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 DLM8K060612Bulb · faultyAT FL 210 OVER PVD HIGH OIL TEMP WAS INDICATED ON LT ENGINE AND ENGINE SHUTDOWN PROCEDURE WAS PERFORMED. INITIAL TEMP WAS 158 DEGREES C AND THEN SPIKED TO 199 DEGREES C AND REMAINED HIGH AFTER ENGINE SHUTDOWN. ALL OTHER ENGINE INDICATIONS WERE NORMAL. ENGINE WSDR DLM88060599Engine · malfunctionedLT ENGINE ROLLED BACK ON T/O ROLL. ABORTED T/O. AFTER STOPPING EGT WAS RISING THRU 560 DEG AND N1/N2 WAS ROLLING BACK. SHUT DOWN ENGINE. REPLACED NR 1 ENG PER TRANS 9T102.SDR ASMF200607009Fcu · failedAIRCRAFT RETURNED TO PLATFORM, RT GENERATOR AND APU FAILED. BCU WAS REPLACED BUT APU FAIL CONTINUED. AIRCRAFT WAS SENT TO THE HANGAR, FCU AND FUEL PUMP WERE REPLACED IAW MM 73-20-01 AND 73-12-01 AND TESTED IAW MM 71-00-00, ALL CORRECT.SDR ASMF200607007Fcu · failedAIRCRAFT RETURNED TO PLATFORM, LOW OIL PRESSURE AND HIGH TEMPERATURE ON RT ENGINE. FCU AND FUEL PUMP WERE REPLACED IAW MM 73-12-00 AND 73-12-02, TESTED CORRECT IAW MM 71-00-00.SDR DLM88060563Connector · shortedON DEPARTURE FROM ATL, CREW HAD RIGHT ENGINE FIRE WARNING SOUND. RIGHT ENGINE B FIRE LOOP WAS ALREADY ON MCO. CREW PULLED FIRE HANDLE AND DISCHARGED BOTH FIRE BOTTLES. FLIGHT RETURNED TO ATL AND LANDED WITHOUT FURTHER INCIDENT. ATL MTC FOUND THE CONNECTOR SDR ASMF200607006Blades · damagedDURING TRANSIT CHECK, 2 BLADES OF LT ENGINE WERE DETECTED DAMAGED BY FOD. DAMAGES WERE 1.8750 INCH FROM BLADE ROOT TO MID SPAN, ONE WITH 0.040 INCH DEPTH AND .5625 INCH LONG, AND THE OTHER ONE WITH 0.030 INCH DEPTH AND .5625 INCH LONG. AIRCRAFT WAS SENT TO THESDR AALA20060445Compressor · stalledRIGHT ENGINE HAD COMPRESSOR STALLS UPON TAKEOFF AT MAXIMUM POWER. STALLS CLEARED AT OR NEAR IDLE THRUST. REPLACED RIGHT ENGINE ON 07 JUL 2006. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR AALA20060426Blade · failedMCI - INFLIGHT STL TO SEA. CLIMBING THROUGH FLIGHT LEVEL 280 HEARD LOUD BANG FROM RIGHT HAND ENGINE ACCOMPANIED BY THRUST LOSS. RIGHT HAND ENGINE N1 LESS THAN LEFT HAND ENGINE N1. RIGHT HAND ENGINE SHUT DOWN AND LANDED MCI OVERWEIGHT WITHOUT INCIDENT. RIGHSDR ASMF200606015Cowling · damagedDURING TRANSIT CHECK, A LOSE OF MATERIAL IN THE LT ENGINE NOISE SUPPRESSOR WAS DETECTED. AN INSPECTION WAS PERFORMED AND DAMAGE WAS OUT OF LIMITS, THEREFORE, THE AIRCRAFT WAS SENT TO THE HANGAR AND THE LT ENGINE NOSE COWLING WAS REPLACED IAW MM 71-10-01, TESTESDR DLM88060522Shaft · shearedAT 18,000 FEET THE NUMBER 1 ENGINE EXPERIENCED AN UNCOMMANDED SHUTDOWN. REMOVED FUEL CONTROL AND FUEL PUMP. FOUND SHAFT SHEARED