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 2026FA0000477Generator · failedIN V1 IF PRESENT LOSS OF ALL GENERATOR WAS PERFORMED EMERGENCY CHECK LIST WITH UNSATISFACTORY STATE. COME BACK AIRPORT OF BOGOTÁ. ACCOMPLISHED CHECKOUT ANALYSIS OF ELECTRICAL GENERATOR SYSTEM IAW 727 AMM 24-20-00 / 101-113. FOREIGN REGISTRATION: HK-5216SDR FXGA07312024001Hose · leakingON DESCENT "A" SYSTEM HYDRAULIC QUANTITY FLUID STARTED DECREASING. FOUND LEAK FROM HOSE FITTING ON #2 SPOILER ACTUATOR. REPLACED ORING ON FITTINGSDR VGCA20230323001Gearbox · leaking#2 ENGINE PRECAUTIONARY SHUTDOWN DUE TO LOW OIL PRESSURE. FOUND LOOSE FASTENER ON MAIN ACCESORY GEARBOX CAUSING OIL LOSS.SDR FXGA2022121400512Battery · dischargedCREW RECEIVED A LOWER AFT CARGO FIRE WARNING AT FL360 ON ARRIVAL INTO EFD. CREW IMMEDIATELY INITIATED THE EMERGENCY PROCEDURE AND BEGAN AN EMERGENCY DECENT AND DIVERTED TO CWF, WHICH WAS JUST SOUTH OF POSITION. THE FIRE CREW SWEPT AIRCRAFT UPON LANDING AND NO SDR FXGA20211129001Duct · crackedON CLIMB APPROXIMATELY 1500' #3 ENGINE HAD FIRE WARNING. ACCOMPLISHED CHECKLIST. LIGHT EXTINGUISHED DID NOT FIRE BOTTLE. RETURNED TO KFLL. ON VISUAL INSPECTION OF ENGINE IT WAS FOUND THAT THE BLEED AIR DUCT HAD RUPTURED/CRACKED.SDR Y2PA2020102920032Engine · fodDISCREPANCY: CREW REPORTED THAT AFTER DEPARTURE FROM KLRD AND CLIMBING THROUGH 10000 FEET, THE NR 3 ENGINE FAILED WITH ASSOCIATED VIBRATIONS. THEY DECLARED AN EMERGENCY AND PERFORMED THE ENGINE FIRE, SEVERE DAMAGE OR SEPARATION CHECKLIST AND LANDED AT THE DEPSDR VGCA20200923001Engine · fodAFTER TAKEOFF DURING CLIMB, NR 3 STARTED VIBRATING EXCESSIVELY. SHUT DOWN ENGINE AND RETURNED TO AIRPORT. UPON INSPECTION OF ENGINE, FOUND EVIDENCE OF FOD DAMAGE TO THE FAN BLADES. REMOVED ENGINE FROM SERVICE.SDR FXGA201903081925Beam · corrodedCORROSION ON RT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM. TO REPAIR A CORRODED HORIZONTAL STABILIZER TRAILING EDGE BEAM. REMOVE AND REPLACE CORRODED BEAM WITH NEW PER SRM 51-30-2 FASTENER REMOVAL AND INSTALLATION.SDR FXGA201903081924Beam · corrodedCORROSION ON RT HORIZONTAL STABILIZER LOWER TRAILING EDGE BEAM. TO REPAIR A CORRODED HORIZONTAL STABILIZER TRAILING EDGE BEAM. CUT DAMAGED BEAM AT STA 88.29 AND SPLICE IN NEW OUTBOARD SECTION PER SRM 55-10-6 FIGURE 1 HORIZONTAL STABILIZER T.E. BEAM REPAIR.SDR FXGA201903081923Beam · corrodedCORROSION ON LT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM. TO REPAIR A CORRODED HORIZONTAL STABILIZER TRAILING EDGE BEAM. CUT DAMAGED BEAM AT STA 82.5 AND SPLICE IN NEW OUTBOARD SECTION PER SRM 55-10-6 FIGURE 1 HORIZONTAL STABILIZER T.E. BEAM REPAIR.SDR FXGA201903081922Beam · corrodedCORROSION ON