Pratt & Whitney JT8D-219
Service difficulty reports · 1,944
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 = 'JT8D219' 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 = 'JT8D219' 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 2008FA0000473Engine · vibrationCAPTAIN REPORTED STRONG VIBRATION IN RT ENGINE WITH EPR`S BETWEEN 1.7 AND 1.75. TECHS VERIFIED THE RT ENGINE CONDITION AND PERFORMED OPERATIONAL TEST IAW AMM 71-00-01 FOUND ALL CORRECT. VIBRATION WAS WITHIN LIMITS (0.4 UNITS INDICATED). (K)SDR AALA200801541Turbine Blades · failedDFW INFLIGHT T1853/06JUN. CREW REPORTED LOUD NOISE FOLLOWED BY ENGINE GAS TEMPERTURE GOING TO 800 DEGREES. NR ONE ENGINE WAS SHUTDOWN BY CREW. LANDED DFW WITHOUT INCIDENT. SINGLE ENGINE TIME SIX MINUTES. FOUND TURBINE BLADE FAILURE AND METAL IN TAIL PIPE.SDR DLM88080820Engine · power lossAT CRUISE HAD LT ENG EPR 1.40 AND RT ENG EPR 1.88 WITH BOTH N1'S AT 75. COULD ONLY CLIMB AT 500 FPM AT 300 KIAS. PRESSURE CHECKED PT2 AND PT7 LINES NR 1 AND NR 2 ENGS. FOUND P FLEX LINE THRU PYLON LEAKING ON NR 2 ENG. REPLACED LINE. PUM EPR SYSTEM UP WITHSDR ASMF200805005Csd · damagedDURING PUSH BACK, CAPTAIN REPORTED THAT AFTER STARTED THE LEFT ENGINE, THE CSD LIGHT TURNED ON AND TEMPERATURE REACHED 150 DEGREES CELSIUS, SO ABNORMAL PROCEDURE WAS ACCOMPLISHED. MAINTENANCE PERSONNEL DETECTED THE LEFT CSD OIL LEVEL IN RED RANGE, SO THE EXCESDR DLM88080719Battery Pack · inoperativeEMERGENCY LIGHTS WOULD NOT TEST FROM FWD FLIGHT ATTENDANT PANEL DURING LAYOVER. REPLACED EMERGENCY LIGHT BATTERY PACK B5-49 FOR OVERWING LIGHTS. CHECKS GOOD.SDR AALA200801180Engine · leakingCOS INFLIGHT T656/02MAY SAN TO ORD - NUMBER TWO ENGINE COMPRESSOR STALLED. HIGH ENGINE GAS TEMPERATURE NOTED. CREW SHUT NUMBER TWO ENGINE DOWN. LANDED COS WITHOUT INCIDENT. SINGLE ENGINE TIME TWENTY FIVE MINUTES. REPLACED NUMBER TWO ENGINE DUE TO OIL QUANSDR DLM88080649Pump · inoperativeRIGHT ENGINE HYDRAULIC PUMP FAILED IN FLIGHT, ZERO PRESSURE PRESSURE GOOD WITH AUX HYD PUMP, RETURNED TO ATL. REPLACED ENGINE HYDRAULIC PUMP, CASE DRAIN AND PRESSURE FILTERS. REPLACED RT HYDRAULIC SYSTEM MAIN FILTERS- OPERATED ENGINE PRESSURE CKS GOOSDR DLM88080616Csd · unserviceableLEFT GEN FAILED DURING INITIAL CLIMB-OUT WITH AN OPEN BUS TIE THE APU GEN WAS RUNNING AT THE TIME AND CARRIED THE LEFT GEN LOAD FWD LT GEN TO MCO AND PLAC PER MEL24-00-01A LT CSD DISC VERIFIED APU OIL FULL AND PERFORMED A CROSSTIE CK. CKD GCU. NO FAULTS. CHSDR DLM88080598Relay · stuckOUTBOUND CREW OF FLT 782 CALLED MTC TO REPORT CLOCKS INOP. MX FOUND THE MAIN BATTERY CHARGER INOP AND BATTERIES LOW. REPLACED CHARGER AND BATTERIES AND CLEARED ITEM. WHEN