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 YYFA20090002Sensor · dirtyDURING CLIMB , TAIL COMPARTMENT HIGH LIGHT ILLUMINATED.SDR DLM88091185Starter · damagedNR 2 ENG STARTER HOUSING CAME APART AND DAMAGED LOWER FWD COWL. A PIECE OF GEAR HIT THE COWL CAUSING A DENT ON THE INSIDE AND SOME FIBERS ON THE OUTSIDE TO SPLINTER OUT. GEAR DID NOT PASS THRU COWL. REPLACED NR 2 ENGINE STARTER, OPS CHECKS OK. REPLACED NR SDR WX0A070343Engine · fodFLIGHT CREW REPORTED ON TAKE OFF AT ROTATION THE AIRCRAFT EXPERIENCED A RYTHMIC PULSING AND A BANGING SOUND CONSISTENT WITH ENGINE COMPRESSOR STALL. TOWER REPORTED FLAMES FROM THE LEFT ENGINE. POST FLIGHT INSPECTION REVEALED NR 1 TIRE HAD TREAD MISSING. MAINATSDR ANCF2009061800050Controller · malfunctionedTHRUST SET FOR TAKEOFF, LT AND RT ENGINE EPR 2.08 LT ENG N1 98 PERCENT RT ENG N1 98.7 PERCENT, LT AND RT ENGINE EGT WITHIN LIMITS. ABOUT 100 KTS A STRONG DECELERATION WAS FELT, RT ENGINE EPR DROPPED TO 1.78, AFT CREW REPORTED A LOUD BANG FROM RT ENGINE. AMMSDR DALA1127840672Skin · damagedFUSELAGE SKIN BULKHEAD FS 1680-1780, STR 29L - 29R TAIL STRIKE DAMAGE REPAIRED IAW ERA 475331-14.SDR DALA1127850672Skin · damagedFUSELAGE SKIN FS 1720 TO 1743, STR 29R TAIL STRIKE DAMAGE REPAIRED IAW ERA 475339-14.SDR DALA1127820672Skin · damagedFUSELAGE SKIN AND BULKHEAD, FS 1682-1720, S-29L TO S-29R TAIL STRIKE DAMAGE. REPAIRED IAW ERA 475227-14.SDR AALA2009060400011Fuel Control · malfunctionedDFW - CREW REPORTED DURING DESCENT HAD NO THROTTLE CONTROL. EMERGENCY DECLARED, LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER ONE ENGINE FUEL CONTROL AND PUMP. SYSTEM GROUND CHECK NORMAL OPERATION.SDR DLM88090929Oil System · emptyRT ENGINE LOST ALL OIL QTY IN FLT. ON DESCENT AT IDLE POWER, ENGINE SHUTDOWN. REPLACED NR 2 ENG IAW TRANS 9T102.SDR AALA2009050400001Duct · leakingLEFT ENGINE FIRE WARNING. EMERGENCY DECLARED RETURNED LAS WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NR 1 ENGINE UPPER RT ANTI-ICE DUCT. SYSTEM GROUND CHECK NORMAL OPERATION.SDR WX0A070287Engine · failedFLIGHT CREW REPORT THE RIGHT ENGINE FAILED AND THE ENGINE WAS SHUTDOWN PER THE EMERGENCY PROCEDURES CHECKLIST. THE AIRCRAFT RETURNED TO LAS VEGAS WITHOUT INCIDENT. MAINTENANCE DEPARTMENT PERSONNEL REPLACED THE ENGINE IAW THE APPLICABLE AIRCRAFT MAINTENANCE MSDR 2009FA0000272Fuel Nozzle · damagedDURING DISASSEMBLY OF THE DIFFUSER MODULE IT WAS NOTICED THAT THE FUEL NOZZLES AT NR 1 AND NR 2 POSITIONS HAD SUSTAINED DAMAGE DUE TO THE AIR SCOOP WELD FAILING, THUS ALLOWING THE AIR SCOOP TO ROTATE AND CAUSE FRETTING EROSION TO THE HEAT SHIELD AND NOZZLE BODSDR 2ARF 20090301Generator · failedAIRCRAFT RETURNED DUE TO APU GENERATOR FAILED AT FL 270 AND LT GENERATOR WAS DEFERRED. MX PERFORMED APU GENERATOR RESET AND TESTED IAW 49-00-00 AND LT GENERATOR WAS REPLACED AND TESTED IAW AMM 24-20-02, ALL CORRECT.SDR YYFA20090001Unknown · unknownUNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF.SDR