN. IT ALMOST TAKES TWO HANDS TO RETRACT GEAR UP. NOT AS BAD SELECTING GEAR DOWN BUT STILL HARDER TO DO THAN NORMAL. REMOVED LANDING GEAR CONTROL CABLE AT GEAR CONTROL HANDLE AND LANDING GEAR SELECTOR VALVE. CLEANED ANDSDR DXTA200601738Control Valve · inoperativeAFTER TAKEOFF GEAR HANDLE WOULD NOT COME UP. TRIED TO PRESS DOWNLOCK OVERIDE AND GEAR HANDLE WOULD NOT MOVE. REPLACED LANDING GEAR CONTROL ASSY. PERFORMED DOWNLOCK SOLENOID / OVERIDE OPERATIONAL CHECK IAW G200 MAINT. MAN CH. 32-30-00. NO DEFECTS NOTED AT THISDR DXTA200601744Unknown · odorAFTER TAKEOFF HAD A SMOKE OIL ODOR IN THE COCKPIT FOR ABOUT 10- 20 SECONDS, THEN IT WENT AWAY. LATER INFLIGHT THE PASSENGERS CAME UP AND SAID THAT THEY SAW A SMOKE HAZE BEHIND THE GALLEY IN THE MAIN CABIN . INSPECTED AMPLIFIER AND CONNECTIONS BEHIND GALLEY. NOSDR DXTA200601736Audio/Video Unit · failedWITH THE AIRCRAFT ON THE GROUND, CABIN DOOR OPEN, APU ON , APU BLEED AIR ON CABIN UPPER LTS ON, LOWER CABIN LTS ON , AIRSHOW ON, A STREAMING PUFF OF SMOKE EMITTED FROM THE LT UPPER SIDEWALL ABEAM, SEAT NR 3 AND THE SEAT NR 3 ENTERTAINMENT CONTROL PANEL. CABISDR DXTA200601663Fire Detector · failedDURING DESCENT ( R ENG FIRE DETECT) AMBER MESSAGE ILLUMINATED AND REMAINED ON. TROUBLESHOT RT ENG- FIRE DETECT SYSTEM, FOUND ZONE 2 FIRE LOOP INOP. REMOVED AND REPLACED RT ENGINE ZONE 2 FIRE LOOP WITH (NEW) UNIT IAWMM 26-10-10 AND CMP'S 261102, 783010, 714202
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