Pratt & Whitney JT8D-15
Service difficulty reports · 2,710
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 = 'JT8D15' 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 = 'JT8D15' 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 2001UALA00429Sensor · failedDURING CLIMB FUEL QUANTITY INDICATION WAS ERRATIC DURING FUEL TRANSFER FROM THE NR 1 FUEL TANK. SUPPLEMENTAL DATA UPDATE. REPLACED INDICATOR.SDR DL72S010548Indicator · inoperativeNR 1 ENG LOW OIL PRESSURE / BYPASS LIGHT ILLUMINATED IN FLIGHT INSPECTED MAIN OIL FILTER FOUND APPRECIABLE COKE DEPOS RAN ENGINE WITH NEW FILTER INSPECTED FOUND VERY LITTLE COKE NOMETAL FOUND AT ANY TIME REPLACED SEC FILTER OIL PRESS INDIC NML.SDR 2001UALA00510Flap · out of adjCREW REPORTED AIRFRAME VIBRATION AT HIGHER SPEEDS. NO VIBRATION AT LOWER SPEEDS. SUPPLEMENTAL DATA UPDATE RIGHT HAND INBOARD AFT FLAP ECCENTRIC REQUIRED ADJUSTMENT. NO PARTS REPLACED. SYSTEM CHECKS NORMAL.SDR 2001UALA00384Stringer · dentedSTRINGER 22R AT STA 336 HAS DENT DAMAGE BEYOND ALLOWABLE LIMITS OF SRM 53-10-01. INSTALLED STRINGER REPAIR PER SRM 53-10-03 FIGURE 1. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00386Rod End · damagedNR 5 SLAT ACTUATOR ROD END ATTACH POINT HAS AN EXISTING REPAIR WITH DOUBLE DRILLED HOLE AND CRACKED CORNERS. REPAIRED RIB PER EVA G07938 WHICH INCORPORATES A DOUBLER AND FILLER ON THE SLAT BEAM WEB. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00387Rod End · damagedNR 5 SLAT ACTUATOR ROD END ATTACH POINT HAS AN EXISTING REPAIR WITH DOUBLE DRILLED HOLE AND CRACKED CORNERS. SUPPLEMENTAL DATA UPDATE REPAIRED RIB WITH DOUBLER AND FILLER ON THE SLAT BEAM WEB PER EVA G07938.MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00418Stringer · dentedSTRINGER 22R AT STA 336 HAS DENT DAMAGE BEYOND ALLOWABLE LIMITS OF SRM 53-10-01. SUPPLEMENTAL DATA UPDATE INSTALLED STRINGER REPAIR PER SRM 53-10-03 FIGURE 1. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00383Light · looseEMERGENCY EXIT LIGHT FELL OFF DURING LANDING. SUPPLEMENTAL DATA UPDATE REINSTALLED EMERGENCY EXIT LIGHT.SDR 2001UALA00385Skin · crackedRT ELEVATOR EXTERIOR SKIN UPPER SURFACE HAS A HALF INCH CRACK ON THE INBOARD FORWARD SKIN. INSTALLED DOUBLER REPAIR PER SRM 55-20-03 FIGURE 4. CALCULATED WEIGHT AND BALANCE PER SRM 51-80-07. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00372Accessory Unit · failedLANDING GEAR HANDLE COULD NOT BE RETRACTED INTO UP POSITION. LANDING GEAR HAD TO BE BROUGHT UP MANUALLY. SUPPLEMENTAL DATA UPDATE REPLACED LANDING GEAR ACCESSORY UNIT. ACCOMPLISHED WIRING CHECK BETWEEN LEVER LATCH SOLENOID AND LANDING GEAR ACCESSORY UNIT. ALSDR 2001UALA00359Pump · inoperativeAIRCRAFT DIVERTED TO DEN DUE TO INOPERABLE NR 2 RIGHT FUEL BOOST PUMP INDICATION. SUPPLEMENTAL DATA UPDATE. REPLACED NR 