CREW NEXT ATTEMPTED TO START APU THEY HAD A FAULT LIGHT AND ECU FAULTED THE STARTER MOSDR DLM88080565Compressor · stalledPOSSIBLE COMPRESSOR STALL LT ENGINE ON TAKEOFF ROLL, REJECTED TAKEOFF ROLL AT 75 KTS. MTC IN PROGRESS REPLACING LT ENGINE.SDR 070192Engine · malfunctionedFLT 400, FLIGHT CREW REPORT RIGHT ENGINE BANG AND A DECREASE IN EPR INDICATIONS, RETURNING TO NORMAL. SUBSEQUENTLY 2 MORE BANGS FROM THE RIGHT ENGINE AND THE CREW ELECTED TO SHUTDOWN THE RIGHT ENGINE AND RETURN. MAINTENANCE PERSONNEL REMOVED AND REPLACED THESDR DLM88080518Connector · damagedFOUND SEAT 26CD EMERGENCY LIGHT INOP. SECURED PIN INTO CONNECTOR OF LIGHT ASSY, OPS OK.SDR DLM88080445Engine · malfunctionedTAKEOFF DISCONTINUED AT 100KTS BECAUSE EPR WOULD NOT RISE ABOVE 1.68 AND N1 BEGAN TO FLASH AT 102 PERCENT. REMOVED AND REPLACED NR 2 ENG EPR TRANS AND SNUBBER PER MM. COMPLETE THRU 77-11-02-201 ST 3.B.11 984600. C/W EPR IND SYS OPR NR 2 ENG PER AMM. CKS NOSDR DLM88080376Engine · damagedNR 1 ENGINE FAILURE ON T/O ROLL, HIGH VIBE ENGINE SHUT DOWN HOT SECTION MISSING BLADES ETC. REMOVED AND REPLACED NR 1 ENGINE PER TRANS 9T102.SDR ASMF200802008Control Cable · brokenDURING TAXING, CAPTAIN REPORTED STEERING FAILURE. MAINT CHECKED THE STEERING BY-PASS, FINDING ALL CORRECT; THEN, THE STEERING VALVE WAS CHECKED, DETECTING THE STEERING CONTROL CABLE BROKEN, AC WAS SENT TO THE HANGAR AND THE CONTROL CABLE WAS REPLACED AND ADJUSSDR DLM88080252Duct · failedAFTER SELECTION CLIMB POWER GOT A FIRE LIGHT ON NR 1 ENGINE FOLLOWED BY A BELL, RETARDED ENG TO IDLE AND LIGHT WENT OUT. INSP AREA FOUND WIRING AROUND NOSE ANTI-ICE VALVE DAMAGED. FOUND DUCT BLOWN APART. REPLACED DUCT. AFT CLAMP SECURED, FWD LOOSE NEEDS MISDR DLM88080243Oil Cooler · unknownNR 1 ENG GEN/CSD OIL TEMP RUNNING IN YELLOW BAND IN CLIMB AND UPON REACHING RED BAND AT TOP OF CLIMB DISCONNECTED CSD. APU GEN ALREADY ON MCO- DIVERTED TO IAD. REMOVED AND REPLACED LEFT CSD AND GENERATOR PER AMM 426246 ENGINE DISCONNECT AND RECONNECTED CSD LSDR DLM88080212Engine · damagedON DEPARTURE, A LOUD BANG WAS HEARD FOLLOWED BY RIGHT ENGINE ROLLBACK. IDLE OIL PRESS OK. QRH FOLLOWED WITH NO OTHER SIGNIFICANT ISSUES NOTED. REPLACED RT ENGINE PER TRANSMITTAL 9T102.SDR ASMF200802005Unknown · unknownAC RETURNED TO PLATFORM DUE TO IGNITION FAILURE IN LT ENGINE. MAINT REPLACED IGNITION BOX IAW MM 74-10-01, TESTED CORRECT. AC WAS DISPATCHED AND RETURNED TO PLATFORM AGAIN DUE TO THE SAME FAILURE. LT ENGINE WAS STARTED WITH EMERGENCY INVERTER, AND BREAKERS R2-SDR DL764080187Actuator · leakingCENTER HYDRAULIC QUANTITY DROPPED AT 28 PERCENT IN FLIGHT FL 300. FOUND RT MLG RETRACT ACTUATOR LEAKING. REPLACED