ON PUMP. REPLACED PUMP PER AMM AND REINSTALLED FUEL CONTROL. CHECK ENG RUN OK PER AMM.SDR DL76G060523Isolation Valve · malfunctionedLEFT ISOLATION VALVE STUCK IN DISAGREE. VALVE CYCLED MANUALLY AND DEFECT CLEARED. REMOVED AND REPLACED VALVE PER M/M, OPS CHECK GOOD .SDR DLM88070734Apu · contaminatedAFTER T/O, ALL LAV SMOKE DETECTORS SOUNDED WITH SMOKE AND HAZE REPORTED IN CABIN BY FLIGHT ATTENDANTS. EMERGENCY RETURN TO ATL. FOUND APU INLET CONTAMINATED WITH OIL. OIL LEVEL IN SIGHT GAUGE WAS AT RE-FILL LINE. OIL TANK CAP IS INSTALLED AND SECURE. MX SSDR DLM88060495Engine · activatedRT ENGINE SLOW TO ACCELERATE. PERFORMED ENGINE ACCELERATION CHECK PER M/M. BOTH ENGINE ACCELERATE WELL WITHIN LIMITS. ENGINE PARAMETERS GOOD.SDR DLM88060476Engine · making metalCLIMBING THROUGH 8000K HEARD A LOUD BANG ACCOMPANIED BY VIBRATIONS. LEFT ENGINE RPM ROLLED BACK AND EGT RISING. ACCOMPLISHED CHECKLIST AND SHUT DOWN ENGINE. NO FIRE WARNING RIGHT INSP INLET AND EXHAUST, NO DAMAGE NOTED. REPLACED MAIN OIL FILTER 1386688. ISDR DL757060477Power Supply · burnedAFTER LEVEL OFF THE F/A CALL LIGHT AT 30A BEGAN SMOKING. CABIN LIGHTS WERE SECURED AND A DEADHEADING CREW MEMBER OPENED THE PANEL AND DISCONNECTED THE SHORTING LEADS FROM THE LIGHT. FOUND CTR READING LIGHT PWR SUPPLY MODULE BURNT. REPLACED OVHD PSU, CHECKS SDR AALA20060370Valve · stuckPVR - INFLIGHT, LEFT ENGINE OIL TEMPERATURE 175 DEGREES WITH FUEL HEAT ON. RETURNED TO PVR AND LANDED WITHOUT INCIDENT. FOUND FUEL HEAT VALVE STUCK OPEN. ACCOMPLISHED ENGINEERING PRE FERRY BILL OF WORK. REPLACED LEFT ENGINE AT DFW. SYSTEM GROUND CHECKED NSDR ASMF200605016Igniter Box · failedAIRCRAFT RETURNED TO PLATFORM DUE TO CAPTAIN REPORTED THAT DURING TAXIING AND AFTER TWO RIGHT ENGINE STARTING ATTEMPTS, EGT'S DID NOT INCREASE, PERCEIVING STRONG FUEL ODOR. AT PLATFORM, IGNITER BOX WAS REPLACED IAW MM 74-10-01, TESTED CORRECT IAW MM 74-00-00.SDR AALA20060333Line · leakingDFW - RIGHT ENGINE SHUT DOWN DUE TO LOSS OF OIL QUANTITY. ENGINE OIL QUANTITY WAS ZERO BUT PRESSURE INDICATION WAS STILL 36 PSI BUT DROPPING WHEN SHUTDOWN. OIL TEMPERATURE WAS ABOVE 100 DEGREES CELSIUS. ENGINE WINDMILLED FOR APPROXIMATELY 22 MINUTES WITH 12SDR ASMF200605011Engine · malfunctionedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING LEFT ENGINE START THE TEMPERATURE REACHED 510 DEGREES CELSIUS. DURING MAINTENANCE REVISION, FUEL WAS IN ENGINE CHAMBER NR 1. OVER TEMPERATURE INSPECTION WAS PERFORMED IAW MM 72-00-00, AND ENGINE STARTESDR ASMF200605005Engine · leakingDURING OVERNIGHT CHECK, A OIL LEAK WAS DETECTED ON LEFT