Pratt & Whitney JT8D-17
Service difficulty reports · 1,680
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 = 'JT8D17' 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 = 'JT8D17' 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 20000424AP011Fire Detector · malfunctionedCUN - FLT TA410 - ENGINE NR 2 OVERHEAT LIGHT CAME ON, THEN FIRE WARNING LIGHT CAME ON, THE QRH PROCEDURES WERE ACCOMPLISHED BY THE CREW, DUE THIS SITUATION THE AIRCRAFT LANDED AT CANCUN. CANCUN MX TECHS PERFORMED A COMPLETE VISUAL INSPECTION AT ENGINE NR 2, NSDR 9900979857Engine · failedDURING CRUISE AT 33,000 FEET, THE RIGHT ENGINE EXPERIENCED A FLAME-OUT. AIRCRAFT DIVERTED TO ATL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE DUE TO CONTAINED FAILURE.SDR CA990330013Bulkhead · cracked(CAN) WHILE INCORPORATING SB 737-53A1173 PRESSURE BULKHEAD REPLACEMENT, THE WEB WAS IDENTIFIED AS CRACKED DURING DISASSEMBLY .11 CM LONG Y SHAPED CRACK. WEB REPLACED.SDR 99UAL900161Structure · damagedDAMAGE CAUSED BY BAGGAGE TRACTOR ON RIGHT SIDE OF AIRCRAFT, JUST FORWARD OF NR 2 SERVICE DOOR ENCOMPASSING A 42 INCH AREA WITH APPROXIMATELY AN 18 INCH HOLE ACROSS ONE STRINGER. *S/D* SHEAR TIE REPAIRED AT STA 344 BETWEEN STR 19R AND 20R PER SRM 53-10-4, FIGURSDR CA990330008Tire · failed(CAN) NR 4 TIRE TREAD SEPARATED AND FRAGMENTS DAMAGED. THE RIGHT INBOARD FLAP, REPLACED.SDR 99UAL900134Apu · malfunctionedAPU FIRE WARNING. *S/D* INSPECTED APU, FOUND NO EVIDENCE OF FIRE. CHECKED LOOPS, CONNECTORS AND OHMED OUT. FOUND NO SHORTS OR OPENS. FOUND OIL ON CONNECTOR AND CLEANED. REPLACED FIRE DETECTION UNIT AS A PRECAUTION. REPLACED FIRE BOTTLE AND SQUIB. RAN APUSDR CA990330012Bulkhead · cracked(CAN) WHILE INCORPORATING SB 737-53A1173 PRESSURE BULKHEAD REPLACEMENT STA 178, VERTICAL WEB STA 178 RBL 5.7 IDENTIFIED AS CRACKED 2 CM LONG FROM EDGE OF WEB THROUGH ADJACENT FASTENER HOLE AND THREE CRACKS THROUGH 3 ADJACENT FASTENER HOLES. REPAIRED.SDR HALA9900055Compressor · stalledFLT 282 - HNL - LOUD BAND WHILE SPOOLING ENGINES. ENGINE COMPRESSOR STALLED. REMOVED AND REPLACED NR 1 ENGINE. (M)SDR CA990308017Actuator · leaking(CAN) LEFT MAIN GEAR ACTUATOR LEAKING, REPLACED.SDR CA990303011Actuator · jammed(CAN) AFTER LANDING, NR 7 RIGHT SPOILER STAYED UP. ACTUATOR REPLACED.SDR 99ZZZM268Turbine · failedMDW - ABORTED TAKEOFF, TAXIED BACK TO GATE. THE NR 2 ENGINE FAILED AND SOME DEBRIS WERE NOTED ON THE RUNWAY. THE NR 3 AND NR 4 TURBINE BLADES FAILED FOR UNKNOWN REASON. ENGINE WAS REPLACED AND TESTED OK. AIRCRAFT RETURNED TO SERVICE. CONTAINED DAMAGE, LIMSDR DHL9974020CTailpipe · damagedAT C CHECK, NR 2 ENGINE, HOLE ON LEADING EDGE TAIL PIPE EXTERIOR LT SIDE ABOUT 7 O'CLOCK POSITION. CUT OUT DAMAGED AREA, INSTALLED DOUBLER, 12 BY 4 PER SRM 51-40-3, N/R 6399.SDR 99UAL900069Valve · failedLOST A SYSTEM HYDRAULIC QUANTITY AND PRESSURE AFTER GEAR EXTENSION AND DURING FLAP OPERATION. *S/D* FOUND THE FLAP FLOW LIMITING VALVE LEAKING. THIS UNIT WAS LEAKING BECAUSE THE BODY SEPARATED INTERNALLY. THE UNIT CONTAINS A FLOW RING WHICH FAILED DUE TO FATIGSDR 99UAL900065Tr Unit · malfunctionedWEATHER RADAR DISPLAY WAS INCONSISTENT. *S/D* WEAK MESSAGE DURING SYSTEM TEST. REPLACED TRANSCEIVER TO CORRECT FOR 80 MILE RANGE. ALL GREEN RETURNS, OPS CHECK OK.SDR 99UAL900055Valve · failedNR 1 ENGINE ANTI-ICE VALVE CIRCUIT BREAKER WILL NOT STAY IN. *S/D* REPLACED NR 1 ENGINE ANTI-ICE VALVE, OPERATIONAL CHECK IS OK.SDR CA990310057Frame · corroded(CAN) DURING INSPECTION OF FUSELAGE DENT, THE FORWARD LEFT LAVATORY WAS REMOVED FOR ACCESS. THE CHORD AT STA 245 AND STA 260 FOUND CORRODED, REPLACED.SDR 99UAL900044Fire Detector · malfunctionedAPU FIRE WARNING INDICATION. *S/D* FOUND APU FIRE DETECTOR ITEM M334 DEFECTIVE. REPLACED DETECTOR, BOTTLE AND DISCHARGE DISC.SDR 99UAL900035Brakes · malfunctionedEXCESSIVE BRAKE DECAY. *S/D* ACCOMPLISHED PARKING BRAKE SYSTEM TEST PER APPLICABLE MAINTENANCE MANUAL. OPERATIONAL CHECK OF SYSTEM CHECKED OK. NO FAULTS FOUND.SDR CA990310050Actuator · failed(CAN) ON INSTALLATION, FOUND ACTUATOR RAN IN OPPOSITE DIRECTION AS REQUESTED. REPLACED AND VENDOR ADVISED.SDR 99UAL900028Valve · failedRIGHT MIX VALVE STUCK IN FULL COLD POSITION IN MANUAL AND AUTO SELECTIONS. *S/D* RIGHT HAND MIX VALVE FAILED IN THE FULL COLD POSITION. REPLACED THE RIGHT HAND MIX VALVE ASSEMBLY, CHECKS GOOD.SDR CA990310049Windshield · cracked(CAN) FIRST OFFICER'S WINDSHIELD CRACKED, REPLACED.SDR CA990310047Regulator · failed(CAN) AIR TURN BACK DUE TO LOSS OF A-SYSTEM HYDRAULIC PRESSURE. REPLACED AIR PRESSURE REGULATING VALVE ON HYRAULIC RESERVOIR.SDR HALA9900004Fcu · malfunctionedHNL - FLT 102 - POWER SURGE RIGHT ENGINE AT MID RANGE EPR SETTINGS, CLIMB POWER. EPR VARIED PLUS/MINUS .05. N1 PLUS/MINUS 2 PERCENT. NOT EVIDENT AT TAKEOFF POWER OR AT IDLE, A/C RETURNED TO HNL WHERE AN UNEVENTFUL LANDING WAS MADE. (M)SDR CA990111027Controller · failed(CAN) ON DESCENT, PRESSURIZATION MODE SET TO LAND AT 3,550 FEET. CABIN DESCENDED TO SEA LEVEL. PRESSURIZATION REINSTATED USING STANDBY MODE. CABIN PRESSURE CONTROLLER REPLACED.SDR CA990310042Module · failed(CAN) LOSS OF A-SYSTEM HYDRAULIC PRESSURE ON PUSH BACK, RETURN TO BLOCKS. REPLACED