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 CA970428010Hose Assembly · leaking(CAN) ON CLIMB HYDRAULIC SYSTEM 'A' LOSS OF QUANTITY AND PRESSURE. FUEL DUMPED AND LANDED. REPLACED HYDRAULIC HOSE AT L/H ELEVATOR POWER PACK.SDR 97UAL900238Lamp · inoperativeEEL LIGHT INOPERATIVE AT SEAT 18C. REPLACED EEL LAMP AND CABLE. OPS CHECK GOOD.SDR 9706479874Oil Press Trans · malfunctionedDURING CRUISE FLIGHT, THE RIGHT ENGINE OIL PRESSURE INDICATION DECREASED TO 32 PSI. AIRCRAFT DIVERTED TO ATL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE OIL PRESSURE TRANSMITTER. OPERATIONAL CHECK OK.SDR 97UAL900230Power Supply · inoperativeEMERGENCY SLIDE LIGHT AT DOOR 2R INOPERATIVE. REPLACED BATTERY, POWER SUPPLY, AND REFLECTOR. OPS CHECK GOOD.SDR 9705739868Epr Indicator · dirtyDURING TAKEOFF ROLL AT 20 KNOTS, THE LEFT ENGINE EPR INDICAITON BECAME ERRATIC. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REMOVED THE LEFT ENGINE EPR INDICATOR, CLEANED, AND RESEATED THE CONNECTOR. ENGINE WAS RUN TO 80 PERCENT POWER. ENGINSDR 97UAL900208Light · inoperativeEMERGENCY SLIDE LIGHT AT DOOR 1R INOP. RELAMPED EMERGENCY SLIDE LIGHT. OPS CHECK GOOD.SDR CA970327007Line · failed(CAN) ONE HOUR OUT 'B' SYSTEM QTY LOSS, AIRCRAFT RETURNED. FOUND 'B' PUMP PRESSURE LINE FAILED. REPLACED.SDR 9704822711Fuel Control · failedDURING CRUISE AT FL350, THE NR 2 ENGINE EXPERIENCED COMPRESSOR STALLS. CREW REDUCED POWER TO IDLE MOMENTARILY AND THEN RESTORED POWER. AS POWER WAS RESTORED, NO STALLS OCCURRED AND PARAMETERS WERE NORMAL. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT FURTHER SDR 97UAL900181Battery · failedHAD A BURNING SMELL IN THE AIRPLANE AND FOUND SMOKE COMING FROM THE BATTERY AND BATTERY CHARGER. REMOVED AND REPLACED BATTERY AND CHARGER. THE 737-291 AIRCRAFT HAVE A PROJECT TO INSTALL NEW CELLS. THE OLD CELLS HAVE BEEN FOUND TO OCCASIONALLY OVERHEAT BECASDR 97UAL900165Gear Handle · malfunctionedWHEN PLACING GEAR HANDLE FROM UP TO OFF, BOTH MAIN GEAR RED AND GREEN LIGHTS CAME ON AND NOTICABLE AIR DRAG FELT. HYDRAULICALLY AND MANUALLY EXTENDED LANDING GEAR SEVERAL TIMES. LUBRICATED LANDING GEAR HANDLE. GEAR LIGHTS WORKING NORMALLY. GEAR HANDLE MAY SDR 97FDEA00125Compressor · stalledAFTER TAKEOFF AND CLIMBING THROUGH 1,000 FEET, THE AIRCRAFT EXPERIENCED AN APPARENT COMPRESSOR STALL. AIRCRAFT SURGED WITH A NOTICEABLE ROLL TO THE LEFT AND ACTIVATION OF THE AUTO PACK TRIP SYSTEM. DUMPED FUEL AND RETURNED FOR LANDING. VISUALLY INSPECTEDSDR 97UAL900163Light · inoperativeEMERGENCY EXIT SIGN AT DOOR 1 LEFT WILL NOT COME ON. *S/D* THE EMERGENCY EXIT SIGN LIGHT ASSEMBLY WAS REPLACED. SHOP FOUND CAPACITOR