LT HORIZONTAL STABILIZER LOWER TRAILING EDGE BEAM. TO REPAIR A CORRODED HORIZONTAL STABILIZER TRAILING EDGE BEAM. CUT DAMAGED BEAM AT STA 78.29 AND SPLICE IN NEW OUTBOARD SECTION PER SRM 55-10-6 FIGURE 1 HORIZONTAL STABILIZER T.E. BEAM REPAIR.SDR Y2PA2018092200029Bearing · failedCREW REPORTED – EXPERIENCED SEVERAL ABNORMAL AIRCRAFT VIBRATIONS. DISCUSSED WITH CREW. DECLARED AN EMERGENCY. LANDED AT NEAREST SUITABLE AIRPORT USING NORMAL PROCEDURES. USA JET MAINTENANCE WAS SENT TO KAFW TO TROUBLESHOOT PROBLEM. UPON INSPECTION OF THE #SDR AALA20170109030Engine · smokeAFTER GATE ARRIVAL, MAINTENANCE PULLED FIRE HANDLE DUE TO SMOKE AND FUEL FROM THE LT ENGINE. AIRCRAFT WAS GROUNDED. ACCOMPLISHED VISUAL CHECKS. STARTED AND SHUTDOWN ENGINE TWICE. RESET ENGINE GENERATOR. ALL PARAMETERS NORMAL. OPS CHECKED GOOD.SDR I5PA2016022642501Unknown · malfunctionedSHORTLY AFTER TAKEOFF THE CREW CALLED IN THE COMPANY RADIO THAT THEY WERE NOT GETTING A GREEN LIGHT FOR THE NOSE GEAR & THAT THE RED UNSAFE LIGHT STAYED ILLUMINATED. THEY CYCLED THE GEARS & STILL DID NOT GET THE RED NOSE GEAR LIGHT TO EXTINGUISH & THE GREEN LSDR FXGA20160226001Controller · failedAIRCRAFT DEPRESSURIZED IN THE MIDDLE OF A PARABOLA. DESCENT WAS INITIATED AT FIRST INDICATION OF DEPRESSURIZATION. MAXIMUM ALTITUDE REACHED WAS FLIGHT LEVEL 310. FOUND THAT THE CABIN PRESS CONTROLLER HAD FAILED.SDR CA160226003Pressure Switch · shorted(CAN) IN CRUISE, NR 1 ENGINE, START VALVE OPEN, CAUTION LIGHT ILLUMINATE. CREW FOLLOW QRH PROCEDURE AND SHUTDOWN THE AFFECTED ENGINE. CREW DECLARED AN EMERGENCY AND LANDED SAFELY. MAINTENANCE FOUND THAT IT WAS ONLY AN INDICATION PROBLEM. THE STARTER VALVE PSDR I5PA2015102631902Line · unknownNUMBER 3 ENG EXPERIENCED OIL LOSS. OIL PRESS AT APPROX 10 PSI ON IDLE PRIOR TO SHUT DOWN. DUE TO WEATHER ACFT DIVERTED TO ALTERNATE, FLIGHT ARRIVED SAFELY. TROUBLESHOOTING IN PROGRESS. ENG HAD APPROX 1 GAL IN THE SYS & SERVICED APPROX 3 GAL. FOUND OIL SUPSDR FXGA20151026001Wire Harness · brokenDURING CRUISE FLIGHT NR 3 ENG FIRE INDICATION. PROCEDURE & CHECKLIST INITIATED. BOTH ENG FIRE BOTTLE DEPLOYED. FIRE INDICATION REMAINED ON. ALL ENG PARAMETERS NORMAL EXCEPT ENG OIL TEMP AT RED LINE. ENG FIRE INDICATION REMAINED ON UP TO SECURING AIRPLANE SDR CA150729007Indicator · failed(CAN) DURING APPROACH THE CREW SELECTED FLAPS 1 POSITION. THE L/E FLAPS LOWERED TO THE EXTEND POSITION, BUT THE TRAILING FLAPS DIDN`T MOVE. THE FLAPS WERE CYCLED SEVERAL TIMES WITH NO MOVEMENT. THE CREW THEN SELECTED ALTERNATE EXTENSION OF THE FLAPS WITH THE SSDR PCSA2015072701Warning Light · illuminatedNR 3 ENGINE LOW OIL PRESSURE LIGHT CAME ON & STAYED ON DURING TAKEOFF. REJECTED