Pratt & Whitney JT8D-17

Service difficulty reports · 1,680

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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.

SDR C1HA200284002EngineShutdown #3 engine due to low oil quantity and pressure. Diverted - oil pressure went below 10psi on approach. Removed and replaced #3 engine.Sep 22, 2002 · N684CA · Boeing 7272S7 · Turbine Engine Oil SystemSDR AUS20021048Fitting · loose(AUS) NO2 ENGINE OIL QUANTITY INDICATION DROPPED FROM 7.6 LITRES (2GAL) TO 3.8 LITRES (1GAL) DURING APPROACH TO LAND. INVESTIGATION FOUND THAT THE AUXILIARY GEARBOX LP5 FITTING THREAD WAS DAMAGED AND LOOSE. PERSONNEL/MAINTENANCE ERROR.Sep 18, 2002 · Boeing 727281 · Turbine Engine Accessory DriveSDR ASAA0210185Skin · crackedDURING SCHEDULED SERVICE CHECK FOUND SKIN PANEL AT BODY STATION 539-540, STRINGER 17 CRACKED. REPAIRED CRACK PER SRM.Sep 15, 2002 · N740AS · Boeing 737290C · Fuselage Main, Plate/SkinSDR AUS20020985Clamp · broken(AUS) LH PRIMARY HEAT EXCHANGER SUPPLY LINE CLAMP BROKEN.Sep 5, 2002 · Boeing 727281 · Air Distribution SystemSDR TSAA0251181Strap · corrodedKEEL BEAM VERTICAL STRAP CORRODED AT BS 532. BLENDED AND FLAP PEENED REPAIR AREA, FABRICATED TWO FILLER STRAPS, INSTALLED FILLERS AND STRAP.Aug 19, 2002 · N807AL · Boeing 7372T4 · Fuselage Miscellaneous StructureSDR TSAA0251178Stringer · corrodedFOUND CORROSION ON BS 500 AT STRINGER 26R. CUT AND REMOVED DAMAGED PORTION OF FORMED SECTION. FABRICATED REPAIR ANGLES AND DOUBLER IAW SRM. REPAIR COMPLETED IAW SRM. AIRCRAFT RETURNED TO SERVICE.Aug 16, 2002 · N807AL · Boeing 7372T4 · Fuselage Main, Longeron/StringerSDR TSAA0253182Spar · crackedRIGHT WING FRONT SPAR CRACK AND CORRODED AT FSS124.79 AND FSS134.80. AIRCRAFT RETURNED TO SERVICE.Aug 16, 2002 · N802AL · Boeing 7372S5C · Wing SparSDR TSAA0251177Skin · crackedSKIN CRACK AT BS 380 BETWEEN STRINGER 28L AND 28R. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER, AIRCRAFT RETURNED TO SERVICE.Aug 15, 2002 · N807AL · Boeing 7372T4 · Fuselage Main, Plate/SkinSDR TSAA0251180Stringer · crackedCRACK LOCATED AT BS 767, S-14L. TRIMMED OUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND REPAIR ANGLES.Aug 15, 2002 · N807AL · Boeing 7372T4 · Fuselage Main, Longeron/StringerSDR CA020823003Housing · split(CAN) ON APPROACH CREW REPORTED COMPLETE LOSS OF HYD FLUID FROM 'A' SYS UPON SELECTION OF FLAPS & MLG. CREW CONDUCTED MISSED APPROACH & PROCEEDED TO COMPLETE 'LOSS OF SYS HYDRAULICS NON NORMAL CHECKLIST. CREW PERFORMED VISUAL APPROACH & LANDED A/C WITHOUT INAug 14, 2002 · Boeing 737281 · Drag Control ActuatorSDR C1HA200282015O-Ring · leakingENGINE NR 3 OIL QUANTITY DROPPED TO 1.5 GALLONS. ENGINE OIL TEMPERATURE WAS 90 DEGREES, OIL PRESSURE WAS 44 AND OIL QUANTITY CONTINUED TO DROP TO .5 GALLONS. TEMPERATURE BEGAN TO RISE AND PRESSURE BEGAN TO DROP, EXECUTED A PRECAUTIONARY SHUTDOWN. FOUND O-RIAug 12, 2002 · N682CA · Boeing 7272S7 · Alternator-Generator DriveSDR CA020806010Brake Assy · failed(CAN) NR 4 MAIN LANDING GEAR BRAKE ASSY FOUND DRAGGING DURING PUSHBACK. NR 4 MAIN BRAKE ASSEMBLY AND MAIN WHEEL REPLACED DUE TO DAMAGE. TOTAL TIME OF BRAKE ASSY ARE 381 CYCLES SINCE OVERHAUL. THE LIFE OF THESE BRAKES PRIOR TO OVERHAUL ARE