2 AFT LEFT CIRCUIT BREAKER.SDR 2001UALA00325Exhaust Pipe · crackedNR 1 ENGINE TAILPIPE CRACKED AT THE 11 OCLOCK POSITION. SUPPLEMENTAL DATA UPDATE CAUSE OF CRACKING UNDER INVESTIGATION. THE CRACKS WERE REPAIRED PER MM 78-34-05.SDR CA010406004Duct · broken(CAN) CREW REPORTED THAT THEY HAD A LOUD NOISE IN THE MID CABIN WHEN THE LEFT AIR CONDITIONING PACK WAS RUNNING. THEY ALSO NOTED THAT THE SMELL THAT WAS NOTICEABLE WHEN THE PACK WAS RUNNING. THE AIRCRAFT WAS REMOVED FROM SERVICE TO INVESTIGATE THE CREW REPORT SDR 2001UALA00312Indicator · malfunctionedNR 3 FUEL FLOW INDICATOR ERRATIC FOLLOWED BY 28 VOLT DC CB POPPED THR0UGH 500 FEET . ELECTRICAL ODOR SMELL IN COCKPIT. FUEL FLOW WILL OPERATE OKAY BUT FUEL FLOW TRANSMITTER WILL REQUIRE REMOVAL FOR REPAIR DUE TO CHAFED WIRE BEHIND TRANSMITTER. SUPPLEMENTAL DSDR 2001UALA00323Regulator · failedAT DEPARTURE TIME CREW LOST ALL OXYGEN PRESSURE TO ALL MASKS IN THE FLIGHT DECK. SUPPLEMENTAL DATA UPDATE FOUND THAT PRESSURE REDUCING REGULATOR WAS NOT LETTING AIR OUT OF PRESSURE REGULATOR VALVE. REPLACED CREW OXYGEN PRESSURE REDUCING REGULATOR PER MAINTENSDR 2001UALA00301Structure · corrodedFORWARD BILGE AREA BS 580 TO 600 STRINGER 28R CORRODED.SDR 2001UALA00304Angle · crackedFORWARD PIT BILGE AREA BS 580 TO 600 BETWEEN STRINGERS 27R AND 28R SUPPORT ANGLE CRACKED.SDR DL72S010462Transmitter · failedNBR 2 ENG OIL PRESSURE READ IN RED ON CLIMBOUT FROM OMA. REPLACED OIL PRESSURE TRANSMITTERSDR 2001UALA00303Angle · crackedLEFT HAND PRESSURE BOX ANGLE CRACKED FORWARD SIDE STATION 760. 3RD NUTPLATE UP FORWARD SIDE.SDR 2001UALA00308Web · crackedLEFT WING TRAILING EDGE VERTICAL SUPPORT WEB HAS CRACK WBL 249.3, INBOARD SIDE OF INBOARD AILERON.SDR 2001UALA00307Controller · malfunctionedCABIN PRESSURIZATION IN AUTO, CABIN PRESSURE CANNOT BE MAINTAINED (CABIN ALTITUDE RISES) IN DECENT. OK IF ENGINE POWER ADDED. PRESSURIZATION SYSTEM INADEQUATE WITH POWER BACK SAME FOR BOTH STANDBY AND AUTO. SUPPLEMENTAL DATA UPDATE FOUND LOW ENG BLEED PRESSURSDR 2001UALA00306Light · inoperativeLEFT FORWARD OVERWING EMERGENCY EXIT LIGHT INOP.SDR 2001UALA00310Stop · out of adjCREW REJECTED TAKEOFF AT 95 KNOTS DUE TO FORWARD DOOR LIGHT. SUPPLEMENTAL DATA UPDATE ADJUSTED DOOR STOPS AND CHECKED DOOR WARNING SYSTEM PER MAINTENANCE MANUAL. OPERATIONAL CHECK NORMAL.SDR 2001UALA00309Receiver · failedBOTH VOR NR 1 AND 2 OFF FLAGS DISPLAYED WITH CDI NEEDLES FLUX 10 - 20 DEGREES. SUPPLEMENTAL DATA UPDATE NR 1 NAV RECEIVER FAILED. REPLACED NR 1 NAV RECEIVER. OPERATIONS CHECK NR 1 & 2 NAV SATISFACTORY PER MM 42-20-02.SDR 2001UALA00305Indicator · failedCREW REPORTS AN OUTBOARD FLAP ASYMMETRIC LOCK OUT, OUTBOARD INDICATOR IS SPLIT, ONE SIDE IS 15 DEGREES OTHER SIDE IS 20 DEGREES, INBOARD FLAPS OK AND HANDLE IS AT 15 DEGREES. SUPPLEMENTAL