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 CA090514001Window · cracked(CAN) DURING CRUISE AT 35,000, THE NR 4 WINDOW CRACKED, CREW DESCENDED TO 14,000 AND CONTINUED THE FLIGHT. WINDOW WAS REPLACED AND ACFT RETURNED TO SERVICE.SDR PCSA2009051801Sensor · out of positionNR1 STRUT OVERHEAT LIGHT ILLUMINATED IN FLIGHT. SHUTDOWN NR1 ENGINE AND RETURNED TO DEPARTURE. WINDMILLING 15 MINUTES, OIL PRESSURE WITHIN LIMITS. MX FOUND NR 1 STRUT SENSING ELEMENT OUT OF POSITION. THE ELEMENT WAS REPOSITIONED AND A PNEUMATIC LEAK CHECK WAS SDR CA090323005Turbine · failed(CAN) AFTER TAKEOFF, THE CREW OBSERVED A SUDDEN LOSS OF POWER ON NR 2 ENGINE COINCIDENT WITH AN UNUSUAL VIBRATION AND NOISE. THE CREW CARRIED OUT AN INFLIGHT SHUTDOWN OF NR 2 ENGINE. THE ACFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT FURTHER DIFFICULTYSDR I5PA030809Transceiver · malfunctionedAIRCRAFT, AIR RETURNED DUE TO NR 1 AND NR 2 HF'S WOULD NOT TRANSMIT OR RECEIVE. CLEANED AND RESEATED BOTH TRANSCEIVERS, OPS CHECK WITH SFO NORMAL. OK FOR SERVICE NO FURTHER PROBLEMSSDR I5PA0308091Actuator · defectiveAIRCRAFT, AIR RETURN DUE TO NR 3 L/E SLAT REMAINED EXTENDED AND NR 3 SLAT REMAINED IN TRANSIT DURING FLAP RETRACTION. REMOVED AND REPLACED NR 3 L/E SLAT ACTUATOR THEN CLEANED AND RESEATED NR 2 L/E SLAT SWITCH. OPERATIONAL CHECK OK.SDR CA090526008Actuator · corroded(CAN) UNIT REMOVED FOR SCHEDULED OVERHAUL. UPON DISASSEMBLY, INTERNAL COMPONENTS BADLY CORRODED AND CONTAMINATED WITH WATER. UNIT SCRAPPED. THERE WERE NO INFLIGHT DEFECTS REPORTED.SDR CA090227002Landing Gear · iced(CAN) DEPARTING, THE CREW OBSERVED A FAIL TO RETRACT INDICATION ON THE NLG. THE ACFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT FURTHER PROBLEM. MX WAS UNABLE TO CONFIRM THE CAUSE FOR THE MALFUNCTION ALTHOUGH THE CREW REPORTED ENCOUNTERING SLUSH WHILE SDR CA090219009Deflector · damaged(CAN) NOSE LANDING GEAR, GRAVEL DEFLECTOR, PLATE, RETAINER AND FIBERGLASS SKIN WITH WEARS, GOUGES, CORROSION AND NICKS. GRAVEL DEFLECTOR COMPONENTS WITH LUGS AND BORES CORRODED. ASSY DEFLECTOR ASSY PN: 65-76611-26 SN: 9994 MODIFICATION INCORPORATED 39-1067.SDR NWAA09449856Unknown · leakingDURING ROTATION AND CLIMB ENGINE NR1 FUEL FLOW WAS ERRATIC AND EPR DROPPED ABOUT 10 PERCENT. ADVANCED THROTTLE TO MATCH ENGINE NR2 BUT EPR DROPPED AGAIN TO 1.6 AND WOULD NOT RESPOND TO HIGHER THROTTLE SETTINGS. FLIGHT CREW RETURNED ACFT TO DEPARTURE AIRPORT.SDR CA090204008Landing Gear · malfunctionedDEPARTING YFB FOR YOW ON JAN 31, 2009, THE CREW OBSERVED A NOSE LANDING GEAR FAIL TO LOCK CONDITION AFTER GEAR WAS SELECTED UP. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE SERVICED THE NOSE GEAR AND THE AIRCRAFTSDR CA090106006Hydraulic System · malfunctioned(CAN) WHILE ON THE TAXI FROM MX HANGAR TO THE TERMINAL, THE TAXI CREW APPLIED THE BRAKES WITH NO EFFECT. THE ACFT WAS SHUT DOWN. THE AMM WAS CONSULTED, AND REMOVED A HYDRAULIC CASE DRAIN FILTER, AND FOUND THE FILTER TO BE COMPLETED BLOCKED WITH ICE. IT IS PSDR CA081217001Compressor · fod(CAN) AIRCRAFT WAS ON TAKEOFF ROLL WHEN THE PILOTS HEARD A LOUD BANG FROM ENGINE NR 2 & EXPERIENCED A YAW TO THE RIGHT AS THEY APPROACHED 110 KNOTS. THE PILOTS THROTTLED BACK, ABORTED THE TAKEOFF, TAXIED BACK TO THE RAMP AND SHUTDOWN THE ENGINES. PASSENGERSSDR CA081210005Cylinder · worn(CAN) RT MLG LOST FLUID. DURING ATTEMPTED SEAL CHANGE, THE INNER CYLINDER OF THE GEAR HAD A 6" BY 2" PIECE OF CHROME MISSING FROM THE INNER CYLINDER.SDR PCSA2008120301Blade · brokenAMERIJET FLIGHT SXM - SJU NUMBER ONE ENGINE VIBRATION FOLLOWED BY HIGH FUEL FLOW. PERFORMED A PRECAUTIONARY SHUTDOWN. MAINTENANCE DISCOVERED A BROKEN C2 BLADE AND COMPRESSOR DAMAGE.SDR PCSA2008103101Garlock Seal · leakingENGINE 2 OIL TEMPERATURE RED BAND INDICATION, OIL QUANTITY NORMAL 3 GALLONS, ENGINE INSTRUMENT PARAMETERS NORMAL. ENGINE SHUT DOWN PER ALTERNATE AND ABNORMAL PROCEDURES. WINDMILL AFTER SHUTDOWN 20 MINUTES, OIL PRESSURE 15 PSI. DIVERTED TO SDQ AND PERFORMED SDR CA081030003Transmitter · failed(CAN) DURING FINAL APPROACH, WHEN THE PILOTS SELECTED FLAPS 25, THE FLAPS STOPPED SLIGHTLY PAST FLAPS 15. THE PILOTS SELECTED FLAPS UP AND OVERSHOT THE APPROACH. THE FLAPS RETRACTED OK. ON THE NEXT APPROACH, THE FLAPS OPERATED NORMALLY. MX INSPECTED AND OPERATSDR CA081016008Switch · inoperative(CAN) ON CLIMB OUT, NR 3 ENGINE THRUST REVERSER OPERATING LIGHT ILLUMINATED THROUGH 5000 FT. THE ACFT RETURNED TO THE AIRPORT. THE NR3 ENG THRUST REVERSER WAS DEACTIVATED AND MEL APPLIED. UPON REACHING THE DESTINATION, THE NR3 ENGINE THRUST REVERSER SWITCH WASSDR CA081002004Battery · overheated(CAN) PASSENGERS WERE ON THE ACFT, ACFT WAS ON EXTERNAL GROUND POWER AT THE TIME. WHEN THE PILOTS WENT TO START THE APU, THEY NOTICED THE START WAS NOT NORMAL, AND THE APU ALSO DID NOT START. APU OVERSPEED CAUTION LIGHT ILLUMINATED. CAPTAIN WENT TO THE E&E SDR CA080905003Controller · malfunctioned(CAN) AT FL300, TOP OF DESCENT, AS THRUST REDUCTION COMMENCED, LARGE BANG WAS EXPERIENCED BY THE FLIGHT CREW WITH FLUCTUATIONS IN NR 2 ENGINE PARAMETERS. ENGINE WAS IDLED FOR THE REMAINDER OF THE FLIGHT AND SHUT DOWN UPON LANDING. MX PERSONNEL CARRIED OUT TROSDR CA080829002Contactor · failed(CAN) AFTER LIFTOFF, SEVERAL FAILURES OCCURED. ANTISKID INOP, F/O PITOT INOP, NR2 EPR GUAGE