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 CA000731005Line · leaking(CAN) ON FINAL INTO YYZ, A COMPLETE LOSS OF A SYSTEM HYDRAULIC PRESSURE OCCURRED. WHEN TRAILING EDGE FLAPS SELECTED, WARNING LIGHTS AND A LEADING EDGE SLAT ASYMMETRIC WARNING INDICATION. AN EMERGENCY WAS DECLARED. FLAPS AND GEAR WERE LOWERED MANUALLY, FLIGHT LSDR 2000UALA00422Actuator · bypassingNR 5 SLAT NOT RETRACTING TO FULL UP. *S/D* FOUND NR 5 SLAT ACTUATOR BYPASSING. REPLACED THE NUMBER 5 SLAT ACTUATOR.SDR 20010104AP010Gearbox · leakingLAS - FLT 402 - AFTER INITIAL START THE NR 3 ENGINE LOST ALL OIL. REMOVED AND REPLACED THE NR 3 ENGINE PER MM. OPERATIONAL CHECKED AND FOUND OK. (M)SDR 2000UALA00408Fire Loop · damagedNR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. *S/D* FOUND LOWER LOOP M337 (LOOP A) SHORTED. REPLACED LOWER LOOP AND SYSTEM TESTED NORMAL. REPLACED ENGINE FIRE BOTTLES PER MM 26-21-01.SDR CA000718007Transmitter · failed(CAN) ON TAKEOFF ROLL AT TAMPA, ABANDONED TAKEOFF AT 70 KNOTS, DUE NR 1 EPR DID NOT INDICTAE ABOVE 1.6 EPR. NR 1 EPR TRANSMITTER REPLACED AS PER WORK CARD 4241.SDR 2000UALA00391Battery Pack · inoperativeRIGHT HAND EMERGENCY EXIT LIGHTS INOPERATIVE AT FORWARD AND AFT OF EMERGENCY EXIT. *S/D* REPLACED THE BATTERY PACK.SDR SCNA00067Start Valve · failedDURING CRUISE FLIGHT THE NUMBER THREE ENGINE START VALVE OPEN WARNING LIGHT ILLUMINATED. THE CREW SHUT DOWN THE ENGINE PER C.O.M. PROCEDURES. THE ENGINE SATRT VALVE PRESSURE SWITCH WAS REMOVED AND REPLACED. OPERATIONALLY CHECKS GOOD.SDR 2000UALA00755Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-11.SDR 2000UALA00375Fire Loop · damagedOVERHEAT WARNING LIGHT ON. *S/D* REPLACED LOWER OVERHEAT SENSING LOOP ON NR 1 ENGINE PER MM 26-11-04. SYSTEM WAS TESTED NORMAL PER MM 26-12-02.SDR SCNA00066Fuel Control · failedDURING THE TAKEOFF ROLL AT LAS, THE NUMBER TWO ENGINE WOULD NOT DEVELOP POWER ABOVE APPROXIMATELY IDLE POWER. THE TAKEOFF WAS ABORTED AT 60 KNOTS, RETURNED TO GATE. REMOVED AND REPLACED ENGINE NUMBER TWO FUEL PUMP AND FUEL CONTROL UNIT. OPERATIONAL AND LEAKSDR HALA0000206O-Ring · leakingHNL - FLT 357 - FUEL SMELL NOTICED ON TAXI IN HNL. REPLACED ALL SEALS ON RIGHT ENGINE AND P/D VALVE. ENGINE RUN, NO LEAKS. OPS OK. REMOVED AND REPLACED H20 SEPARATOR COALESCER BAGS. OPS CHECK OK. LEAK CHECK GOOD. (M)SDR CA000706001Gcu · failed(CAN) NR 2 ENGINE GENERATOR SYSTEM FAILED, UNABLE TO ESTABLISH APU ON AIRCRAFT BUSS. AIRCRAFT DIVERTED TO YHZ. NR 2 GENERATOR CONTROL PANEL REPLACED AS PER WORK CARD, SYSTEM CHECKED SERVICEABLE. APU GENERATOR OPERATIONS CHECKED NORMAL WHEN FUNCTIONED GROUND ANSDR CA000720013Switch · loose(CAN) CARGO DOOR LIGHT ILLUMINATED IN FLIGHT DURING MODERATE TURBULENCE. IT EXTINGUISHED AT DIFFERENTIAL PRESSURE OF 7.4 