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 CA101004009Actuator · failedSEPTEMBER 30/2010 PILOTS REPORT ELEVATOR FEEL FAIL REPEATEDLY ILLUMINATION IN FLIGHT. TROUBLESHOT BY MFG, ACFT HYD SYS BLED AND ACFT RELEASE FOR RETURN TO SERVICED. OCTOBER 01/2010, PILOTS REPORT ELEVATOR FEEL FAIL BETWEEN 1-6 TIMES IN FLIGHT, TROUBLESHOT ANDSDR CA101006004Bleed Valve · failedLOW OIL PRESSURE/IFSD JUST AFTER LANDING, THE CREW OBSERVED A LOW OIL PRESSURE WARNING, HIGH TEMP AND DECAYING ENGINE PARAMETERS. THE ENGINE WAS SHUTDOWN AND THE ACFT TAXIED TO THE RAMP. SUBSEQUENT GROUND RUN SHOWED THE ENGINE HANGING AT 25 PERCENT N2, CONFISDR DXTA2010092004244Display · intermittentCOPILOT'S PFD TURNS ON AND OFF INTERMITTENTLY. REMOVED CO-PILOT MFD. CHECKED THE FILTER SCREEN ON BACK OF MFD. FOUND DEBRIS ON SCREEN. REMOVED AND CLEAN ALL DEBRIS FROM THE FILTER SCREEN. RE-INSTALLED THE CO-PILOT MFD INTO ITS ORIGINAL POSITION. OPS CHECKSDR CA100921003Engine · leakingSMOKE IN CABIN DURING CLIMB AT FL 50, SMOKE STARTED ENTERING THE CABIN. THE CREW ELECTED TO RETURN TO THE POINT OF DEPARTURE WHERE AN UNEVENTFUL LANDING WAS MADE. POST FLIGHT INSP FOUND OIL ON THE FAN AND THE CABIN BLEED PORT. TROUBLESHOOTING IS ON-GOING.SDR DXTA2010090704221Slat System · bindingFLAPS JAMMED AT 18 DEGREES AT 400 AGL AFTER TAKEOFF. FLAP HANDLE PLACED TO 20 & FLAPS & KRUEGERS RETURNED. FLAPS 0 SELECTED & FLAP RETRACTED TO 0. SLATS 0 SELECTED & SLATS JAMMED AT APPROX 2-3 DEGREES. FLAP HANDLE MOVED TO VARIOUS POSITIONS, SLATS REMAINED JSDR DXTA2010071604156Turbine Blades · crackedABOUT 45 MINUTES INTO THE FLIGHT, CLIMBING THRU FL 360, CREW HEARD A LOUD "BANG", FELT A VIBRATION, ITT BEGAN AN IMMEDIATE CLIMB, FOLLOWED BY THE "FIRE" LIGHT AND SMOKE IN THE CABIN. CREW BROUGHT THE THROTTLE TO IDLE, SHUT THE ENGINE DOWN VIA THE FUEL CUTOFF SSDR CA100726007Engine · vibrationDURING REVENUE FLIGHT, LT ENGINE WAS SHUTDOWN BY CREW DUE TO VIBRATION INDICATOR AT MAX LEVEL WITH CORRESPONDING RISING ITT AND ENGINE FIRE CAS MESSAGE. THERE WAS ALSO THE ODOR OF SMOKE IN THE CABIN, BUT NOT VISIBLE. ACFT DIVERTED. MFG LOCAL FIELD SUPPORT SDR DXTA201007160415Engine · overtempRT ENGINE SHUTDOWN INFLIGHT DUE TO VIBRATION DETECTOR AT MAX LEVEL WITH CORRESPONDING RISING HIGH ITT LEVEL (NOT IN RED) AND ENGINE FIRE CAS MESSAGE. THERE WAS ALSO THE SMELL OF SMOKE IN THE CABIN BUT NOT VISIBLE. ENGINE WAS SECURED BY POWER TO IDLE AND FUELSDR 2010FA0000759Cable · damaged(K5SR) WHILE PERFORMING A 500 HR/12 MONTH INSP ON THE LT ENGINE, DISCOVERED THE EMERGENCY FUEL SHUTOFF CABLE HAD UN-TWISTED AT THE CABLE END GOING FROM THE FUEL SHUTOFF VALVE. R & R WITH NEW CABLE ASSY. OPD CKD SATISFACTORY.SDR DXTA2010063004134Engine · overservicedAT FL190 EXPERIENCED SMOKE IN CABIN AND COCKPIT. WENT THRU SMOKE ELIM PROCEDURES AND SELECTED LT ENGINE ECS. SMOKE STOPPED BILLOWING AND SLOWLY DISAPPATED. SMELL REMAINED. EXPERIENCED SAME ODOR ON PREVIOUS LEGS WITH THROTTLES IN A MIDRANGE POSITION. EXTERNASDR CA100629005Limiter · intermittent(CAN) SLATS FAIL ON THREE OCCASIONS. SLAT FAIL TO RETRACT- INOP, MAY 17TH 2010. THE SYSTEM WAS TROUBLE SHOOT BY GULFSTREAM USING TEST BOX TO CHECK FAILURE, SYSTEM STARTED TO OPERATE PROPERLY COULD NOT DUPLICATE PROBLEM. THE SLAT SYSTEM WAS INSPECTED AND NR 3SDR DXTA2010060904118Selector Valve · leakingAFTER TAKEOFF AND ON INITIAL GEAR RETRACTION, RT HYD PUMP PRESS LOW, AUX HYD PUMP ON, AND RT HYD LOW LEVEL CAUTION MESSAGES ILLUMINATED. FLUID QTY LEVEL WAS AT 24 ON RT HYD SYS. RAN QRH PROCEDURES AND LANDED SJC. ON POSTFLIGHT, HYD FLUID NOTED ON BOTTOM ON PLASDR DXTA2010060104107Actuator · faultyUPON LANDING GEAR EXTENTION THE RT MLG SHOWED A AMBER UNKNOWN POSITION THEN A RED UNSAFE POSITION. AFTER A MINUTE IT SHOWED A DOWN AND LOCKED POSITION. REMOVED RT MLG HYD ACTUATOR AND INSTALLED MODIFIED UNIT IAW CMP 321004. OPS AND LEAK CHECKS GOOD.SDR DXTA2010052404097Control Unit · bindingON APPROACH AFTER DISENGAGING THE AUTO PILOT/YAW DAMP AT 180KTS THE ACFT WOULD ONLY ROLL (5) DEGREES TO THE RT. BOTH THE CAPTAIN AND COPILOTS CONTROLS SEEMED JAMMED. ONCE ON THE GROUND WE ARE ABLE UNJAM THE CONTROLS WITH FULL MOVEMENT. REPLACED AILERON AFU.SDR DXTA2010051704094Switch · out of adjustON TAKEOFF, AFTER SELECTING GEAR UP, IT SEEMS LIKE ALL THE GEAR RETRACT NORMALLY EXCEPT THE LT MAIN INDICATES RED HASH MARKS. THE OTHER (2) INDICATE UP, BUT THE LT MAIN STAYS RED HASH MARKS. IT STAYS THIS WAY WITH NO CHANGE OR INPUT FROM US FOR 3 TO 4 MINUTES SDR DXTA2010041904071Windshield · failedRT WINDSHIELD SHATTERED DURING FLIGHT. REPLACED COPILOT WINDSHIELD WITH NEW. OPS/LEAK CHECKS GOOD. DONE IAW MM 56-10-05.SDR 2010FA0000159Landing Gear · malfunctionedNOSE GEAR DOES NOT INDICATE DOWN AND LOCKED AFTER PULLING EMERGENCY GEAR HANDLE.SDR CA100224002Engine · noisy(CAN) ABORTED TAKEOFF: DURING REVENUE FLIGHT ON TAKEOFF ROLL, THE PILOT REPORTED LOUD NOISES AND DECIDED TO ABORT THE TAKEOFF. THE ENGINES ARE BEING TROUBLESHOT FOR POSSIBLE SURGES.. (TC 20100224002)SDR CA100117005Oil System · low pressure(CAN) DURING TAXI, THE RT ENGINE WAS SHUTDOWN FOLLOWING A LOW OIL PRESSURE WARNING AND A HIGH ITT INDICATION. THE EDU DOWNLOAD SHOWED A SUDDEN RISE IN T45 WITH A GRADUAL DECREASE IN N2 SPEED. THE ENGINE WILL BE REMOVED FOR REPAIR. THERE IS NO TROUBLESHOOTING ISDR CA091008005Trim Tab · cracked(CAN) THIS WAS FILED ON SEPT 30/2009. DID NOT GET ANY CONFORMATION RESUBMITTED