A-SYSTEM MODULE.SDR 98UAL900596Air Dist · odorOIL SMELL COMING FROM BOTH PACKS. CHECKED BOTH LEFT AND RIGHT PACK COALESCER BAGS, WATER SEPARATOR, AND PACK DUCTS FOR OIL RESIDUE OR CONTAMINATION. OPERATIONALLY CHECKED AND FOUND NO ODORS OR SIGNS OF OIL/FLUID RESIDUE.SDR 98UAL900587Oil Line · crackedNUMBER TWO ENGINE HAD LOW OIL PRESSURE. *S/D* THE NR 6 BEARING OUTER INTERNAL OIL PRESSURE LINE HAD CRACKED AT THE BRAZE JOINT NEAR THE 'B' NUT CONNECTION, CAUSING THE OIL LOSS. THE LINE WAS REPLACED AND THE ENGINE WAS BASE CHECKED, RUN IN THE TEST CELL, ANSDR CA981230024Switch · failed(CAN) NOSE GEAR UNSAFE LIGHT ILLUMINATED IN-FLIGHT WITH GEAR HANDLE UP, NLG LOCK AND POSITION SWITCHES REPLACED.SDR CA981214013Line · punctured(CAN) 2ND OFFICERS DILUTER DEMAND SUPPLY HOSE HAS A SMALL HOLE. REPLACED.SDR CA981214012Regulator · leaking(CAN) 1ST OBSERVERS DILUTER DEMAND REGULATOR EMERGENCY SUPPLY NOT FULLY CLOSING. REPLACED.SDR CA981214010Indicator · malfunctioned(CAN) FLAPS WENT TO 2 DEGREES, THEN LOCKED OUT, INBOARD FLAP POSITION INDICATOR REPLACED.SDR CA981125024Sensor · malfunctioned(CAN) AT TOP OF DESCENT, RT RED GEAR WARNING LIGHT FLICKERED WITH GEAR SELECTED UP. REPLACED RT MLG UPLOCK SENSOR.SDR CA981214011Compensator · leaking(CAN) OXYGEN LEAK AT CONNECTIONS TO CREW OXYGEN SHUTOFF VALVE AND AT CONNECTORS TO THERMAL COMPENSATOR AND REGULATOR. VALVE REPLACED.SDR CA981214009Switch · misrigged(CAN) IN CRUISE, BOTH RED CARGO DOOR LIGHTS AND MAIN CARGO DOOR NOT CLOSED, AMBER LIGHTS ON IN DESCENT AT 7.0 DIFF, ALL LIGHTS OUT. DOOR TESTED PER A.E.I. M/M SERVICEABLE. ADJUSTED CARGO DOOR CLOSED MICROSWITCH. PART TC: 162.SDR CA981116008Clamp · loose(CAN) AIRCRAFT RETURNED FROM TAXI-OUT DUE NR 1 STRUT OVERHEAT INDICATION. FOUND LEAK AT 13TH STAGE MODULATING VALVE DOWN STREAM CLAMP. CLAMP SECURED.SDR MZZA98210Engine · failedTKK - FLT 957 - NR 3 ENGINE WITH HEAVY VIBRATION. MAINTENANCE FOUND TURBINE BLADES MISSING IN EXHAUST SECTION. MAINTENANCE REMOVED AND REPLACED NR 3 ENGINE PER WORKCARD 07-7100-1-8001. OPS AND LEAK CHECK COMPLIED WITH, NO LEAKS NOTED. POWER ASSURANCE RUN CSDR CA981027020Valve · leaking(CAN) NR 1 STRUT OVERHEAT LIGHT WARNING CAME ON WHILE CLIMBING THROUGH 8,000 FEET ON TAKEOFF. POWER WAS REDUCED, LIGHT EXTINGUISHED AND AIRCRAFT RETURNED TO ITS POINT OF DEPARTURE. POST-FLIGHT INSPECTION FOUND THE 8TH STAGE CHECK VALVE, ON NR 1 ENGINE LEANINSDR CA981027019Switch · corroded(CAN) CREW REPORTED RUDDER SYSTEM A LOW PRESSURE LIGHT CAME ON. CANNON PLUG ON RUDDER A SYSTEM LOW PRESSURE SWITCH WAS FULL OF RUST. SWITCH AND