DATA UPDATE REMOVED AND REPLACE OUTBOARD FLAP INDICATOR PER MAINTENANCESDR 2001UALA00311Controller · malfunctionedFLIGHT RETURNED TO LAS WITH NR 2 LEADING EDGE FLAP PROBLEM. FLAP WOULD NOT RETRACT. SUPPLEMENTAL DATA UPDATE ADJUSTED NR 2 LEADING EDGE FLAP LINKAGE AND CYCLED FLAPS SEVERAL TIMES. CHECKS NORMAL.SDR AU010334Actuator · faulty(AUS) MAIN CARGO DOOR REAR ACTUATOR EYE END BEARING MIGRATED RESULTING IN DISTORTION OF THE EYE END. MINOR DAMAGE TO RETRACTION ARM.SDR 2001UALA00244Light · inoperativeEMERGENCY LIGHT ASSEMBLY AT DOOR 2L WAS INOPERABLE. SUPPLEMENTAL DATA UPDATE REPLACED EMERGENCY LITE ASSEMBLY AT DOOR 2L. OPERATIONAL CHECK NORMAL.SDR 2001UALA00245Switch · intermittentDURING GEAR RETRACTION, THE RIGHT MAIN LANDING GEAR AND DOORS LIGHT REMAIN ILLUMINATED. LIGHT DISTINGUISHED WHEN THE GEAR WAS RECYCLED. SUPPLEMENTAL DATA UPDATE FOUND SWITCH INTERMITTENT AND CONNECTOR WITH BURNED PINS. REPLACED DOOR ACTUATOR SWITCH & ASSOCISDR 2001UALA00242Shutoff Valve · failedLOW FUEL INDICATION ON NR 2 TANK. AIRCRAFT DIVERTED TO DTW. SUPPLEMENTAL DATA UPDATE CROSSFEED SHUTOFF VALVE FAILED. REPLACED SHUTOFF VALVE.SDR 2001UALA00243Vent Line · leakingNR 3 FUEL TANK QUANTITY STEADILY DECREASED DURING CLIMB. SUPPLEMENTAL DATA UPDATE ELBOW VENT TUBE CRACKED. REPLACED VENT TUBE.SDR 01FDEA00183Line · leakingNR 2 LOW OIL PRESSURE BYPASS LIGHT CAME ON. FOLLOWED BY LOSS OF OIL QUANTITY SHUT DOWN NR 2 IN FLT PER CKLIST. *S/D* FOUND MAIN SCAVENGE OIL LINE LEAKING AT COUPLING NUT PACKINGS DETERIORATING. REMOVED AND REPLACED PACKINGS PER MM 79-20-002-2, MAIN OIL FILSDR 01FDEA00182Relief Valve · stuckNR 2 OIL BYPASS LIGHT ILLUMINATED. SECURE ENG PER RED TAB PROC. REMOVED AND REPLACED MAIN OIL SCREEN, FOUND FILTER PRESSURE RELIEF VALVE STUCK. REMOVED AND REPLACED VALVE PER PW JT8D72-009G518C-518D. INSP OIL SCREEN PER MM 79-00-000-2. NONE NOTED. LEAK ASDR 2001UALA00258Fitting · crackedRT WHEEL WELL AT STA 870 REPAIR FITTING CRACKED UNDER TRAPEZOID FITTING. REPLACED CRACKED WEB PER BAC DWG 65-25370 AND INSTALLED PER SRM 51-30-02.SDR 2001UALA00263Rib · crackedNR 6 SLAT ACTUATOR MOUNT RIBS CRACKED ON BOTH INBOARD AND OUTBOARD SIDES.SDR 2001UALA00222Oven · overheatedSMOKE IN GALLEY. SUPPLEMENTAL DATA UPDATE GALLEY OVEN ADJACENT TO DOOR 1R OVERHEATED & EMITTED SMOKE. ELECTRICAL HOOK-UPS CHECKED AND FOUND NORMAL. GALLEY OVEN TAGGED UNSERVICEABLE AND REPLACED. SUBSEQUENT OVENS NOW CHECK NORMAL.SDR 2001UALA00221Duct · brokenAIRCRAFT RTFL DUE TO NR 1 ENGINE FIRE WARNING LIGHT. SUPPLEMENTAL DATA UPDATE FOUND ANTI-ICE DUCT BROKEN. REPLACED DUCT. NO LEAKS FOUND AFTER DUCT REPLACEMENT. RAN ENG AT TAKEOFF POWER. NO ENGINE FIRE WARNINGS RESULTED. FIRE SYSTEM OPERATION TESTED GOODSDR CA010314006Circuit Board · shorted(CAN) ON TAKEOFF ROTATION MASTER WARNING LIGHT