PSI. FOUND MAIN CARGO DOOR CLOSED MICRO SWITCH LOOSE. RESECURED, ADUSTED, TESTED AND SEATTED DOOR CLOSED MICRO SWITCH I.A.W. AEI M/M 7-11 PSDR CA000621004Switch · failed(CAN) ON TAKE, THRUST REVERSER ISOLATION VALVE WARNING LIGHT ILLUMINATED. RETURNED TO YYZ. THRUST REVERSERS OPERATED AS PER WORK CARD 1187, COULD NOT DUPLICATE DISCREPANCY. REPLACED NR 1 AND 2 THRUST REVERSER PRESSURE SWITCHES PER MM 78-31-16. OVERWEIGHT LANDISDR SPAA0000024Intermed Gearbox · leakingFLT 214 FROM IFP TO DTW: NR 2 ENGINE WAS SHUT DOWN IN FLIGHT FOR LOSS OF OIL QUANTITY AND PRESSURE. THE AIRCRAFT DIVERTED TO ABQ. INVESTIGATION REVEALED THAT THE LP5 PORT FITTING ON THE NR 2 ENGINE ACCESSORY GEARBOX WAS LOOSE DUE TO DAMAGED INTERNAL THREADS TSDR 2000UALA00305Generator · failedCREW REPORTS, NR 1 GENERATOR FAILED IN CRUISE WITH ZERO VOLTS AND ZERO FREQUENCIES. *S/D* THE NR 1 ENGINE GENERATOR WAS REPLACED AS WELL AS THE NR 1 CONSTANT SPEED DRIVE TRANSMISSION AS PRECAUTIONARY.SDR 2000UALA00228Panel · failedUNABLE TO CONTROL CABIN PRESSURATION IN AUTO OR STANDBY. *S/D* A FAILURE OF THE CABIN PRESSURE SELECTOR PANEL. REPLACED CABIN PRESSURE SELECTOR.SDR 2000UALA00226Rod End · brokenRIGHT MAIN LANDING GEAR WOULD NOT EXTEND HYDRAULICALLY. MANUAL EXTENSION WAS SUCCESSFUL. *S/D* DURING MAINTENANCE EVALUATION OF RT MLG ASSSEMBLY DUE TO USE OF MANUAL EXTENSION TO LOWER GEAR, FOUND RT MLG UPLOCK ACTUATOR ROD END BROKEN.SDR 2000UALA00754Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-11.SDR 2000UALA00282Sensor · out of adjAFT CARGO LIGHT INDICATION. *S/D* ADJUSTED DOOR SENSOR TARGET. DOOR INDICATION SYSTEM HAS PERFORMED NORMAL SINCE THE ADJUSTMENT.SDR CA000511009Attach Fitting · broken(CAN) ON APPROACH WHEN LANDING GEAR LOWERED CREW REPORTED A BANGING NOISE FROM THE AREA OF THE NOSE. INSPECTION AT THE GATE FOUND THE TAXI LIGHT SUPPORT HAD BROKEN AND THE TAXI LIGHT WAS TRAILING THE GEAR BY THE WIRE HARNESS. REPAIRED.SDR 2000UALA00753Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-11.SDR 2000UALA00188Blanket · wornELECTRICAL SMELL REPORTED AT ROW 11 SIDEWALL NEAR FLOOR. *S/D* FOUND INSULATION BLANKET ON APU DUCT DETERIORATED. REPLACED INSULATION BLANKET ON APU BLEED DUCT.SDR C1HA200092003Duct · failedAFTER TAKEOFF CREW REPORTED FIRE WARNING ON NR 1 ENGINE. CREW FOLLOWED STANDARD PROCEDURES AND RETURNED TO MBJ.CAUSE: RUPTURED 13TH STAGE SADDLE DUCT #1 ENG.SDR 0000749881Warning Light · illuminatedTHE LEFT ENGINE REVERSER UNLOCK LIGHT INDICATION ILLUMINATED DURING TAKEOFF. TAKEOFF WAS ABORTED AT 101 KNOTS. AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE PLACED THE LEFT ENGINE REVERSER ON MEL 78-1 AND COMPLIED WITH DISPATCH DEVIATION GUIDESDR CA000410002Switch · failed(CAN) SHORTLY AFTER TAKEOFF THE THRUST REVERSER ISOLATION