TAKEOFF AT 100 KNOTS. MODERATE BRAKING. NR 3 ENGINE EGT RUNS HOT AT TAKEOFF POWER, REDUCED POWER A LITTLE BEFORE OIL LIGHT CAME ON. REPLACED THE MAIN OIL FILTER & REPLACED THE SDR F7JR2015FA0000417Turbine Wheel · crackedT-3 DISK REMOVED FROM ENGINE. THE T-3 DISK EXPERIENCED A FATIGUE CRACK AND MATERIAL FAILURE. THE CRACK APPEARS TO HAVE ORIGINATED ON THE FRONT OF THE DISK ABOUT HALF WTH WAY UP THE FIR TREE BLADE MOUNT ANEE AT THE ADJACENT BLADE MOUNT. WHEN THE MATERIAL FSDR CA150126008Fitting · broken(CAN) DURING INSTALLATION AND RIGGING OF NR 5 SLAT ACTUATOR FAIRING, MAINTENANCE NOTED EXCESSIVE PLAY ON ACTUATOR ATTACHMENT. UPON INSPECTION IT WAS FOUND THAT OUTBOARD ATTACHMENT LUG WAS BROKEN. BUSHINGN P/N NAS72-9E006 WAS NOT FOUND INSTALLED IN THE FITTING SDR CA140923009Circuit Breaker · failed(CAN) DURING TAXI, THE FLT CREW REPORTED THEY HAD NO HYDRAULIC PRESSURE FROM THE NR 1 HYDRAULIC B PUMP AND RETURNED TO THE RAMP. DURING MAINTENANCE TROUBLESHOOTING, THEY FOUND A SYS 40 AMP CIRCUIT BREAKER TRIPPED WITH SIGNS OF BEING BURNED. THE FAULTY BREAKESDR CA140619002Hose · failed(CAN) WHILE IN FLIGHT, THE FLIGHT CREW HAD NOTICED THE HYDRAULIC FLUID LEVEL DECREASING. "A" SYSTEM FLUID LEVEL WAS EXHAUSTED, AND THE AIRCRAFT CONTINUED ENROUTE, ON THE "B" SYSTEM IAW THE FLIGHT MANUAL ABNORMAL PROCEDURES. THE LOSS OF "A" SYSTEM AFFECTS THE BSDR I5PA201405010001Gearbox · unknownAT APPROXIMATELY 0730Z, THE CREW EXPERIENCED NR 3 ENG LOSS OF OIL QTY FOLLOWED BY LOW OIL PRESS, HIGH ENG TEMP AT FL 330. THEY DECLARED AN EMERGENCY AT 0738Z & AIR RETURNED BACK TO HNL STATION SAFELY AT 0908Z. TROUBLESHOOTING IN PROGRESS. R & R NR 3 ENG GEASDR I5PA201405010002Gearbox · leakingAT APPROX 0730Z, THE CREW EXPERIENCED NR 3 ENG LOSS OF OIL QTY, FOLLOWED BY LOW OIL
PRESS, HIGH ENG EMP AT FL 330. DECLARED AN EMER AT 0738Z & AIR RETURNED BACK SAFELY AT 0908Z. TROUBLESHOOTING IN PROGRESS. R & R NR 3 ENG GEARBOX IAW AMM 72-63-00. INSPECTESDR CA140408002Indicator · failed(CAN) T/E FLAP SYS STALLING AND LOCKOUT TROUBLESHOOTING CARRIED OUT. T/E FLAP ASSEMBLIES INCLUDING TRACKS AND ROLLERS INSPECTED FOR DAMAGE, NO FAULTS FOUND. FLAP POSITION INDICATOR REPLACED AND ACFT RELEASED PENDING SATISFACTORY TEST FLIGHT. TEST FLIGHT CARSDR SPUY201403310033Skin · corrodedNR 3 ENGINE, LT UPPER COWLING SKIN SHOWS CORROSION FROM NAC STA. 185.20-194.8.SDR SPUY201403310037Latch · crackedNR 1 ENGINE, UPPER COWLING FITTING LATCH ATTACHMENT CRACKED ONE INCH.SDR SPUY201403310038Former · corrodedNR 1 ENGINE, THRUST REVERSE FWD SIDE EXTERIOR FORMER CORRODED AT STA 96.25 AT 5 O´CLOCK POSITION.SDR CA140311010Heater · shorted(CAN) CAPTAIN`S MAIN WINDSCREEN WINDOW HEAT GOES