OCT 8TH 2009. CRACK ON FWD AND AFT ENDS OF RUDDER TRIM TAB LWR ROD, FROM ACTUATOR BELLCRANK TO RUDDER TRIM TAB. THIS WAS FOUND DURING SCHEDULE MX ON THE ACFT WHILE CARRYING OUT (A) SDR CA090724004Fire Loop · failed(CAN) ON CLIMB OUT AT APPROX 18,000 FEET, ACFT ROUTED ON EICAS THE PILOTS REPORTED THAT THE LT ENG FIRE DETECTOR INDICATED FAILED. PILOTS REPORTED THAT CHECK LIST HAD BEEN COMPLETED AND AS A PRECAUTIONARY MEASURE PROCEEDED TO SHUTDOWN ENG IN FLIGHT. ACFT WASSDR CA090727004Actuator · binding(CAN) PILOTS REPORTED ALL SYS NORMAL. ON PRE-FLIGHT THE PILOTS COULD NOT GET THE SLATS TO MOVE WHEN SELECTED FLAPS DOWN. MX WAS CALLED AND COULD NOT DETECT WHAT WAS FAILED ON THE SYS. ACFT PROCEEDED TO COMPLETE A FERRY FLIGHT WITH SLATS RETRACTED USING BYPASDR CA090715002Terminal · misinstalled(CAN) WHILE CONDUCTING THE 1200HR INSP OF THE RT WINDSHIELD ‘ANTI STATIC COATING’ ON G200, IT WAS FOUND UNSERVICEABLE AND DID NOT MEET THE SPEC BY THE MFG IAW MM. THIS REQUIRED WIND-SHIELD REPLACEMENT. ON REMOVAL OF THE WINDSHIELD, FOUND ONE (1) OF THE PWR CASDR DXTA2009070203712Engine · overservicedDURING CLIMB OUT COCKPIT FILLED WITH WHITE SMOKE (SMELLED AND TASTED ELECTRIC) DISCONNECTED GALLEY ELECTRIC NO CHANGE, DUMPED CABIN SMOKE, DISSIPATED TEMPORARILY THAN RETURNED. RETURNED TO DEPARTURE. FOUND LT ENGINE OVERSERVICED WITH ENGINE OIL. DRAINED ENGISDR DXTA2009062903707Oil System · overservicedDURING CLIMBOUT COCKPIT FILLED WITH WHITE SMOKE (SMELLED AND TASTED ELECTRIC). DISCONNECTED GALLEY ELECTRIC, NO CHANGE. DUMPED CABIN, SMOKE DISSIPATED TEMPORARILY THEN RETURNED. FOUND LT ENG OVERSERVICED WITH ENGINE OIL. DRAINED ENGINE OIL TO PROPER LEVEL SDR CA090601002Wire · broken(CAN) PILOT`S SIDE PITCH TRIM SWITCH IN-OP. MX INVESTIGATED AND FOUND PITCH TRIM WAS INTERMITTENT WHEN THE CONTROL COLUMN WAS OPERATED AFT (PULLED AFT). FLOOR ACCESS PANELS REMOVED IN COCKPIT AREA AND FOUND HARNESS ROUTING VERY TIGHT. ALLOWING WIRES TO WORK ASDR DXTA2009022303520Engine · hung startDURING A MAINTENANCE TASK, RT ENGINE (RT) HAD A HUNG START NO LIMITATIONS WERE EXCEDED NOTED A ODOR AND SMOKE AT S/G EXHAUST.SDR DXTA2009022003520Contactor · inoperativeCHANGED CONTACTOR 60P. PERFORMED SEVERAL NORMAL ENG STARTS AND SEVERAL ABORTED STARTS WITH NO DEFECTS NOTED. COULD NOT DUPLICATE SQUAWK. REF TO GDAS BAF WO NJ2962.1.9 DATED 3/2/09 FOR DETAILS.SDR DXTA2009010103451Fan Blade · damagedON PREFLIGHT WE DISCOVERED DAMAGE TO 2 OF THE LT ENGINE FAN BLADES THERE IS ALSO DAMAGE TO THE ENGINE SHROUD AT THE 7 O`CLOCK POSITION. REPLACED 3 FAN BLADES, FAN EXIT VANE RING, FAN CASE, AND INLET COWL. PERFORMED A SATISFACTORY 5 POINT GROUND PERFORMANCE RUSDR J1QA20081019001Sensor · failedAIRCRAFT