ENGINE. DEOILER SEAL WAS REPLACED AND LEAK CONTINUED. AIR CODITIONING AND PRESSURIZATION TEST WERE PERFORMED AND OIL ODOR WAS DETECTED IN PASSENGERS CABIN AND RIGHT LAVATORY SMOKE ALARM WAS ACTIVATED. SDR DLM88060388Engine · seizedLT ENG OIL PRESS BEGAN FLASHING ON TAKEOFF OIL PRESS REACHED 58 PSI. THE OIL PRESS DROPPED BELOW 55 PSI AT APPROX 5000FT. INDICATIONS NORMAL AFTER THAT. REPLACED OIL PRESSURE TRANSMITTER, NO HELP ADJUSTED PRESSURE REGULATOR TO LOW END AT IDLE. AT T/O POSDR FX7A200600004Bleed Valve · failedON TAKEOFF ROLL WITH TAKEOFF THRUST LEFT ENGINE EGT TEMP RAPIDLY INCREASING TO 600 DEGREES WITH 1.45 EPR MASTER CAUTION ILLUMINATED. MTX REMOVED AND REPLACED THE LT ENGINE PRBC VALVE, OP CHECKED NORMAL IAW MM REF 71-00-00.SDR DL738060358Warning Light · illuminated20 MINS OUT FROM CVG, MASTER CAUTION AND FLT CONT LIGHTS CAME ON. FLT CONT B LOW PRESS LIGHT AND BOTH HYD PUMP B LOW PRESS LIGHTS ILLUM. B SYS INDICATED 88 PERCENT QTY. SERVICED B SYS HYD. CYCLED FLAPS, SPOILER, CONT SURFACES. NO HYD LEAKS NOTED. RAN ESDR DLM88060357Line · leakingLEFT HYDRAULIC SYSTEM QTY AT 4 WITH LIGHT ON SECURED. LEFT HYDRAULIC SYSTEM QTY WENT TO 9 CONTINUED TO ATL. REPLACED LEFT HYDRAULIC AFT FILTER PRESSURE MODULE PIPE ASSEMBLY AND ADJACENT BRAIDED HOSE. SERVICE LEFT HYDRAULIC SYSTEM PER M/M. RAN LEFT ENGINE, SDR DLM88060345Engine · malfunctionedCREW REPORTED THE LEFT ENGINE OIL TEMP STARTED FLUCTUATING. TEMP WENT ABOVE 135 DEG AND THEN BACK TO NORMAL. TEMP THEN ROSE TO 165 AND CREW SHUT DOWN ENGINE PER QRH. NONE NOTED. MILLION AIR MTC AP 2664148, REPLACED LT ENG OIL TEMP BULB RAN ENG PER MM. CKSDR ANCF200600017Fuel Control · out of trimDURING T/O, A DIFFERENCE BETWEEN LT AND RT OF EPR 0.5 PERCENT. DURING FLIGHT AT FL 320 MACH 076 LT EPR 1.98 AND RT EPR 1.82. THEN USING ENG ANTI ICE AUTO THROTTLE DISCONNECT AND LT EPR 1.28 & RT EPR 1.72. WITH THIS PROBLEM IS UNABLE TO FLY IN IT CONDITIONS ISDR DLM8K060325Oil Cap · leakingATB CREW REPORTED SMOKE IN CABIN T/S SYS-REPLACED APU OIL CAP-FOUND HOLD DOWN SPRING WEAK. INSPECTED OIL SYS-TIGHTENED LOOSE B-NUT. PERFORMED OPN 508 DUCT BURNOUT. ALL OPS NML AND OPN 5088 CABIN SMOKE/ODOR T/S-ALL OPS NML.SDR FX7A200600003Unknown · malfunctionedAFTER TAKE OFF THE PRESSURIZATION WAS ABNORMAL, RETURNED TO VLN, DUE TO THE PROBLEM LOG PAGE : 39529 MAINTENANCE PERFORMED AN AIRCRAFT AND CABIN PRESSURIZATION CHECK IAW AMM 21-32-00 FOUND NO DEFECTS, SYSTEM OP CHECKED OKAY.SDR ASMF200604007Transmitter · failedAIRCRAFT ABORTED TAKEOFF AND RETURNED TO PLATFORM AS A CONSEQUENCE OF THE LEFT ENGINE DID NOT