FAILURE AS LIKELY CAUSE. LIGHT ASSEMBLY WAS REPLACED, OPS CHECK GOOD.SDR 9703799861Transmitter · failedEN ROUTE, NR 1 ENGINE OIL QUANTITY INDICATION BEGAN DECREASING. THE FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE OIL QUANTITY TRANSMITTER AND INDICATOR WITH SERVICEABLE UNITS. OIL QUANTITY SYSTEM OPERATION SATISFACTORY.SDR 97UAL900148Light · inoperativeEMERGENCY EXIT LIGHT AT LOWER FORWARD CORNER OF DOOR 1R INOP. REPLACED EMERGENCY EXIT LIGHT AT DOOR 1R, OPERATION CHECKS NORMAL.SDR 97UAL900143Tire · failedABORTED TAKEOFF DUE TO BLOWN NR 2 TIRE AND APPARENT BRAKE FIRE. INVESTIGATION REVEALED THAT EITHER NR 3 OR NR 4 TIRE BLEW DUE FOR UNKNOWN REASONS. NO FIRE OCCURRED. REPLACED LT AND RT MLG INNER CYLINDERS. REPLACED ALL FOUR BRAKE AND TIRE/WHEEL ASSEMBLIES. SDR 97UAL900140Light · inoperativeEMERGENCY EXIT LIGHT ABOVE DOOR 2 LEFT INOP. REPLACED LIGHT ASSEMBLY, OPS CHECK GOOD.SDR 97UAL900142Connector · looseEEL LIGHTS OVER MLG VIEWER INOPERABLE. SECURED LIGHT STRIP CONNECTOR, OPS CHECK GOOD.SDR 9703372716Relief Valve · malfunctionedDURING TAKEOFF AND CLIMB, THE NR 3 ENGINE OIL PRESSURE INDICATION WAS HIGH. CREW REDUCED POWER ON THE NR 3 ENGINE AND DUMPED 16,000 LBS OF FUEL. THE AIRCRAFT DIVERTED TO MSP AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE OIL PRESSURE TRANSMITSDR AU970147Wheel · fractured(AUS) NO4 MAIN WHEEL CENTRE HUB FAILED. DAMAGE TO BRAKE AND WHEEL BEARING. FUSE PLUG MELTED AND TYRE DEFLATED.SDR AU971262Wheel · fractured(AUS) NO4 MAIN WHEEL HALF FAILED IN THE CENTRE HUB AREA. DAMAGE CAUSEDTO THE BRAKE AND WHEEL BEARING. FUSE PLUG MELTED AND TYRE DEFLATED.SDR 97ZZZM333Engine · fodFLT 730 - MCO-TOL - NR 2 ENGINE STALLED ON POWER UP. IN IDLE, ALL INDICATIONS SHOWED NORMAL (NO OVERTEMP). VISUAL INSPECTION REVEALED MINOR C-1 DAMAGE, MAJOR C-2 AND A SUBSEQUENT BOROSCOPE INSPECTION REVEALED THE C-12 AND C-13 BLADE DISTRESS WAS PRESENT. RESDR 97UAL900114Battery · dischargedEMERGENCY LIGHT AT DOOR 1R IS INOPERABLE. REPLACED BATTERIES, OPS CHECK GOOD.SDR 97ZZZM334Engine · fodFLT 681 - LOG STATED 'CHECK NR 2 ENGINE, HEARD LOUD THUMP'. ON INSPECTION OF INLET AND EXHAUST, FOUND FOREIGN OBJECT DAMAGE TO C-1 AND C-2 BLADES. REMOVED AIRCRAFT FROM FLIGHT LINE FOR ENGINE CHANGE AT HANGAR. REMOVED DEFECTIVE ENGINE AND REPLACED IT WITH ASDR CA970220002Clamp · loose(CAN) AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. ALL MODES UNSUCCESSFUL. BLEED AIR CLAMP LOOSE AND JUMPED OVER FLANGE. DUCT AND CLAMP SECURED.SDR 97UAL900101Lens · missingLENS ON EXIT LIGHT OVER LEFT OVERWING EMERGENCY EXIT DOOR MISSING. REPLACED LENS ASSEMBLY.SDR 97UAL900093Light · inoperativeEMERGENCY LIGHTS NOT ARMED, LIGHT INOP. RELAMPED LIGHT, OPS CHECK GOOD.SDR CA970306012Sensor · dirty(CAN) UNABLE TO RETRACT LANDING GEAR, LANDING GEAR LEVER WOULD NOT PASS THE OFF POSITION. DUMPED FUEL AND RETURNED. CLEANED AIR/GROUND SENSOR ACTUATOR CONNECTOR.SDR CA970318002Bearing · failed(CAN) ON LANDING CREW REPORTED NOSE WHEEL SHIMMY. INBOARD BEARING OF THE L/H WHEEL WAS FOUND TO HAVE FAILED. THE ROLLER AND CAGE ASSEMBLY DEPARTED THE AIRCRAFT AND THE SECTION IN CONTACT WITH THE AXEL WELDED ITSELF TO THE AXLE. SEVERAL PIECES OF THE BEARINGSDR 9702092717REpr Indicator · malfunctionedAS TAKEOFF POWER WAS APPLIED, THE NR 3 ENGINE EPR INDICATION DID NOT RESPOND. SYSTEM WAS PLACED ON MEL AND FLIGHT CONTINUED TO DESTINATION. MAINTENANCE LATER REPLACED THE NR 3 ENGINE EPR INDICATOR.SDR 97UAL900091Proximity Sensor · malfunctionedWITH FLAPS UP DURING CRUISE, THE LEADING EDGE FORWARD TRANSIT LIGHT AND THE OVERHEAD ANNUNCIATOR TRANSIT LIGHT FOR SLAT NR 2 IS ON STEADY. SUPPLEMENTAL DATA UPDATE NUMBER 2 SLAT FULL EXTEND PROXIMITY SENSOR WILL NOT DEACTUATE. REPLACED PROXIMITY SENSOR ANDSDR 97UAL900069Windshield · bird strikeAT 100 KIAS, HEARD A LOUD BANG AND SAW DUST OR SMOKE ABOVE GLARESHIELD. *S/D* SUSPECTED BIRD STRIKE. NOSE AND COCKPIT WERE INSPECTED WITH NO DEFECTS NOTED. AIRCRAFT HAS CONTINUED OPERATING NORMAL.SDR CA970128008Clamp · loose(CAN) DURING CLIMB #3 OVERHEAT STRUT LIGHT CAME ON, REDUCED ENGINE POWER, LIGHT WENT OUT. DUMPED FUEL LANDED. ANTI-ICE VALVE, 6TH AND 13TH STAGE BLEED AIR LEAKING, TIGHTENED.SDR TWAA9710012Tie Down Track · corrodedMCI - DURING OP-16, FOUND CORROSION AT MOUNT SCREW HOLES ON AFT CARGO RT TIEDOWN TRACK, FROM 1007 TO 1155. REPLACED TRACK PER SRM 51-01, PAGE 1 AND TWA STANDARD PRACTICES. (M)SDR 97UAL900022Cover · looseEMERGENCY EXIT LIGHT COVER LOOSE ON FORWARD CABIN DOOR 2L. SECURED DOOR 2L EMERGENCY EXIT LIGHT COVER, OPS CHECK GOOD.SDR CA970109006Apu · failed(CAN) APU AUTO SHUTDOWN DUE LOW OIL PRESSURE. LOW OIL PRESSURE SWITCH REPLACED, NO FIX, SUSPECT OIL PUMP. APU REPLACED.SDR CA970109007Track · broken(CAN) #3 FLOOR TRACK BROKEN OUT AT STATION 365, #1 PALLET POSITION. FORWARD LOCK DAMAGED WITHIN 40 INS OF SPLICE. TRACK REPLACED.SDR CA970109010Detector · shorted(CAN) PRIOR TO DEPARTURE APU FIRE WARN SOUNDED. AIRCRAFT EVACUATED USING REAR SLIDES AND FORWARD ENTRY DOORS. M515 LOOP FOUND SHORTED TO GROUND. REPLACED.SDR CA970109011Solenoid · failed(CAN) LANDING GEAR LEVER WOULD NOT MOVE TO GEAR UP POSITION WITHOUT USE OF OVERRIDE LEVER. LANDING GEAR LEVER LOCK SOLENOID REPLACED.SDR 9700619863Epr Indicator · malfunctionedAS TAKEOFF POWER WAS APPLIED, THE LEFT ENGINE EPR INDICATION WAS ERRONEOUS. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE LEFT ENGINE EPR INDICATOR, OPERATIONAL CHECK OK.SDR 96UAL900997Battery Pack · dischargedEMERGENCY LIGHT AT THE TRAILING EDGE OF THE RT WING IS INOP. RELAMPED AND REPLACED BATTERY, OPS CHECK OK.SDR CA970107007Switch · failed(CAN) ON DEPARTURE #2 ENGINE START VALVE LIGHT CAME ON AND REMAINED ON. ENGINE SHUTDOWN. REPLACED VALVE.SDR 9626909853N1 Indicator · malfunctionedDURING TAKEOFF ROLL, THE RIGHT ENGINE N1 INDICATION WAS ABNORMALLY LOW. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE N1 INDICATORS FOR BOTH ENGINES, OPERATIONAL CHECK OK.SDR 9626719869Pt 2 Line · looseDURING CLIMB, THE RIGHT ENGINE EPR INDICATION WAS ABNORMAL. A/C RETURNED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE TIGHTENED THE RIGHT ENGINE PT-2 FLEX LINE. OPERATIONAL CHECK WAS OK.SDR CA961217003Skin · cracked(CAN) 3/4 INCH CRACK IN THE LEFT HAND FUSELAGE SKIN, 4 INCHES AFT OF THE OVERWING LIGHT, AT STATION 520 STRINGER 16. REPAIRED AS PER SRM.SDR CA961216002Detector · damaged(CAN) ON CLIMB #2 ENGINE FIRE WARNING, AIRCRAFT RETURNED, FIRE WARNING STAYED ON FOR SEVERAL SECONDS, ENGINE SHUT DOWN AND FIRE BOTTLE FIRED. CONDITION REMAINED THE SAME WITH FIRE WARNING INTERMITTENT. FIRE SENSING ELEMENT DAMAGED, REPLACED.SDR CA961220003Switch · intermittent(CAN) TEN MINUTES AFTER TAKEOFF, CLIMBING THROUGH 20,000 FEET #2 START VALVE OPEN LIGHT ILLUMINATED. ENGINE SHUT DDOWN, LIGHT OUT AND DUCT PRESSURE UP. #2 START PRESSURE SWITCH REPLACED.SDR CA961220005'B' Nut · loose(CAN) ON TAKEOFF 'A' SYSTEM QTY INDICATED ZERO. MAIN GEAR EVENTUALLY RETRACTED BECAUSE IT WAS ALREADY SELECTED UP. 'A' SYSTEM CYCLED ON AND OFF SEVERAL TIMES AND INDICATED 200 PSI. EMERGENCY DECLARED AND LANDING CARRIED OUT. PRESSURE LINE 'B' NUT LOOSE, TIGHTESDR CA961220006Start Valve · intermittent(CAN) ON CLIMB RH STARTER VALVE OPEN LIGHT CAME ON. ENGINE SHUT DOWN. PNEUMATIC STARTER REGULATING AND SHUT OFF VALVE REPLACED.SDR HALA96164Engine · failedHNL - FLT 529 - LEFT OIL STRAINER CLOGGING LIGHT ILLUMINATED DURING CLIMB-OUT, LT WOULD NOT EXTINGUISH W/THROTTLE BACK TO IDLE. ALL ENGINE INSTRUMENT READINGS NORMAL. AIR RETURN TO HNL. REMOVED NR 1 ENGINE MAIN OIL FILTER. FOUND EXCESSIVE AMT OF FERROUS MASDR 96UAL900911Boost Pumps · failedAFTER TAKEOFF, NUMBER ONE ENGINE FORWARD AND AFT LOW PRESSURE LIGHTS ILLUMINATED. CIRCUIT BREAKERS WERE FOUND POPPED, RETURNED TO DEN. *S/D* REPLACED FWD AND AFT FUEL BOOST PUMPS, FUEL PANEL, FWD AND AFT CIRCUIT BREAKERS, BLED PUMP LOW PRESSURE SWITCHES, SU
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