AALA2009031100001Engine · failedJFK - INFLIGHT LGA-ORD. AFTER TAKEOFF RIGHT ENGINE FAILED. CREW SHUTDOWN ENGINE AND THERE WAS NO FIRE OR HEAT WARNING. EMERGENCY DECLARED, LANDED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER TWO ENGINE ON MARCH 12, 2009 AT JFK DUE SDR AALA2009012800246Oil System · leakingAMA INFLIGHT SAN ORD - CREW REPORTED NUMBER ONE ENGINE OIL PRESSURE LOSS. CREW SHUT DOWN NUMBER ONE ENGINE. SINGLE ENGINE TIME 17 MINUTES. LANDED AMA WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE DUE TO OIL PRESSURE LOSS. SYSTEM GROUND CHECKED NORMAL OPERASDR DLM88090092Connector · shortedRT ENG "A" FIRE LOOP INTERMITTENT FAULT IN FLIGHT. FLT CREW MCO AND PLACARD APPLIED PER MEL 26-00-01A. SELECTED "B" LOOP PER MEL. DURING HI SPEED TURN OFF RECEIVED RT ENG FIRE WARNING. PULLED FIRE HANDLE AND SELECTED RT ENG "BOTH" FIRE LOOPS AND MSG EXTINGSDR AALA2009011500163Oil System · low pressureEUG INFLIGHT PDX TO DFW - ABOUT TEN MINUTES AFTER TAKEOFF AT 25000 FEET OIL STRAINERS CLOG LIGHT ILLUMINATED. PRESSURE WAS DROPPING SLOWLY THROUGH 35 PSI AND OIL TEMPERATURE WAS RISING SLOWLY. CREW SHUT DOWN NR 1 ENGINE. OIL QUANTITY NORMAL. ENGINE WINDMILSDR ANCF2009010500033Fuel Control · malfunctionedTHROUGH FLIGHT LEVEL 240 LET ENGINE EPR WAS 1.60 AND RT ENG WAS 2.70 WE SHUTDOWN THE LT ENG AND AFTER SHUTDOWN THE LT ENG AND AFTER SHUTDOWN THE PARAMETERS WERE OK FOR THAT CONDITION AFTER AIRSTART THE PARAMETERS IN IDLE WERE NORMAL AFTER ACCELERATE THE L ENGISDR DLM88090010Engine · power lossON CLIMB-OUT FLT LEVEL 175, NR 2 ENGINE SHUTTERED, FLT CREW FOLLOWED ENGINE FAILURE PROCEDURES AND SHUT NR 2 ENGINE DOWN.SDR YYFA20080004Amplifier · inoperativePA SYS INTERMITTENT.SDR ASMF 20081202Control Valve · leakingDURING TRANSIT CHECK, A HYD LEAK ON THE RT ENG WAS DETECTED. MX TIGHTENED HYDRAULIC LINE AND REPLACED AND TESTED THE RT ENG REVERSE CONTROL VALVE IAW AMM 78-31-04, ALL CORRECT.SDR DLM88081703Engine · leakingCREW REPORTS OILY SMELL/ODOR IN CABIN AFTER TAKEOFF. DISSIPATED. FOUND NR 1 ENG CREATING SMOKE AND ODOR WHILE PERFORMING OPN 5088. ENGINE CHANGE.SDR DLM88081653Line · looseON DEPARTURE WITH TAKEOFF POWER SELECTED CREW NOTICED SLIGHT ODOR IN COCKPIT SMELLED LIKE OVERHEATED DUCTS NOT ELECTRICAL, BRAKE OR TIRES. AFTER LANDING PASSENGERS TOLD F/A THAT THEY SAW HAZE AND ODOR IN AFT CABIN. AFTER TAKEOFF ODOR DISSIPATED AFTER 1 MINUTSDR DLM88081640Engine · smokeDURING CRUISE, FLIGHT ATTENDANT REPORTED SMOKE IN CABIN. BOTH AFT LAV SMOKE DETECTORS WERE GOING OFF. ENGINE ANTI-ICE ON, LT PACK TURNED OFF SMOKE OUT. CAPTAIN DECLARED EMERGENCY ON APPROACH. LANDED AT SCHEDULED DESTINATION. REPLACED NR 1 ENGINE.SDR ASMF 20081102Fan Blade · nickedDURING OVERNIGHT CHECK, FOUND A NICK OF 0.005 INCHES DEPTH ON THE LEADING EDGE OF ONE FAN BLADE AT .4375 INCHES FROM THE ROOT, AND A NICK OF 0.0035 INCHES OUT OF LIMITS ON THE LEADING EDGE OF THE