INOP, NR2 AFT FUEL PUMP INOP, PINNED ASSOCIATED LIGHTS TO TRANSFER BUS PROBLEMS. LANDING BOTH 115V AND 28V AC TRANSFER BUS INOP. NR2 TRANSFER BUS CONTACTOR WAS FOUND TOSDR DHLA200800082Compressor · stalledENG FAIL LIGHT/AUTO PACK TRIP LIGHT FAILED AS THRUST APPLIED FOR T/O. RAN APPROPRIATE PROCEDURE IN AOM. CONTACTED MX AND DISPATCH. ALL INDICATIONS NORMAL AFTER PROCEDURE, APPARENT COMPRESSOR STALL AS THRUST APPLIED. NOTE, CREW REPORTED HEAVY CROSSWINDS DURSDR DHL2008F00000Pin · damagedSMALL DAMAGE ON NR (6) L/E SLAT AT IB GUIDE PIN EXISTING DOUBLER. DAMAGE WAS BLENDED SMOOTH LESS THAN 1 INCH X .100 MATERIAL LOSS, WORK ACCOMPLISHED IAW SRM 57-50-01. (K)SDR 2008003Engine · inoperativeON TAKEOFF, CREW EXPERIENCED A SLIGHT VIBRATION ON NR 3 ENGINE, VERIFIED ALL PARAMETERS NORMAL, CONTINUED WITH TAKEOFF CREW THEN NOTICED A LOSS OF OIL ON NR 3 ENGINE. SHUTDOWN ENGINE AND RETURN TO DEPARTURE. ON INSPECTION, FOUND BLADE DAMAGE, 2ND STAGE FAN BLSDR NWAA082079880Manifold · leakingDURING TAKEOFF ENGINE NR 2 EPR ROLLED BACK FROM 2.17 TO 2.10. FLIGHT CREW ADVANCED ENG NR 2 THROTTLE TO STOPS BUT EPR REMAINED AT 2.10. AFTER TAKEOFF ENGINE NR 2 APPEARED TO FUNCTION NORMAL REMAINDER OF FLIGHT. AT DESTINATION MAINTENANCE NOTICED ENG NR 2 EXSDR CA080623001Rod End · worn(CAN) MINOR BUT PERSISTENT VIBRATION COULD BE FELT IN THE STEERING TILLER DURING TAXI, PARTICULARLY AT HIGHER SPEEDS.SDR CA080423004Windscreen · burned(CAN) AFTER COCKPIT SETUP SMOKE AND FLAME WAS OBSERVED BY THE FLIGHT CREW FROM THE TOP LT CORNER OF THE R1 WINDOW. WHEN THE R1 WINDOW HEAT WAS SELECTED OFF THE FLAME AND SMOKE CEASED. THE R1 WINDSCREEN WINDOW HEAT SYS WAS DEFERRED BY MAINT. UPON ARRIVAL AT THSDR 2008040101Warning System · malfunctionedAMERIJET FLIGHT 8110 FROM TSSJ TO KMIA - MAIN CARGO COMPARTMENT SMOKE WARNING CAME ON IN CRUISE FLIGHT. VISUALLY CHECKED FALSE WARNING. ON ARRIVAL KMIA THE MAIN CARGO SMOKE DETECTION SYSTEM WAS OPERATIONALLY TESTED AND NO DEFECTS WERE FOUND.SDR CA080208006Nose Bullet · separated(CAN) FOLLOWING DEPARTURE, THE CREW REPORTED COMPRESSOR STALLING OF THE NR 1 ENG AT CLIMB PWR. THE ENGINE PWR WAS REDUCED AND COMPRESSOR STALLS STOPPED. THE AC RETURNED TO DEPARTURE WITH NO FURTHER INCIDENT. INSP OF THE ENGINE IDENTIFIED THAT THE NR 1 ENGINE NSDR NWAA074319860Engine · failedDURING TAKEOFF ROLL FLIGHT CREW HEARD A LOUD "POP" AND NOTICED N1 ROLLBACK. FLIGHT CREW ABORTED THE TAKEOFF AT 110 KNOTS. MAINTENANCE FOUND METAL IN THE TAILPIPE AND REPLACED ENGINE NR 2.SDR DHLA200700091Clamp · looseNR 1 ENG STRUT OVERHEAT DURING CRUISE. PERFORMED ABNORMALS PROCEDURE RESULTED IN IN-FLIGHT ENG SHUTDOWN ALL CHECK LISTS, PROCEDURES