ACCELERATE WITH EPR'S ON 1.4 AND EGT'S LIGHT BLINKING. WATER TRAMP WAS DRAINED AND ACCELERATION CHAMBER WAS LUBRICATED IAW MM 73-20-03 AND 73-20-01. DURING ENGINES SDR AALA20060232Engine · malfunctionedDFW INFLIGHT DURING CLIMB AT 4000 FEET AIRCRAFT ENCOUNTERED A COMPRESSOR STALL FROM NUMBER 2 ENGINE. SUBSEQUENT POWER APPLICATIONS CAUSED REPEATED SURGES. SHUT RIGHT HAND ENGINE DOWN AND PULLED FIRE HANDLE AS PRECAUTION. RETURNED TO DFW AND LANDED WITHOUT ISDR AMF200604005Indication Sys · malfunctionedAIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF DURING CLIMB RIGHT OIL TEMPERATURE INDICATOR SHOWED 135 GRADES AND INCREASED UP TO 145 IN 5 SECONDS, SO THRUST WAS REDUCED IN ORDER TO PREVENT HIGHER OIL TEMPERATURE. AT PLATFORM, RIGHT ENGINE TEMPERATURE SENSORSDR DLM88060269Starter · looseWHEN ATTEMPT START ON RIGHT ENGINE GOT START VALVE LIGHT OPEN BUT NO ROTATION. UPON INVESTIGATION FOUND THE NR 2 STARTER NOT CONTAINED AND THE REAR COMPRESSOR DUCT DAMAGED. REPLACED STARTER. PUNCTURE IN ENG HONEY COMB JUST ABOVE START REPAIRED ENG S/N726824SDR MWEA060018Engine · frozenRIGHT ENGINE PRESSURE RATIO DID NOT ADVANCE PAST 1.02, ALL OTHER INDICATIONS NORMAL. DISCONNECTED PT7 LINES AT CROSSBRIDAL AND DETERMINTED THAT THE LINES WERE OBSTRUCTED WITH ICE BETWEEN BRIDAL AND PT7 TRAP, RAN ENGINES, OPERATIONS CHECKED GOOD.SDR AALA20060137Drain Valve · inoperativeORD - AFTER TAKEOFF LEFT ENGINE COMPRESSOR STALLED AT APPROXIMATELY 2000 FEET ABOVE GROUND LEVEL AT CLIMB POWER. ENGINE POWER REDUCED AND STALL CLEARED. NO OTHER INDICATIONS. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED LEFT HAND ENGINE FIRST STAGSDR ANCF200600010Oil System · lowPILOT REPORT DURING CLIMB, CROSSING FL 313, THE -LEFT OIL PRESS LOW- ANNUNCIATION CAME ON EOAP ALONG WITH A DROP OF OIL PRESS TO 32 PSI. TIME 1545Z. ENGINE WAS REDUCED AND CHECK LIST WAS ACCOMPLISHED. LEFT ENGINE WAS SHUTDOWN AT 1548Z (3 MINUTES LATER). INSDR AALA20060073Blade · failedSEA INFLIGHT T875/01FEB, AFTER TAKEOFF AT 6000 MEAN SEA LEVEL HEARD A BAND AND INDICATIONS FOR LEFT ENGINE ROLLED BACK TO ZERO. ENGINE SHUTDOWN WAS COMPLETED AND RETURNED TO SEA AND LANDED WITHOUT INCIDENT. THERE WERE NO FIRE INDICATIONS AND NO BOTTLES USED.SDR ANCF200600008Unknown · unknownDURING ROLLING TAKEOFF AUTOSPOILER ALARM CAME ON TAKE OFF WAS DISCONTINUED AT 80 KTS AND RETURN TO GATE. NOTE: AUTOBRAKE WAS ARM TO, THE AURAL ALARM CAME ON WITH NO ANNUN ON THE EOAP. IAW AMM 05-57-00 PAG 601 HIGH ENERGY STOP/MAIN LANDING GEAR WHEELS TIRES ASDR ASMF200601015Pitot Tube · lightning strikeCAPTAIN REPORTED THAT