ACT PER M/M LEAK CHECK GOOD.SDR ASMF200802004Wire · damagedAC RETURNED, DUE TO TRANSPONDERS FAILED AND NO RADAR CONTACT WAS REPORTED BY CONTROL TOWER. MAINT PERFORMED AUTO TEST IN THE TRANSPONDER 1 AND 2 IAW MM 34-54-00, ALL CORRECT. AC WAS SENT TO THE HANGAR AND SYSTEMS WERE TESTED WITH TESTER MODEL TR-220 AND (C) ANSDR DLM88080184Turbine · failedIN FLT RETURN RT ENG FAILURE DURING CLIMB-OUT NORMAL PWR T/O WITH ENG A/I ON. ALL INDICATIONS NORMAL. AT 1300' AGL BUMP NOISE LIKE A COMP STALL. PERFORM INITIAL ACTION ITEMS AND STARTED RETURN TO AIRPORT. PLANNED TO RUN ENG AT IDLE BUT APPROX 2-3 MIN ENG SSDR ASMF200802002Link · looseAC RETURNED TO DEPARTURE DURING TAKEOFF, NOISE AND VIBRATION IN THE NOSE LANDING GEAR WERE DETECTED AND CONTINUED WITH FLAPS AT 40 DEGREES. ABNORMAL PROCEDURE SECTION 5-10 WAS PERFORMED. AT PLATFORM, MAINT DETECTED THE NOSE LANDING GEAR DOOR OPEN AND UNLOCKESDR ASMF200801002Blades · damagedDURING OVERNIGHT CHECK, 10 FAN BLADES OF THE RT ENG WERE DETECTED WITH DENTS AND LOSS OF MATERIAL DUE TO AN FOD. MAINTENANCE PERFORMED A BOROSCOPIC INSP IAW MM 72-00-00 AND NO ADDITIONAL DAMAGES WERE FOUND; THE 10 DAMAGED BLADES WERE REPAIRED IAW MM 72-33-21,SDR AALA200800139Start Valve · failedSLC INFLIGHT T2036/23JAN - AT ROTATION RIGHT START VALVE OPEN LIGHT ILLUMINATED AND FIRE BELL SOUNDED FOR ABOUT 2 TO 3 SECONDS THEN EXTINGUISHED. THE RIGHT START VALVE OPEN LIGHT ALSO EXTINGUISHED. RETURNED TO SLC AND LANDED WITHOUT INCIDENT. INSPECTED ENGISDR DLM88080096Ballast · burned outFLIGHT ATTENDANT REPORTED SMELLING SMOKE IN THE MID CABIN. OVERHEAD LIGHT AT 20ABC FLICKERED THEN WENT OUT FOLLOWED BY ODOR. DISCOVERED BALLAST AT 20ABC HOT. PULLED AND COLLARED C/B FOR LT O/H LIGHTS. C/W OPN 5088. FWD LIGHT TO MCO/PLAC PER MEL 33-00-02. SDR DLM88080094Oil System · leakingSMOKE IN CABIN, FOUND APU OIL LEAKING INTO APU INLET. FOUND OIL LEAK AT ATTA POINTS FOR OIL FILL/SIGHT GLASS, SECURED BOLTS THAT WERE FOUND LOOSE AND REPLACED OIL CAP. LEAK CKS OK REF ITEM 004 NEXT LOG PAGE FOR DUCT BURN OUT OPERATION.SDR DLM88080095Fan Blade · bentDURING CLIMB-OUT, NR 1 ENG HAD TWO COMPRESSOR STALLS AND FLAMES AS REPORTED BY F/A AND PASSANGERS. REPLACED 1ST STAGE FAN BLADES PER TRANS 9T133.SDR ANCF200700034Wire · burnedDURING CRUISE STRONG BURNING ODOR IN COCKPIT DUE TO PREVIOUS REPORTS ON RT PACK THE PACK WAS TURNED OFF AND THE ODOR DISSIPATED. THE ODOR WAS IN COCKPIT. IAW WDM AND AMM 33-22-07/525 AND 20-50-01 /201 IN LT UPPER SIDE WALL LIGHTING TRANSFORMER LINE IL 1701F1SDR FX7A200700008Actuator · inoperativeAFTER TAKEOFF, AROUND 2,500 FEET, FLIGHT CREW WAS UNABLE TO TRIM AIRCRAFT WITH CAPTAIN, F/O SUITECASE OR