DEPARTED KPSP, DURING CLIMB OUT AT 14,000 FEET THE AMBER "EMERGENCY BATTERY OVERHEAT" LIGHT CAME ON. CREW CHECKED THE BATTERY TEMPURATURE AND THE READING WAS 140 DEGREES F AND CLIMBING. THE CREW PER THE CHECKLIST TURNED OFF THE "EMERGENCY BATTERY". SDR CA081016014Fuel Control · malfunctioned(CAN) 2 TO 3 MINUTES AFTER ENGINE START, IT FLAMED OUT UNCOMMANDED. NO FAULT CODES WERE RECORDED ON THE FADEC. INSPECTION FOUND THE FAN FREE TO ROTATE WITH NO EVIDENCE OF INGESTION. THE PILOT MOTORED THE ENGINE AND THEN PERFORMED AN ENGINE START. THE BOOSTSDR YRR2008F00000Blower · failedTHE ACFT WAS LEVELING OFF AT CRUISE ALTITUDE OF FL400 AFTER DEPARTING AND ENROUTE, WHEN THE CREW NOTED THE ODOR OF SMOKE AND SMOKE COULD BE SEEN COMING FROM THE AFT SECTION OF THE CABIN. THE CREW DECLARED AN EMERGENCY AND BEGAN A DESCENT WHILE COMPLETING THE SDR DXTA200803056Connector · contaminatedAFTER TAKEOFF, RT MLG WOULD NOT RETRACT WHEN GEAR WAS SELECTED UP.SDR DXTA200803042Engine · vibrationCLIMBING THROUGH 12,000 FEET HEARD A LOUD BANG, THE RIGHT ENGINE, VIB INDICATOR TURNED YELLOW AND CLIMBED ABOVE THE 3RD TICK MARK ON THE RIGHT ENGINE. THE ENG LOST SOME OIL PRESSURE BUT STAYED IN THE GREEN. ALL OTHER PARAMETERS STAYED IN THE GREEN. ENG HAD SDR DXTA200803024Display · malfunctionedCO-PILOT'S MFD WENT IN-OP IN FLT WITH A BURNING SMELL. REMOVED DISPLAY & INSTALLED PER CMP 342304 GAC SAV W/O 142032 SQUAWK 6.1 OPS CHECK GOOD NO DEFECTS NOTED.SDR DXTA200802998Engine · overservicedSHORTLY AFTER ROTATION THERE WAS AND OVERWHELMING ODOR SIMILAR TO BURNED RUBBER. INSPECTED LT & RT ENGINES FOR ABNORMAL CONDITIONS, INSPECTED ECS SYS, FOUND NO DEFECTS. TECHS PERFORMED ENGINES RUN. AN ODOR LIKE BURNED OIL FROM LT ENGINE AT BOTH LOW & HIGH POWESDR DXTA200802991Brake Assy · weakMAIN BRAKES REQUIRE EXCESSIVE PRESSURE ON TOE BRAKES TO SLOW OR STOP ACFT. REMOVED AND REPLACED NR 2 BRAKE REF MM 32-40-21 REF CMP 324302 COMPLIED WITH BRAKE BLEED AND OPS CHECK REF CMP 324005 AND 324017.SDR DXTA20082986Warning Message · illuminatedAFTER TAKEOFF, ELEVATOR FEEL FAIL MESSAGE CAME ON.SDR DXTA20082970Slat System · malfunctionedON DEPARTURE, GOT FLAP / SLAT MAINT MESSAGE. SLATS DID NOT COME ALL THE WAY UP. PERFORMED FUNCTIONAL TEST OF THE FLAP/SLAT CONTROL AND DRIVE SYSTEM WITH NO DEFECTS NOTED AT THIS TIME. ALL WORK COMPLETED IAW CMP 275101.SDR DXTA200802970Slat · malfunctionedON DEPARTURE, GOT FLAP/SLAT MAINT MESSAGE. SLATS DID NOT COME ALL THE WAY UP. PERFORMED FUNCTIONAL TEST OF THE FLAP/SLAT CONTROL AND DRIVE SYS WITH NO DEFECTS NOTED AT THIS TIME. ALL WORK COMPLETED IAW CMP 275101.SDR DXTA20082966Control Unit · inoperativeLEAVING TQPF AFTER GEAR RETRACTION, SELECTED FLAPS TOP 0 