ILLUMINATED WITH NO LOSS OF ESSENTIAL POWER, ELEVATOR LOW PRESSURE LIGHT, GPWS WARNING LIGHTS, FLIGHT CONTROL PCU LIGHTS, ALL OIL PRESSURE/FILTER BYPASS LIGHTS, FLIGHT INSTRUMENT TRANSFER LIGHTS TRANSPONDER FAIL LSDR 2001UALA00214Control Valve · failedDURING CLIMB AIRCRAFT EXPERIENCED A PRESSURIZATION PROBLEM. AIRCRAFT RETURNED TO DEN. *S/D* REPLACED NR 1, AND NR 3 ENGINE HI STAGE BLEED AIR MODULATING VALVES. REPLACED LEFT AND RIGHT FLOW CONTROL VALVES.SDR 2001UALA00213Wire · brokenEMERGENCY EXIT SIGN AT DOOR 1L HAS A BROKEN POWER STRIP. SUPPLEMENTAL DATA UPDATE POWER STRIP FAILED. REPLACED POWER STRIP. OPERATIONS CHECK NORMAL.SDR 2001UALA00184Controller · failedAUTO PRESSURIZATION FAILED DURING CLIMB. *S/D* THE PRESSURE CONTROLLER FAILED. REPLACED THE ELECTRONIC PRESSURE CONTROLLER.SDR 2001UALA00187Adc · failedDURING CRUISE THE CAPTAINS ALTIMETER AND AUTOPILOT WERE INOPERABLE. SUPPLEMENTAL DATA UPDATE MAINTENANCE REPLACED CAPTS AIR DATA COMPUTER - OPS CHECK NORMAL (REFERENCE AMIS ITEM 9522003) NO FURTHER PROBLEMS REPORTED.SDR 2001UALA00188Wire · brokenEMERGENCY EXIT SIGN IS LOOSE AND EEL LIGHTING IS INOPERABLE. SUPPLEMENTAL DATA UPDATE ACCOMPLISHED CABLE ASSEMBLY INTERIM REPAIR PER MM 33-50-32. OPERATIONS CHECK NORMAL.SDR EISA20010034Fitting · looseINFLIGHT NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. ASSOCIATED PRESSURE INDICATED 10-12 PSI. ENGINE SHUT DOWN IAW EXPRESS ONE CHECKLIST, DIVERTED INTO OMA. REPLACED GEARBOX FITTING TO DIFFERENTIAL PRESSURE PORT IAW 72-61-00. NO DEFECTS NOTED.SDR CA010313021Gearbox · worn(CAN) AIRCRAFT WAS ENROUTE FROM CALGARY TO WINNIPEG WHEN THE RIGHT HAND ENGINE EXPERIENCED A LOSS OF ENGINE OIL. THE CREW SHUT DOWN THE ENGINE WHEN THE OIL PRESSURE STARTED TO DROP AND THE ENGINE OIL TEMPERATURE BEGAN TO CLIMB. THE OIL APPEARED TO HAVE LEAKED SDR 2001UALA00223Tip Cap · puncturedRT STABILIZER AFT END TIP PUNCTURED. REPAIRED TIP PER SRM 51-40-09.SDR 2001UALA00224Skin · delaminatedRT VERTICAL FIN PANEL 9608 IS DELAMINATED. REPAIRED PANEL PER GN MM 1-0-1-24 AND GN MM 1-0-1-66. INSTALLED NEW CORE FILLER AND REPLACED INNER AND OUTER SKIN.SDR 2001UALA00226Rib · crackedNR 5 SLAT ACTUATOR ATTACHMENT RIBS ARE CRACKED. REPLACED RIBS PER BAC DWG 65-17276, GN MM 1-0-0-23, AND INSTALLED PER SRM 51-30-02.SDR 2001UALA00227Skin · puncturedRT WING NR 8 GROUND SPOILER PUNCTURED. REMOVED SPOILER PER MM 27-61-01. REMOVED DOUBLERS AND LOWER SKIN, REPAIRED SKIN PER GN MM 1-0-1-66, INSTALLED PANEL PER MM 27-61-01, AND RIG CHECKED PER MM 27-60-01. OPERATIONS CHECK NORMAL.SDR 2001UALA00228Skin · crackedNR 13 SPOILER PANEL LOWER SKIN IS CRACKED AROUND THE ACTUATOR ATTACHMENT. REPLACED SPOILER PANEL PER MM 27-61-04. RIGGED AND OPERATIONS CHECK NORMAL PER MM 27-61-04.
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