CANNON CONNECTOR CLEANED AND RESECURED. SYSTEM SERVICEABLE.SDR CA981125015Regulator · failed(CAN) LOSS OF A-SYSTEM HYDRAULIC PRESSURE NOTED. SUSPECT PRESSURE REGULATING VALVE FOR RESERVOIR HEAD PRESSURE. REPLACED VALVE.SDR CA981116007Bolt · misinstalled(CAN) WHILE REPLACING CLAMPS ON RIGHT MLG, TECH NOTICED DRAIN HOLE ON FORWARD TRUNNION FAIRING BLOCKED. INVESTIGATION FOUND RIGHT MLG TRUNNION LINK FUSE BOLT LOCKING SLEEVE, SEAL RING AND GREASE RESERVOIR ADRIFT IN BOTTOM OF FAIRING. LEFT MLG FOUND FUSE BOLTSDR CA981006024Indicator · failed(CAN) INBOARD FLAPS LOCKED OUT AT 15 DEGREES AFTER TAKEOFF. DUMPED FUEL AND LANDED USING ALTERNATE FLAP EXTENSION. REPLACED FLAP INDICATOR.SDR CA981006025Indicator · failed(CAN) INBOARD FLAPS LOCKED OUT AT 5 DEGREES AFTER TAKEOFF. AIRCRAFT RETURNED TO BLOCKS. INDICATION ADJUSTED AND FLAP INDICATOR REPLACED.SDR CA981013010Clamp · leaking(CAN) NR 2 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED IN-FLIGHT. POST-FLIGHT INSPECTION FOUND NR 2 ENGINE RIGHT HAND PRECOOLER CLAMPS LEAKING. ALSO NR 3 ENGINE LEFT HAND 13TH STAGE CROSSOVER DUCT MANIFOLD GASKET LEAKING.SDR 98FDEA00581Turbine · failedAT ROTATION, HEARD LOUD POP FROM RT SIDE OF A/C. ENG NR 3 HAD ROLL BACK TO EPR, OF 1.80, N1=80 PERCENT, EGT=500 DEG CELSIUS, N2=80 PERCENT, FUEL FLOW=5,000 LBS. ENG NR 1 AND NR 2 IND NORM PWR, CONT T/O AND CLIMBOUT. ACCOMPLISHED ENG FAIL/SEVERE DAMAGE CKLISSDR CA980922018Engine · failed(CAN) EXTREME ENGINE AND AIRFRAME VIBRATION WAS FELT ON CLIMB-OUT AFTER TAKEOFF. NR 2 ENGINE FAIL LIGHT ILLUMINATED. ALL ENGINE PARAMETERS DECAYED TO IDLE. PRECAUTIONARY ENGINE SHUTDOWN WAS CARRIED OUT AND THE AIRCRAFT RETURNED TO ITS POINT OF DEPARTURE.SDR CA981006017Valve · cracked(CAN) LANDING GEAR SELECTOR LEAKING FROM BODY CASTING. REPLACED.SDR CA980916027Fire Loop · malfunctioned(CAN) SHORTLY AFTER TAKEOFF, APU FIRE WARNING LIGHT CAME ON AND BELL SOUNDED. APU SHUT DOWN. FIRE DRILL COMPLETED. FIRE LIGHT REMAINED ON AND FIRE BELL SOUNDED INTERMITTENTLY. AIRCRAFT RETURNED. REPLACED TAIL PIPE AND EXHAUST DUCT FIRE DETECTION LOOPS ASSDR 98UAL900386Indication · malfunctionedRETURNED TO DENVER DUE TO LANDING GEAR INDICATION PROBLEMS. *S/D* LUBED GEAR HANDLE AND JACKED AIRCRAFT PER 32-60-05 AND SYSTEM CHECKS OK.SDR CA980908026Static Valve · leaking(CAN) ON 24 MONTH INSPECTION, FOUND CAPTAIN'S ALT STATIC SOURCE VALVE LEAKING, REPLACED.SDR CA981006016Valve · sticking(CAN) NR 3 ENGINE WOULD NOT GO INTO REVERSE. THRUST REVERSER DIRECTIONAL VALVE FOUND STICKING AND LEAKING.
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