DONE. T/S FOUND CLAMP ON PRESSURE MODULATING VALVE LEAKING ON PRECOOLER SIDE TIGHTENED CLAMP IAW MM 36-00-1 MM 36-12-42, RAN ESDR DHLA200700080Switch · malfunctionedAPPROXIMATLY 35 MIN, AFTER TAKEOFF NR 3 ENG OIL PRESSURE/BYPASS LIGHT ILLUMINATED. ABNORMAL PROCEDURE ACCOMPLISHED, DETERMINED THAT BYPASS MODE WAS RESPONSIBLE AND ENGINE WAS SHUT DOWN AT 0835Z. PRESSURE AND QUANTITY WAS NORMAL PRIOR TO SHUT DOWN. WINDMILL SDR DHLA200700066Engine · malfunctionedFLT 594 IN CRUISE FL 320 CLEAR CONDITIONS NR 2 ENGINE PARAMETERS STARTED TO FLUCTUATE ALONG WITH SEVERE VIBRATION, PERFORMED ABNORMAL PROCEDURE OBSERVED NR 2 OIL QTY GO TO ZERO AND PERFORMED ENG SHUTDOWN ABNORMAL PROCEDURE UPON LANDING OIL QTY RETURNED TO NORMSDR DHLA200070006Engine · malfunctionedFLT NR 594 IN CRUISE FL320, NR 2 ENGINE PARAMETERS STARTED TO FLUCTUATE ALONG WITH SEVERE VIBRATION, PERFORMED ABNORMAL PROCEDURE OBSERVED NR 2 OIL QTY GO TO ZERO AND PERFORMED ENG SHUTDOWN ABNORMAL, PROCEDURE UPON LANDING OIL QTY RETURNED TO NORMAL AFTER ENG SDR 1018200701Control Unit · malfunctionedAMERIJET FLIGHT 843 DURING TAXI LOWER CARGO FIRE RED LIGHT ILLUMINATED AND REMAINS ILLUMINATED. THE AIRCRAFT RETURNED TO BLOCKS, THE CHANNEL A LOWER CARGO SMOKE DETECTOR CONTROL UNIT WAS REPLACED, AND THE AIRCRAFT RETURNED TO SERVICE.SDR 200700026Wire · chafedTRAILING EDGE FLAPS ASYMMETRY LOCKOUT BETWEEN ZERO AND ONE DEGREE. THERE IS A SPLIT IN T/E FLAP INDICATION, LT T/E FLAPS INDICATE ONE DEGREE AND RT T/E FLAPS INDICATE ZERO. FLIGHT CREW EXPERIENCED AN UNEVENTFUL LANDING AND NO UNCOMMANDED ROLL. MAINTENANCE DSDR CA070911003Valve · malfunctioned(CAN) APPROXIMATELY 25 MINUTES AFTER DEPARTING, THE CREW OBSERVED THE NR 1 ENGINE OIL TEMPERATURE CLIMBING THROUGH THE YELLOW BAND. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT RETURNED TO POINT OF DEPARTURE. MAINTENANCE REPLACED THE NR 1 FUEL HEAT VALVE AND CONDUSDR CA070911012Stud · dislodged(CAN) DURING CRUISE, THE NR 2 OIL QUANTITY SLOWLY DECREASED TO ZERO. WHEN THE OIL QUANTITY WENT BELOW THE GREEN ARC THE FLIGHT CREW SHUTDOWN THE ENGINE USING THE APPROPRIATE CHECKLIST AND AN EMERGENCY WAS DECLARED INTO AIRFIELD. THE AIRCRAFT LANDED WITHOUT FURSDR SROM200700012Trunnion · wornWEAR DAMAGE, LT MLG FUSELAGE TO TRUNNION SUPPORT BEAM ATTACH FITTING. BLEND REPAIRED IAW MFG, FORM 8100-9, MESSAGE NR 1-515849678-6, DATED AUGUST 23, 2007.SDR SROM200700008Skin · dentedNR247- DENT FOUND STA 900 LT BETWEEN STRINGERS 17 AND 18. REPAIRED IAW MFG SRM 53-30-3, PAGES 253-320 AND 51-30-3, PAGE 7 AND 51-30-02.SDR SROM200700023Nut Plate · strippedNR122-LT ELEVATOR TRIM TAB IB HINGE FITTING MISSING BOLT. NEW