ALTERNATE TRIM. AIRCRAFT WAS FLOWN WITH ELEVATORS ONLY. AROUND 250 KTS VIBRATION WAS FELT THROUGHTOUT THE AIRCRAFT. AFTER LANDING, TRIM SYSTEM OPERATED SDR AALA20072483Oil System · leakingFAT INFLIGHT T1846/20DEC SJC TO DFW - LEFT ENGINE INDICATIONS OIL QUANTITY ZERO AND OIL TEMPERATURE RISING. CREW SHUT DOWN ENGINE AS PRECAUTION. LANDED FAT WITHOUT INCIDENT. SINGLE ENGINE TIME 46 MINUTES WITH POSITIVE OIL PRESSURE. REPLACED NUMBER ONE ENGISDR FX7A200700007Circuit Breaker · trippedFORWARD CENTER TANK CIRCUIT BREAKER POPPED OUT DURING CLIMB.SDR DLM88071607Hydraulic Line · looseLEFT HYD PRESSURE SYSTEM FAIL IN FLT PRESSURE DROPPED TO ZERO AND QTY DROPPED TO 2 QTS. FOUND PRESSURE LINE AT NR 1 ENG DISCONNECT LEAKING. TIGHTENED LINE AND RAN ENG, THRUST REVERSER AND ELEC PUMPS. NO LKS FOUND.SDR DL76G071608Bottle · emptyLEFT OVERWING SLIDE BOTTLE FOUND EMPTY DURING ROUTINE CHECK BOTTLE REPLACED.SDR ANCF200700030Warning System · false activationDURING ROLL T/O FLAPS CONFIGURATION ALARM SOUNDS WITH THE FLAPS T/O SELECTOR IN TO POSITION AT 60 KTS. IAW AMM 27-53-01 PAG 201. FLAPS WARNING SWITCH CHECK AND TEST WERE EFECTUATED. FAULT NOT DUPLICATED.SDR DLM88071509Transformer · burnedSMOKE AND FUMES IN CABIN. FOUND VARIABLE TRANSFORMER FOR LOWER SIDE WALL PANEL BAD AT AFT F/A PANEL. REMOVED AND REPLACED ON ITEM 5 TRANSFORMER HAD STRONG BURNED ELECTRICAL ODOR PERFORMED ALT DUCT BURN ON ITEM 7.SDR DLM88071496Engine · stalledLT ENGINE COMPRESSOR STALL AT FLT LEVEL 290, NO POWER EPR WOULD NOT INCREASE. ALL OTHER INDICATIONS NORMAL. REPLACED NR 1 ENG.SDR ASMF200711002Engine · failedAIRCRAFT REJECTED TAKEOFF AT 130 KNOTS DUE TO RT ENGINE HAS LOSS OF POWER AND BRAKES REACHED 350 DEGREE C. DURING MAINTENANCE CHECK, T4 STAGE WAS DETECTED WITH LOSS OF MATERIAL, THEREFORE, RT ENGINE WAS REPLACED AND TESTED IAW MPSM 71-00-02 AND 71-00-01. HIGH SDR AALA20072196Tailpipe · debondedSTL INFLIGHT T531/13NOV - NUMBER ONE ENGINE HAD MULTIPLE COMPRESSOR STALLS DURING CLIMB. RETURNED TO STL AND LANDED WITHOUT INCIDENT. DISCOVERED DISBONDED LINING IN TAIL PIPE. REPLACED NUMBER ONE ENGINE ON 14 NOV 2007 AT STL. REPLACED LEFT ENGINE ISOLATORSSDR AALA20072188Compressor · stalledSAT INFLIGHT T1303/12NOV - NUMBER TWO ENGINE HAD COMPRESSOR STALLS ON INITIAL CLIMB-OUT PASSING 3500 FEET. CREW HEARD THREE OR FOUR BANGS. ENGINE WAS BROUGHT TO IDLE UNTIL LANDING. RETURNED TO SAT AND LANDED WITHOUT INCIDENT. FOUND INTERNAL DAMAGE TO 12 ANSDR 070176Engine · failedALLEGIANT AIR FLIGHT 722 FROM CID (CEDAR RAPIDS, IOWA) TO SFB (SANFORD, FLORIDA), FLIGHT CREW REPORTED THE NR 1 (LEFT) ENGINE FAILURE ON CLIMB-OUT. PERFORMED EMERGENCY QRH ITEMS AND RETURNED TO