VALVE CAME ON THE OVERHEAD PANEL. CHECKLIST CAFFIED OUT, A/C RETURNED. LIGHT WENT OUT WHEN THE LANDING GEAR LOWERED. NR 1 THRUST REVERSER HYDRAULIC SYS PRESSURE SWITCH REPLACED.SDR C1HA200093001Fuel Control · blockedDURING TAKEOFF ROLL, ENGINE NR 1 EPR, N1, N2, FUEL FLOW FLUCTUATED. FUEL CONTROL MOISTURE TRAP HAD PLUGGED ORIFICE.SDR 2000UALA00153Line · leakingLOST OF SYSTEM ''A'' HYDRAULICS DUE TO A HYDRAULIC LEAK FROM A FLEX LINE. *S/D* LEAK WAS FOUND COMING FROM LEFT HAND MAIN LANDING GEAR LOCK ACTUATOR. REPLACED DAMAGED HYDRAULIC FLEX LINE.SDR 2000UALA00147Transceiver · malfunctionedNUMBERS 1 AND 2 VERY HIGH FREQUENCY COMMUNICATIONS SYSTEMS FAILED FOR FIVE MINUTES. *S/D* REPLACED THE NUMBER 1 VERY HIGH FREQUENCY COMMUNICATIONS TRANSCEIVER (P/N 6221181003) AND THE NUMBER 1 AUDIO CONTROL PANEL (P/N G283304).SDR CA000410012Plug · damaged(CAN) RT MLG SIDE STRUT LOWER SEGMENT PLOG ADRIFT. PLUG CRACKED NEW PLUG INSTALLED.SDR 20000420AP010Generator · malfunctionedSAL - FLT TA561 - DURING CLIMB, THE CAPTAIN REPORTED TROUBLE WITH THE ELECTRICAL SYSTEM, F/O SIDE INSTRUMENTS LOST ELECTRICAL POWER, SEVERAL CIRCUIT BREAKER POPPED OUT DUE TO THIS SITUATION THE AIRCRAFT RETURN TO SAL STATION FOR MAINTENANCE. AFTER AN UNEVENTFSDR 2000UALA00130Skin · crackedTHE FUSELAGE SKIN CRACKED ALONG STRINGER S-25L AT BODY STATION 935. REMOVED THE EXISTING ADJACENT DOUBLER. FABRICATED AND INSTALLED THE NEW EXTENDED DOUBLER.SDR 20000619AP005Turbine Wheel · failedCUN-MSY - DURING CLIMB-OUT, THE NR 2 ENGINE FAILED IN FLIGHT, NR 2 ENGINE THROTTLE WENT FULL FORWARD AND HIGH VIBRATION STARTED WITH LOSS OF OIL QTY AND PRESSURE. LANDED WITHOUT FURTHER INCIDENT. FERRIED THE A/C ON TWO ENGINES TO MAINTENANCE. ENGINE WAS REPSDR 20000619AP003Blade · damagedDURING POST FLIGHT WALK AROUND, FOUND NR 1 ENGINE WITH FOD DAMAGE THROUGH THE INTAKE. AFTER FURTHER INSPECTION FOUND 22 FIRST STAGE BLADES DAMAGED, EIGHT BLADES WERE OUT OF REPAIRABLE CONDITION. FERRIED A/C FOR MAINTENANCE. FOD SUSPECTED. REPLACED ENGINE. SDR 20000420AP008Pump · damagedSJO - FLT LR626 - AFTER TAKEOFF, NR 1 ENGINE EXPERIENCED A FLAMEOUT, DUE TO THIS SITUATION THE ENGINE WAS SHUTDOWN (IFSD), AND THE AIRCRAFT RETURNED TO SJO AIRPORT. AFTER AN UNEVENTFUL LANDING, MAINTENANCE TECHNICIANS PERFORMED COMPLETE INSPECTION OF ENGINE NSDR CA000215019Actuator · failed(CAN) A/C TURNBACK DUE TO LE FLAP ACTUATOR WOULD NOT RETRACT. NR 2 LE FLAP INDICATES DOWN WHEN FLAP IN RETRACT POSITION. REPLACED.SDR SCNA00014Compressor · malfunctionedDURING LEVEL OFF AND ON DESCENT, THE NUMBER TWO ENGINE UPON ADVANCING THRUST LEVERS EXPERIENCED COMPRESSOR STALL. ENGINE RUN CARRIED OUT. HOT AND COLD INSPECTION CARRIED OUT AS PER MM 7200. SURGE BLEED OPERATION CHECK OKAY AS PER 7200.SDR CA000209003Bolt · broken(CAN) NR 4 SLAT BOLT BROKEN THROUGH GREASE PASSAGE DUE TO LACK OF LUBRICATION, BOLT WORN. REPLACED.SDR 2000UALA00039Fire Loop · shortedTHE AIRCRAFT DIVERTED DUE TO AN AMBER ALERT ON THE AUXILIARY POWER UNIT FIRE INDICATION. *S/D* THE LOWER LOOP M334 SHORTED TO GROUND. REPLACED THE LOWER LOOP M334 AND AUXILIARY POWER UNIT FIRE BOTTLE.SDR 0000179863Pump · failedRIGHT ENGINE FLAMED OUT AFTER TAKEOFF AT APPROXIMATELY 200 AGL. CREW DECLARED A YELLOW EMERGENCY AND FLIGHT WAS RETURNED TO MEM. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RIGHT ENGINE FUEL PUMP HAD FAILED. REPLACED PUMP AND FUEL CONTROL. OPERATISDR AU000128017Oil Filter · leaking(AU) OIL FILTER BYPASS SW BANJO FITTING HAD STRIPPED THREADS CAUSING OIL LEAK.SDR CA000128017Gearbox · leaking(CAN) OIL FILTER BYPASS SW BANJO FITTING HAD STRIPPED THREADS CAUSING OIL LEAK.SDR 2000UALA00005Detector · shortedTHE AUXILIARY POWER UNIT FIRE BOTTLE DISCHARGED BY THE FLIGHT CREW . *S/D* THE SHORTED M717 DETECTOR CAUSED A FALSE FIRE INDICATION. REPLACED THE M717 LOOP AND THE AUXILIARY POWER UNIT FIRE BOTTLE. REPLACED THE M515 LOOP AS A PRECAUTION.SDR AU000110Floorbeam · corroded(AUS) FLOORBEAM UPPER CHORD CORRODED AROUND ANCHOR NUTS IN THE AREABETWEEN RBL20 AND RBL60.SDR HALA0000005Blade · crackedHNL - FLT 181 - NR 1 ENGINE HAD COMPRESSOR STALL UPON THROTTLE ADVANCE FOR PARKING. FOUND NR 10 COMPRESSURE BLADE CRACK AT C-1 FAN HUB. REMOVED NR 1 ENGINE ASSY PER HAL M144. (X)SDR CA000110016Window Post · cracked(CAN) INSP REVEALED CRACKS OF C-D WINDOW POST UPPER OTBD CORNERS OF LT AND RT WINDOWS. ROUTED OUT TO REVEAL UNDER SKIN ALSO CRACKED FROM SITE MARKS. REPAIRED PER BOEING TELEX.SDR CA000110017Fitting · damaged(CAN) REMOVED FITTING FOR BEARING REWORK AND FOUND HIDDEN DAMAGE. THREE OF FOUR BOLTS FROZEN IN BORES, TWO BOLTS SHEARED, EVIDENCE OF EXTENSIVE CORROSION TO SHEAR FACE. FWD INBD BOLT CUT FOR REMOVAL. FITTING REPLACED.SDR 9905389875Engine · failedDURING TAKEOFF, THE LEFT ENGINE FAILED AT ABOUT 100 KNOTS AIRSPEED WITH AN ASSOCIATED EPR INDICATION OF 1.0, A DECREASE OF N1 AND N2 RPM SPEED, AND A NOTICEABLE ENGINE VIBRATION. TAKEOFF WAS ABORTED WITHOUT INCIDENT AND THE FLIGHT RETURNED TO BLOCKS. MAINTENSDR 99UAL900652Warning Light · illuminatedTHE CREW REPORTED THE 'A' HYDRAULIC SYSTEM QUANTITY INDICATION OF 1.9 GALLONS ALONG WITH THE ILLUMINATION OF THE LOW QUANTITY LIGHT FOR THE STANDBY HYDRAULIC SYSTEM.SDR CA991208056Csd · failed(CAN) ON TAKEOFF, NR 1 GENERATOR DROPPED OFF-LINE WHEN POWER APPLIED FOR TAKEOFF. TAKEOFF REJECTED DUE NR 2 GEN US AND ON MEL, APU TOOK OVER POWER ELECTRONICS. NR 1 GENERATOR ON BUS WHEN RESET. NR 1 ENGINE RUN-UP CARRIED OUT AND TAKEOFF POWER WAS COMPLETED,
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