ELEVATOR INSTALLED 12/06/06, 982 TT, 717 TC. (2) OUT OF (4) HINGE ATTACH FITTING NUTPLATES STRIPPED FROM THE FACTORY. REPLACED NUTPLATES IAW SRM 51-30-2, FIGURES 3 AND 7.SDR SROM200700006Frame · crackedNR63-CRACK ON BODY FRAME INNER CHORD BS616 RT SIDE AT STUB BEAM LOWER CHORD ATTACH (ABOVE WING BOX BL64R). DAMAGE OF BODY FRAME INNER CHORD STA 616 RT SIDE AT STUB BEAM LOWER CHORD ATTACH REMOVED IAW MFG SB 737-53-1182R1. REPAIR ANGLE INSTALLED IAW MFG SB 737-SDR KNNA200700040Skin · crackedAFT CARGO DOOR/CRACKED SKIN NEAR OF LATCH HANDLE, ACO NR 0753101 PROVIDE INSTRUCTIONS ON REPAIRING CRACK IN AFT CARGO DOOR SKIN NEAR HANDLE, SRM 52-30-2 FIG 3.SDR NWAA072509875Shaft · shearedDURING CRUISE FLIGHT ENGINE NR 2 FLAMED OUT. FLIGHT CREW SECURED ENGINE NR 2 AND LANDED AT DESTINATION. MAINTENANCE FOUND THE FUEL PUMP SHAFT SHEARED, REPLACED FUEL CONTROL UNIT AND FUEL PUMP.SDR KNNA200700037Skin · crackedSKIN IS CRACKED AT THE LOWER FWD CORNER OF THE L-2 DOOR CUT OUT. ACO NR 075397 REV 0 PROVIDES INSTRUCTIONS ON REPAIR OF L-2 DOOR CRACK SRM 53-30-3 FIGURE 46.SDR 706200701Engine · damagedFLIGHT 743 DEPARTED, WHEN THE CREW REPORTED, DURING CLIMBOUT, THE NR 3 ENGINE STARTED TO VIBRATE ABOUT FL340, ENGINE INDICATIONS WERE ERRATIC, NR 3 FUEL QTY GAUGE SHOWED 1700 LBS. DIFFERENCE WITH NR 1 FUEL TANK, THEN NR 3 ENGINE FLAMED OUT. THE CREW ACCOMPLISHSDR SPAA0700093Power Supply · inoperativeAFT EXIT AND FLOOR PROXIMITY EMERGENCY LIGHTING DOES NOT ILLUMINATE WHEN TURNED ON. REPLACED CHARGER AND BATTERY PACK IAW AMM 33-51-81,SYSTEM OPS TEST NORMAL IAW AMM 33-51-11.SDR SPAA0700094Power Supply · inoperativeAFT EXIT AND FLOOR PROXIMITY EMERGENCY LIGHTING DOES NOT ILLUMINATE WHEN TURNED ON. REPLACED CHARGER AND BATTERY PACK IAW AMM 33-51-81,SYSTEM OPS TEST NORMAL IAW AMM 33-51-11.SDR SPAA0700095Power Supply · inoperativeAFT EXIT AND FLOOR PROXIMITY EMERGENCY LIGHTING DOES NOT ILLUMINATE WHEN TURNED ON. REPLACED CHARGER AND BATTERY PACK IAW AMM 33-51-81,SYSTEM OPS TEST NORMAL IAW AMM 33-51-11.SDR CA070531003Pitot System · obstructed(CAN) THE AIRCRAFT BEGAN THE TAKEOFF ROLL WHEN THE FLIGHT CREW NOTICED A LAG IN THE FIRST OFFICERS AIR SPEED INDICATION. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WITH NO ADDITIONAL PROBLEMS. UPON INSPECTION OF THE FIRST OFFICERS PITOT INSTSDR CA070518005Duct · ruptured(CAN) WHILE PERFORMING THE DAILY INSPECTION, MAINTENANCE PERSONNEL HEARD A LOUD BANG, WHICH WAS FOLLOWED BY A DROP IN APU DUCT PRESSURE TO 0 PSI. UPON INSPECTION, 2 BLEED AIR DUCTS WERE FOUND RUPTURED, FORWARD OF THE APU LOAD CONTROL VALVE THAT CONNECT TO THE
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