OTHER FAN BLADE AT .7500 INCHES FROM THE ROOT. RT ENG WAS REPLACSDR DLM88081598Duct · damagedRT ENGINE FIRE LIGHT CAME ON DURING FLIGHT. FOUND BLOWN DUCT AT AFT SIDE OF COWL ANTI-ICE VALVE. REPLACED DUCT FROM 13TH STAGE SADDLE DUCT TO COWL ANTI-ICE VALVE.SDR AALA2009021201036Fuel Control · inoperativeABQ - INFLIGHT DFW-SJC - LEFT ENGINE LOST THROTTLE RESPONSE. CREW SHUT DOWN ENGINE. SINGLE ENGINE TIME 30 MINUTES. EMERGENCY DECLARED LANDED ABQ WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE FUEL CONTROL AND FUEL PUMP. SYSTEM GROUSDR DL757081641Cargo Track · corrodedCORROSION ON AFT CARGO TIE DOWN FITTING BS 1383 RBL 25 WL 147 AT DOOR CUTOUT, NO ALLOWABLE LIMITS. REMOVED AND REPLACED FITTING PER SRM 51-40-02.SDR DLM88081573Duct · damagedON CLIMB-OUT AT LEVEL OFF THE RT ENGINE THROTTLE WAS BOUND. UNUSUAL RESISTANCE TO MOVING TO IDLE. AFTER BRINGING THE ENGINE BACK TO IDLE THE THROTTLES OPERATED NORMALLY. FOUND THE NUMBER 2 ENG COWL ANTI-ICE DUCT BLOWN WHICH CAUSED DAMAGE TO THE UPPER ENGINESDR AALA200802463AEngine · low pressureINFLIGHT - ABOUT 160 MILES OUT OF DFW NUMBER TWO ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED ALONG WITH ZERO OIL PRESSURE READING. OIL TEMPERATURE AT 30C. CREW SHUT DOWN NR 2 ENGINE. LANDED DFW WITHOUT INCIDENT. REPLACED NR 2 ENGINE ON 4 NOV AT DFW DUE TO OISDR DLM88081662Mount · scratchedSCRATCHED INNER WALL ON FLANGE OF AFT MOUNT BOLTS FOR LT ENGINE. SCRATCHES REWORKED IAW EA 49-469467-14. WITHIN LIMITS AND NO CRACKS NOTED IAW EA 49-469467-14 REV ORIGINAL.SDR AALA200802396ACompressor · stalledORD INFLIGHT - CREW REPORTED SUSPECTED NUMBER ONE ENGINE COMPRESSOR STALL DURING CLIMB THROUGH 25000 FEET. FELT AND HEARD BANG N1 ENGINE PRESSURE RATIO RAPID FLUCTUATION. CREW BROUGHT ENGINE TO IDLE. FLIGHT ATTENDANTS REPORTED EXTREME VIBRATION ON LEFT SIDESDR DLM88081664Bolt · wornWEAR ON AFT CONE BOLT FLANGES (BOTH SIDES) ON RT ENGINE. WEAR REWORKED IAW EA 49-469467-14 REV ORIG. WITHIN LIMITS AND NO CRACKS NOTED IAW EA 49-469467-14 REV ORIGINAL.SDR DLM88081349Csd · making metalON CLIMB-OUT MULTIPLE GEN RELAY TRANSFERS FOLLOWED BY LEFT CSD OIL PRESSURE LOW MESSAGE QRH FOLLOWED LEFT CSD WOULD NOT DISCONNECT. RTN TO ATL. FOUND CSD FULL OF METAL, REMOVED AND REPLACED TRANSMISSION AND GENERATOR WET SPLINE SERVICED NEEDS LINE TO OIL COOSDR DALA1149659017Latch · defectiveENGINE UPPER COWL DOOR LATCH REPLACED IAW EA 09-056907-12, ME06.SDR DLM88081300Engine · malfunctionedRT OIL PRESSURE DROPPED TO 0 AND RT OIL PRESSURE LOW MSG ON EOAP. SECURED RT ENG IN ACCORDANCE WITH THE QRH. OPENED LOWER COWL DOOR, REMOVED MAG CHIP DETECTOR. CLEANED INTO PAPER TOWEL. RE-INSTALLED MAG DETEDCTOR. PAPER TOWEL WITH ME LOCATED IN MCO PLACARDSDR DL76G081301Iru · malfunctionedON TAXI OUT GOT AN EICAS MSG UNABLE RNP. THIS IS AN ADVISORY MESSAGE AND REQUIRES NO MTC ACTION BUT CREW RTB. T/S PER FIM NTF. REPLACED CTR IRU AS A PRECAUTION.SDR YYFA200800003Pa System · inoperativeAIRCRAFT RETURNED TO THE GATE DUE TO P/A SYSTEM INOPERATIVE.SDR AALA200802386Rotor · seizedORD INFLIGHT T779/20SEP. AT APPROX 2000 FEET NR 1 ENGINE LOST ALL POWER. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE ON 20 SEP AT ORD DUE TO ROTOR SEIZED. SYSTEM GROUND CHECKED NORMAL OPS.SDR DLM88081141Line · leakingLT ENG HYD FLUID DEPLETED IN FLT, LT ENG HYD PUMP PRESS LINE LEAK IN TAIL OF A/C. REPLACED ENG DRIVEN PUMP AND INSTALLED TEMP FLEX LINE PER M/M.SDR MAS2008F00063Engine · malfunctionedACFT REJECTED TAKE OFF 70 KNOT DUE TO RT ENGINE DID NOT ACCELERATE (EPR 1.14). MX PERSONNEL CHECKED THE RT ENGINE IAW MM 72-00-00 PAGE 501, ALL CORRECT. ADDITIONALLY, A HIGH ENERGY STOP INSPECTION WAS PERFORMED IAW MM 05-57-00, NO DAMAGES WERE FOUND. DURINGSDR MAS2008F00065Prbc · malfunctionedACFT REJECTED TAKE OFF AT 70 KNOTS DUE TO RT ENGINE DID NOT ACCELERATE. MX PERSONNEL REPLACED PRBC`S IAW MM 75-31-01 AND FCU IAW 73-20-01. ADDITIONALLY THE PS3 WAS VERIFIED AND CLEANED, THE BLEED VALVES WERE LUBRICATED IAW 75-31-05 AND TRIM BOTH ENGINES WAS SDR AALA200802022Turbine · failedJFK INFLIGHT T2393/04AUG. LGA TO ATL. NR TWO ENGINE SEIZED ON TAKE OFF ROTATION. ALL INDICATIONS WENT TO ZERO. LANDED JFK WITHOUT INCIDENT. SINGLE ENGINE TIME 13 MINUTES. REPLACED NR TWO ENGINE DUE TO TURBINE FAILURE ON 05AUG AT JFK. SYSTEM GROUND CHECKSDR MWE2008F00029Lanyard · detachedLANYARD TO AFT SLIDE PACK DETACHED. REINSTALLED LANYARD. (K)SDR AALA200801951Turbine · damagedDFW INFLIGHT T2457/24JUL. CREW REPORTED NR 1 ENGINE MADE LOUD BANG FOLLOWED BY ENGINE GAS TEMPERATURE HIGH. CREW SHUT DOWN NR 1 ENGINE AND RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND TURBINE DAMAGE. REPLACED NR 1 ENGINE ON 24 JUL AT DFW. SYSTEM GROSDR WX02008F00001Manifold · leakingFLIGHT CREW PERSONNEL REPORTED ON THE INITIAL CLIMBOUT OF FLIGHT 883-3 FROM PIE, THE FIRE DETECTOR HANDLE AND LOOP "A" ILLUMINATED ON THE LT ENGINE. THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE DEPARTMENT PERSONNEL PERFORMED A VISUAL INSPECSDR MWE2008F00002Outflow Valve · obstructedUNABLE TO CONTROL CABIN WITH NR 1 PRESSURE SYSTEM CABIN, SWITCHED OVER NR 2 PRESSURE SYSTEM FLOW LIGHT ON. FOUND INSTALLATION BAG WAS STUCK IN AFT PRESSURE RELIEF VALVE. REMOVED OBSTRUCTION. (K)SDR AALA200801692Anti-Ice Valve · malfunctionedDFW - INFLIGHT T1776/24JUN. CREW REPORTED NR ONE ENGINE START VALVE INDICATION AFTER TAKEOFF. CREW SHUT DOWN ENGINE. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME EIGHT MINUTES. FOUND OUTBOARD ANTI ICE VALVE NOT CLOSING COMPLETELY. REPLSDR 2008FA0000490Acoustic Liner · damagedAC RETURNED TO PLATFORM, DURING ENGINE ACCELERATION UP TO 1.4 EPR, STRONG NOISE IN THE RT ENG WAS HEARD. MAINT PERFORMED AN INSPECTION AND DETECTED ACOUSTIC LINER DELAMINATION OF THE DIFFUSER OUTER FAN DUCT, BUT WITHIN LIMITS TO OPERATE TEN HOURS IAW MM 72-00
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