DIRECTLY TO OVERHEAT WHEN SWITCH SELECTED. DURING TROUBLESHOOTING IT WAS FOUND THAT THE CONTROL BOX HAS AN INTERNAL SHORT CAUSING A VERY LARGE CURRENT DRAW POPPING THE MAIN POWER BREAKER. CONTROLLER REPLACED. MFSDR CA140225014Proximity Switch · failed(CAN) AFTER TAKEOFF, DURING CLIMB, THE FLAPS HAD BEEN SELECTED UP IAW NORMAL OPERATING PROCEDURE. THE FLAP POSITION INDICATION, INDICATED THAT THE LT INBD FLAP WAS IN TRANSIT AND NOT FULLY RETRACTED. THE ACFT RETURNED TO THE RAMP AFTER EXECUTING A NORMAL LANSDR CA140224017Oil System · bypassing(CAN) WITH POWER LEVERS ADVANCED FOR TAKEOFF, AN INDICATION OF AN IMPENDING "OIL FILTER BYPASS" LIGHT ON NR 1 ENGINE HAD OCCURRED. POWER LEVERS RETARDED AND ACFT RETURNED TO THE RAMP. THE NR 1 ENGINE OIL FILTER WAS REMOVED AND INSPECTED. FILTER INSPECTION ISDR CA140130013Hose · failed(CAN) DURING TAKEOFF CREW REPORTED LOSS OF HYDRAULIC SYSTEM "A" AND THE LANDING GEAR WOULD NOT RETRACT. OVERWEIGHT LANDING PERFORMED. ON THE GROUND MAINTENANCE DISCOVERED HYD LEAK FROM RT THRUST REVERSER FLEX LINE. THE HOSE ASSY WAS MFG JAN 1975. HYDRAULICSDR CA131017005Tube · fractured(CAN) DURING CLIMB OUT APPROXIMATELY 10 MINUTES THE FLIGHT CREW REPORTED THE NR 2 ENGINE SURGE WITH ASSOCIATED VIBRATION AND HIGH TEMPERATURE. THE ENGINE WAS SHUTDOWN AND AN EMERGENCY WAS DECLARED. THE NR 2 VORTEX DISSIPATOR TUBE FRACTURED AND WAS NOT RECOVESDR CA131004006Sliding Window · cracked(CAN) THE CAPTAIN`S SLIDING WINDOW, OUTER PANE CRACKED WHILE IN FLIGHT. PILOTS FOLLOWED THE APPLICABLE AFM PROCEEDURES. TT SINCE O/H 1,219.5 HRS AND 845 CYCLES SINCE O/H. THE WINDOW SHOWED NO SIGNS OF DELAMINATION, OR WATER/MOISTURE INGRESS. ASIDE FROM THE SDR CA131007024Engine · flamed out(CAN) AT TOP OF DECENT, THE NR 2 ENGINE FLAMED OUT. ENGINE FLAMEOUT CHECKLIST WAS COMPLIED WITH AND THE ENGINE WAS RESTARTED. THE NR 2 ENGINE FUEL FILTER WAS INSPECTED, AND REPLACED. THE FUEL S/O VALVE WAS FUNCTION CHECKED WITH NO FAULTS FOUND. ENGINE RUNS SDR CA130803010Pressure Switch · malfunctioned(CAN) IN CRUISE, CREW NOTICED THE NR 3 ENGINE, LOW OIL PRESSURE/FILTER BYPASS, LIGHT ILLUMINATE. THE LOW OIL PRESSURE WARNING SYS WAS DEFERRED AND THE ACFT CONTINUED TO FINAL DESTINATION. MAINTENANCE REPLACED THE LOW OIL PRESSURE SWITCH AND THE ACFT RETURNEDSDR CA130726007Tire · failed(CAN) ACFT SUSTAINED A MAIN WHEEL TIRE FAILURE NR 1 POSITION. THE TREAD AND CHORD HAD SEPARATED FROM THE TIRE CASING. THE ACFT IS CERTIFIED AND OPERATED FROM GRAVEL RUNWAY SURFACES. THE TIRE IS CONSIDERED AS SCRAP. THE ACFT WAS INSPECTED IAW MM AND RESULTESDR CA130719007Clamp · broken(CAN) SHORTLY AFTER TAKEOFF, THE CREW RECEIVED A START VALVE OPEN CAUTION LIGHT FOR