DEG AND FLAPS WOULD NOT RETRACT FROM 20 DEG. REMOVED ORIGINAL FSECU AND INSTALLED INSPECTED UNIT. PERFORMED SATISFACTORY RIG AND OPS CHECK OF FLAP SLAT SYSTEM. FOR ALL WORK REF MM 27-51-00, 27-50-05 ANDSDR DXTA200802966Fseu · inoperativeLEAVING, AFTER GEAR RETRACTION, SELECTED FLAPS TOP 0 DEG AND FLAPS WOULD NOT RETRACT FROM 20 DEG. REMOVED ORIGINAL FSECU AND INSTALLED INSPECTED UNIT. PERFORMED SATISFACTORY RIG AND OPS CHECK OF FLAP SLAT SYSTEM. FOR ALL WORK REF MM 27-51-00, 27-50-05 AND 27-SDR DXTA20082955Fuse · failedAFTER ENGINE START (BOTH ENGINES STARTED) WITH ECS SELECTOR STILL IN (RAM), APU FIRE WARNING MESSAGE ILLUMINATED. T/S FOUND BLOWN FUSE 405. REPLACED FUSE WITH NEW PART. OPS CHECK GOOD. IAW MM 26-10-25.SDR DXTA20082943Warning Light · illuminatedON TAKEOFF ROLL AT APPROX 60 KIAS, WE GOT A L. BLEED PRESS/TEMP HI CAS. PERFORMED APU & ENGINE RUNS WITH BLEEDAIR SELECTED ON BOTH ENGINES WITH NO DEFECTS NOTED. THEN PERFORMED BLEED AIR SELECTED ON APU WITH NO DEFECTS NOTED AT THIS TIME WITH ENGINES & APU RUSDR DXTA20082944Autopilot Sys · failedAUTO PILOT PITCH FAILED. PERFORMED HORIZONTAL STABILIZER TRIM SYSTEM INTERFERENCE TEST, TRAVEL TEST, AND FUNCTIONAL TEST I.A.W. G200 M.M. 27-40-00. OPS CHECK GOOD.SDR DXTA20082940Circuit Breaker · trippedCLIMBING THROUGH FL 3111 I HEARD A CB POP, FOLLOWED BY NUMEROUS EICAS CAUTION AND WARNING MESSAGES. TROUBLESHOT SYSTEM, FOUND CB135P EMERGENCY BUSS BATTERY CB (60 AMP) TO BE DEFECTIVE. REPLACED CB135P AND PERFORMED GCU OPERATIONAL TEST AND DC LOAD SHEDDING OPSDR DXTA20082934Brake · weakBRAKES ARE VERY SOFT AND WONT GRAB ON LANDING ROLLOUT UNTIL ABOUT 30 KNOTS (BOTH CAPTAIN AND PILOT SIDES). BLED BRAKES AFTER INSPECTION FOUND BRAKES WERE WITHIN TOLERANCE. NO AIR NOTED AT THIS TIME. WORK DONE IAW MM 32-40-20.SDR DXTA20082925Adapter · dirtyON APPROACH TO ASE, SELECTED GEAR DOWN AND GOT RED HASH MARKS ON NOSE GEAR. TROUBLESHOT SYSTEM FOUND ON VISUAL INSPECTION OF NOSE GEAR TOW ADAPTOR WOULD NOT SPIN TO THE DOWN POSITION. REMOVED TOW ADAPTOR, CLEANED DEBRIS, LUBED, INSTALLED, OPS CHECK GOOD. CSDR DXTA20082916Actuator · leakingAFTER TAKEOFF AND ON SPEED, RETRACTED KRUEGERS FROM FLAPS UP POSITION TO KRUEGER/SLATS UP POSITION. THE KRUEGER UNBAL CAS MSG ILLUMINATED WITH KRUEGER POINTER INDICATOR YELLOW. FOUND THE RT KRUEGER ACTUATOR TO BE LEAKING. REMOVED ACTUATOR AND REPLACED WITH INSDR DXTA20082887Control Unit · inoperativeON DEPARTURE, RECEIVED (KRUEGER IMBALANCE) CAS MESSAGE. REMOVED AND REPLACED FLAP/SLAT ELECTRIC CONTROL UNIT. PERFORMED FUNCTIONAL TEST WITH NO DEFECTS NOTED. ALL WORK DONE IAW MM CHAPTER 27-51-45 AND CHAPTER 27-52-00. (SQK NR 1.4)
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