DURING DESCENT THE AIRCRAFT RECEIVED A LIGHTING STRIKE IN THE RADOME ZONE. AIRCRAFT WAS SENT TO HANGAR TO ACCOMPLISH AN INSPECTION BY LIGHTNING STRIKE IAW M/M 05-53-00; THE CENTER PITOT TUBE WAS FOUND WITH DAMAGES. THE PITOT TUBE WAS REPLSDR ASMF200601014Engine · failedAIRCRAFT RETURNED TO PLATFORM, DURING TAXING CAPTAIN INFORMED THAT THE RT ENGINE DID NOT START, THERE WAS NO ROTATION OF N2. THE START VALVE WAS OPENED MANUALLY BUT THE STARTING WAS NOT POSSIBLE. THE STARTER WAS REPLACED BUT THE CONDITION CONTINUED. METALLIC DSDR AALA20060060Turbine Blades · failedAUS INFLIGHT T1135/21JAN - AFTER TAKEOFF AT 4000 FEET HEARD A LOUD BANG. RIGHT ENGINE FAILED. RETURNED TO AUS AND LANDED WITHOUT INCIDENT. FOUND TURBINE BLADE FAILURE. REPLACED RIGHT HAND ENGINE PER MCM 71 91 99. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR AALA20060068Pump · inoperativeDFW INFLIGHT T1760/10JAN - ON CLIMB-OUT, RIGHT HAND ENGINE STOPPED RESPONDING TO THROTTLE MOVEMENT. EXHAUST GAS TEMPERATURE AT CLIMB LIMIT AND ENGINE ENGINE PRESSURE RATIO AT 1.3. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED FUEL PUMP AND FUEL CONSDR ASMF200601009Static Port · damagedDURING PRE-FLIGHT INSPECTION CAPTAIN REPORTED THAT THE RT STATIC PORT PLATE WAS FOUND DEFORMED. THE DAMAGE WAS DETECTED OUT OF LIMITS IAW M/M 34-11. THE RT STATIC PORT PLATE WAS REPLACED IAW M/M 34-11-01 AND THE SYSTEM WAS TESTED IAW M/M 34-11-00, ALL CORRECT.SDR ASMF200601010Starter · failedDURING TAXING CAPTAIN INFORMED THAT THERE WAS NOT INDICATION OF THE LEFT ENGINE, RETURNING TO PLATFORM. DURING MAINTENANCE REVIEW, THE ENGINE STARTER AND ITS COUPLE WERE FOUND DAMAGED. BOTH ITEMS WERE REPLACED AND SYSTEM TESTED IAW M/M 80-10-01. DURING OVERSDR ASAA0680002Longeron · corrodedC-CHECK, LONGERON CORRODED. REPLACED DAMAGED SECTION WITH SPLICES. (K)SDR ASAA0680004Floor Panel · puncturedC-CHECK, CABIN FLOOR PANEL PUNCTURED. REPLACED FLOOR PANEL. (K)SDR ASAA0680005Floor Panel · gougedC-CHECK, CABIN FLOOR PANEL GOUGED. REPLACED FLOOR PANEL. (K)SDR ASAA0680006Floor Panel · delaminatedC-CHECK, CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (K)SDR ASAA0680007Floor Panel · delaminatedC-CHECK, CABIN FLOOR PANEL DELAMINATED AT FASTENER LOCATIONS. REPLACED FLOOR PANEL. (K)SDR ASAA0680008Floor Panel · delaminatedC-CHECK, CABIN FLOOR PANEL DELAMINATED. REMOVED DAMAGED AREA. APPLIED GLASS CLOTH REPAIR. (K)SDR ASAA0680009Floor Panel · delaminatedC-CHECK, CABIN FLOOR PANEL DELAMINATED. REMOVED DAMAGED AREA. APPLIED GLASS CLOTH REPAIR. (K)
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