CID. AIRCRAFT LANDED NORMALLY, MAINTENANCE DEPARTMENT PERSONNELSDR DLM88071413Engine · shutdownAT FL320, THE LEFT ENGINE SHUT DOWN. THE N2/HYD PRESSURE/OIL PRESSURE WENT TO -0-. THE ENGINE WINDMILLED FOR 25 MINS WITH -0- OIL PRESSURE. REMOVED AND REPLACED NR 1 ENGINE PER TRAS 9T102.SDR ASMF200710012Brake · failedCAPTAIN REPORTED THAT DURING TAXING AT RUNWAY THRESHOLD, THE TEMPERATURE OF THE MAIN LANDING GEAR BRAKE NR 1 REACHED 450 CELSIUS DEGREES, SO IT WAS NECESSARY TO STOP THE AIRCRAFT. MAINTENANCE PERSONNEL REPLACED THE LT BRAKE ASSY AND THE MAIN LANDING GEAR WHEESDR ASMF20071008Seal · damagedAIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT HMO DUE TO CAPTAIN REPORTED THAT DURING NOSE LANDING GEAR RETRACTION, STRONG VIBRATION WAS FELT, BURNED RUBBER ODOR WAS DETECTED AND RED WARNING LIGHT TURNED ON ALL THE TIME. MAINTENANCE PERSONNEL VERIFIED THE NOSE SDR ASMF200710008Generator · damagedCAPTAIN REPORTED THAT DURING TAXING, LT GENERATOR WAS OUT OF SERVICE. MAINTENANCE PERSONNEL DEFERRED REPORT IAW MEL 24-1 CAT B. LATER DURING NEXT TRANSIT CHECK, LT GENERATOR WAS REPLACED IAW MM 24-20-01, TESTED CORRECT.SDR ANCF200700023Packing · brokenDURING APP AT BOG, R HYD QTY DROPPED TO 1 QT WITH THE SYSTEMS PRESSURIZED. THERE WAS NOT R HYD QTY ANNU ON THE EOAP. (THIS CAUSES EMERGENCY LANDING) SEVERE HYD LEAK FOUND AT FWD OUTLET LINE FITTING OF MOTOR OPERATED DUAL SHUTOFF VALVE. DURING INSPECTION FITTSDR AALA20071940Blades · damagedDFW INFLIGHT T1157/15OCT - RIGHT ENGINE PRESSURE RATIO FLUCTUATION AND VIBRATION ON TAKEOFF ROLL ENGINE COMPRESSORS STALLED. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NUMBER TWO ENGINE ON 16 OCT 2007 AT DFW DUE TO FAN FOD DAMAGE DURING TAKEOFF. SDR ASMF200710002Strut · leakingAIRCRAFT AIR TURNED BACK DUE NOSE LANDING GEAR DID NOT RETRACT AND THE CORRESPONDING RED LIGHT TURNED ON. DURING MAINTENANCE CHECK, THE NOSE LANDING GEAR STRUT WAS DETECTED COMPRESSED, SO IT WAS SERVICED IAW MM 32-21-02 AND THE NOSE LANDING GEAR PROXIMITY SENSSDR ASMF200709010Actuator · damagedCAPTAIN REPORTED THAT IT WAS NECESSARY TO ADJUST THE RUDDER TRIM COMPENSATOR 7 UNITS TO THE RIGHT IN FLIGHT. AT PLATFORM, MAINTENANCE PERSONNEL REPLACED THE RUDDER HYDRAULIC POWER PACKAGE AND THE YAW DAMPER ACTUATOR IAW MM 27-20-04 AND 22-13-01 RESPECTIVELY, SDR ANCF200700021Electrical Sys · multiple failDURING TAKEOFF ROLL, HAD AN ELECTRICAL FAILURE: TAKEOFF WAS ABBORTED AT 90 KNOTS. THE FLIGHT GUIDANCE STATUS AND MAINT PNL C/B G 25 WAS TRIPPED. THE AC BUSS PHASE B C/B WAS ALSO TRIPPED. ART WAS ACCURATED. IAW AMM 24-20-00/201 GCU`S WERE CHECKED AND RESET
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