ENGINE NR 1. THE CREW FOLLOWED THEIR SOPS AND SHUTDOWN THE NR 1 ENGINE. THE CREW THEN HELD A CIRCUIT FOR APPROXIMATELY 1 HR TO BURN OFF FUEL SO THEY COULD PERFORM A NON-OVERWSDR CA130905014Tube · cracked(CAN) THE CREW REPORTED LOW ENGINE PRESSURE RATIO ON ENGINE NR 2 AND SUBSEQUENTLY REJECTED TAKEOFF, RTO, DUE TO AN EPR FAILURE. MAINTENANCE TROUBLESHOT THE SYS VIA LEAK TESTS ON THE EPR SYSTEM AND, THROUGH THE PROCESS OF ELIMINATION, DETERMINED THE CAUSE WAS SDR CA130702001Power Lever · obstructed(CAN) UNABLE TO REACH TAKEOFF EPR ON NR 2 ENGINE DURING TRIM RUNS AFTER FCU REPLACEMENT DIFFERENT READING WERE OBSERVED WITH COWLING OPEN VERSUS COWLING CLOSED. AFTER TROUBLESHOOTING FCU POWER LEVER FOUND INTERFERING WITH COWLING.SDR CA130325004Pcu · separated(CAN) DURING ROUTINE MAINTENANCE, WITH "B" PUMPS ON AND HYDRAULIC INTERCONNECT "OPEN" TO LOWER THE FLAPS, WHEN NORMAL OPERATING PRESSURE WAS REACHED IMMEDIATE LOSS OF HYDRAULIC PRESSURE WAS NOTICED ALONG WITH MASSIVE AMOUNTS OF HYDRAULIC FLUID GUSHING OUT OF TSDR CA130315005Circuit Breaker · burned(CAN) WHILE PERFORMING THE PREFLIGHT INSPECTION THE WINDOW HEAT FAILED. AFTER TROUBLESHOOTING IT WAS FOUND THAT THE CIRCUIT BREAKER FOR THE WINDOW HEAT SUPPLY C239 HAD BURNED. THIS BURNING HAD ALSO CAUSED DAMAGE TO THE CIRCUIT BREAKER IMMEDIATELY ON TOP OF TSDR 7AHR20130129011Rib · wornRT ENGINE COWL HAS AREA OF DAMAGE, AREA NR 7 RIB. REMOVED DAMAGE RIB ANGLE IAW SRM 51-40-3. FABRICATED NEW REPAIR ANGLE IAW SRM 51-40-3. INSTALLED NEW REPAIR ANGLE TO NR 7 RIB IAW SRM 51-40-3.SDR 7AHR20130129012Rib · wornRT ENGINE COWL HAS AN AREA OF DAMAGE AT NR 10 RIB. AREA OF DAMAGE IS FOUND TO BE OUT OF LIMITS IAW SRM 54-10-1. REMOVED DAMAGED PARTS (ANGLES). FABRICATED NEW REPAIR ANGLES IAW SRM 51-40-3. INSTALLED REPAIR ANGLES IAW SRM 51-40-3.SDR 7AHR20130129013Rib · wornRT ENGINE COWL HAS AN AREA OF DAMAGE AT NR 11 RIB. AREA OF DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 54-10-1. REMOVED DAMAGE AND WORN PARTS (ANGLE) IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW REPAIR ANGLE IAW 200 51-40-3.SDR 7AHR20130129014Skin · wornRT ENGINE COWL WORN. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW REPAIR DOUBLER ON THE RT ENGINE COWL IAW SRM 51-40-3.SDR R5KB2013031150507Skin · corrodedSKIN CORRODED UNDER EDGE OF DOUBLER AT STA 950E, STR 27R.SDR CA121113005Pin · failed(CAN) A DEFICIENCY WAS DETECTED ON THE GROUND IN THE NR 7 FLAP UNIVERSAL JOINT, BOLT/PIN, PN 65-76606-01. THE FLAP WOULD NOT FULLY RETRACT PAST THE NR 1 POSITION. THE RETENTION FEATURE OF THE LOCKING NUT WAS LOST AT THE THREAD TO PIN SHANK AREA SHEARED AT THE
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