APPROXIMATELY 450 CAug 6, 2002 · Boeing 727217 · BrakeSDR BJNA020811Shear Tie · corrodedFOUND CORROSION IN FORWARD PIT AT STA 500 LBL 2 TO RBL 2 FRAME LOWER LEG, LEVEL 2 CORROSION. CUT AND REMOVED CORROSION FROM SHEAR TIE LEG. FABRICATED AND INSTALLED SHEAR TIE REPAIR AND DOUBLER IAW SRM.Aug 6, 2002 · N344TM · Boeing 737282 · Fuselage Main, StructureSDR BJNA020812Tie Clip · crackedFOUND TENSION TIE FITTING AT STA 104 STR 19L AND 20L CRACKED ON CORNER. LEVEL 2 CORROSION. REMOVED SECTION OF STATION 19L AT FS 104 FABRICATED REPAIR SECTION OF STATION AND TIE CLIP AT 19L AND 1104 TREATED, PRIMED AND INSTALLED STRINGER, SPLICES SECTION AND Aug 6, 2002 · N344TM · Boeing 737282 · Fuselage Miscellaneous StructureSDR BJNA020803Skin · corrodedLAP SEAM RIVETS PULLING SKIN BULGING SEPARATING BS 1088 AT AFT FUSELAGE JACK POINT, LEVEL 2 CORROSION. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW REO. PERMANENT REPAIR.Aug 5, 2002 · N344TM · Boeing 737282 · Fuselage Main, Plate/SkinSDR BJNA020804Stringer · corrodedEACH STRINGER 26L AND 27L AT STA 957 AND 976 HAS CORRODED THROUGH STRINGERS, LEVEL 2 CORROSION. REMOVED CORRODED SECTIONS OF STRINGERS 26L AND 27L, FABRICATED REPAIR SECTIONS FROM BAC1498.163 24 INCHES AND BAC1448-117 12.5 INCHES AND INSTALLED IAW SRM.Aug 5, 2002 · N344TM · Boeing 737282 · Fuselage Main, Longeron/StringerSDR BJNA020808Floor Support · corrodedFOUND CORROSION AT SCREW HOLES (7 EACH AT FRAME LBL 20 BETWEEN BS 947.5 TO BS 986.5. REMOVED AND REPLACED 2 EACH FLOOR SUPPORTS IAW SRM. PERMANENT REPAIR.Aug 5, 2002 · N344TM · Boeing 737282 · Fuselage Miscellaneous StructureSDR BJNA020801Frame · corrodedFORWARD CARGO COMPARTMENT STA 480 MAIN FRAME IS CORRODED AT STRINGER 26R UNDER TRANSITION PANEL. LEVEL 2 CORROSION. REMOVED CORROSION. FABRICATED AND INSTALLED FRAME REPAIR IAW SRM.Aug 4, 2002 · N344TM · Boeing 737282 · Fuselage Main, FrameSDR BJNA020805Skin · chafedLEFT WING OUT BOARD MID AND AFT FLAPS LOWER TRAILING EDGE SKIN HAVE CHAFED AREA JUST OUT BOARD OF NR 2 FLAP TRACK FAIRING. BLENDED AREA ON LEFT WING OUTBOARD MID AND AFT FLAPS LOWER TIE SKIN OUTBOARD OF NR 2 FLAP TRACK FAIRING.Aug 3, 2002 · N344TM · Boeing 737282 · Trailing Edge FlapsSDR CA020806012Motor · binding(CAN) ON APPROACH STAB TRIM REPORTED TO HAVE JAMMED.THE FLT LANDED W/O EVENT.RECTIFICATION UPON LANDING ENGINEER CONTACTED.THE STAB TRIM SYS BRAKE FOUND APPLIED.STAB TRIM SYS THEN FUNCTIONED IN BOTH DIRECTIONS W/O FAULT. TRIM SYS THEN INSPECTED PER AMM WITH NOAug 2, 2002 · Boeing 7372T2 · Stabilizer Control SystemSDR BJNA020807Beam · corrodedCORROSION IN AFT PIT AT STA 727 T CAP SPAR BETWEEN STR 24L 27L CORROSION AT STR 20 AND 21L BETWEEN STA 727 TO 727A. CORROSION LEVEL 2. CUT OUT CORROSION, FABRICATED AND INSTALLED REPAIR SECTION. REMOVED CORRODED VERTICAL BEAM AT BS 737 524-256. FABRICATED Aug 2, 2002 · N344TM · Boeing 737282 · Fuselage Miscellaneous StructureSDR GAIA02078OPDuct · brokenFLT 863 - EWR-FWA - AT THE BEGINNING OF DESCENT TO FWA, THE NR 1 ENGINE FIRE WARNING CAME ON INTERMITTENTLY. POWER WAS REDUCED TO IDLE AND THE WARNING CEASED. THE AIRCRAFT CONTINUED TO FWA AND AN UNEVENTFUL LANDING WAS MADE. INSPECTION REVEALED THAT THE RIGJul 26, 2002 · N916PG · Boeing 727287 · Engine Anti-Icing SystemSDR MEX2002241Wheel · damagedDURING TOWING PROCEDURE IT WAS OBSERVED THE MISSING OF ONE NUT IN A WHEEL OF THE NLG. AIRCRAFT RETURNED TO PLATFORM TO REPLACE THE WHEEL 1 OF THE NLG IAW MM 32-21.Jul 26, 2002 · N1003P · Doug DC932 · Wheel/Ski/FloatSDR 0202399856Pump · failedDURING AIRCRAFT ROTATION FOR FLIGHT, THE RIGHT ENGINE EXPERIENCED A FLAME-OUT. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE RIGHT ENGINE FUEL PUMP. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE.Jul 21, 2002 · N765NC · Doug DC951 · Engine Fuel PumpSDR CA020731016Actuator · failed(CAN) L/E FLAP TRANSIT ON AFTER T/O. NR 5 RT WING SLAT FULLY EXTENDED FOR APPROX 2 MIN. WHEN IT RETRACTED AND BEFORE WE RECYCLED THE FLAPS. REPLACED NR 5 SLAT ACTUATOR AS PER AMM. SYSTEM CHECKED SERVICEABLE AND CERTIFIED.Jul 13, 2002 · Boeing 737217 · Leading Edge Slat ActuatorSDR TSAA0225160Slide · defectiveDURING A ROUTINE TRAINING EXERCISE AND AFTER SUCCESSFUL SLIDE DEPLOYMENT, THE SLIDE ASSEMBLY EXPLODED AT THE SEAM. NO HARM TO PERSONNEL. REMOVED AND REPLACED SLIDE; CONTINUED WITH EXERCISE. SLIDE SENT TO VENDOR FOR EVALUATION.Jul 11, 2002 · N819AL · Boeing 73725A · Escape SlideSDR ASAA0210170Gearbox · damagedBRW - APPROXIMATELY TWENTY SECONDS AFTER TAKEOFF, NR 2 ENGINE EXPERIENCED AN INFLIGHT SHUTDOWN. ENGINE READINGS, N1=7 PERCENT, N2=0 PERCENT, OIL PRESSURE = 0. ENGINE SENT TO SEATTLE EBU FOR EVALUATION, FOUND SIGNIFICANT INTERNAL DAMAGE TO THE GEARBOX. GEARBJul 10, 2002 · N743AS · Boeing 737210C · Turbine Engine Accessory DriveSDR CA020731013Control Cable · failed(CAN) NR 5 FLAP ACTUATOR ROLLER TRACK DISENGAGED AND WENT THROUGH THE INBOARD SIDE OF NR 5 FLAP FAIRING. NR 5 FLAP TRACK FITTING FOUND DAMAGED (SNAPPED) DUE BOOM CABLE BROKEN. CABLE, TRACK FITTING, PULLEYS, BOOM ASSY, AND CAM FOLLOWER GUARD ADJUSTED AS PERJul 9, 2002 · Boeing 7372T7 · Trailing Edge Flap Control SystemSDR C1HA200281006Fuel ControlDuring climb through FL 29 the # 3 engine at fire wall thrust would only maintain 1.8 EPR N1 82 % EGT 480C N2 87% FF 3500, at 35 engine # 3 EPR 1.25 N1 65% EGT 470, N2 70% FF 2000 applied engine anti-ice and fuel heat with no change.Removed and replaced # 3 ENJul 8, 2002 · N681CA · Boeing 7272S7 · Fuel Controlling SystemSDR TSAA0253183Frame · corrodedAUXILIARY POWER UNIT COMPARTMENT CORRODED AT BS 1156 REMOVED DAMAGED SECTION OF FRAME FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER FROM SRM, AIRCRAFT RETURNED TO SERVICE.Jun 29, 2002 · N810AL · Boeing 7372Y5 · Fuselage Main, FrameSDR C1HA200292007Engine · leakingDURING CLIMB THROUGH FL280 NR 2 ENGINE OIL TEMP INDICATED BEYOND REDLINE RADIAL. NR 2 ENGINE SHUTDOWN 2 GALLONS OF OIL LOST, OIL PRESSURE 5PSI DURING DESCENT. OIL TEMP BACK IN GREEN AND AFTER SHUTDOWN NR 2 ENGINE WINDMILLED FOR 21 MINUTES. REMOVED AND REPLACJun 24, 2002 · N292AS · Boeing 727212 · Engine (Turbine/Turboprop)SDR 0202089885Duct · crackedDURING CLIMB, THE LEFT ENGINE EXPERIENCED A FIRE WARNING INDICATION. CREW RETARDED THE LEFT ENGINE THRUST TO IDLE. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE LEFT ENGINE FUEL HEAT DUCT. ENGINE OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICEJun 21, 2002 · N401EA · Doug DC951 · Engine Anti-Icing SystemSDR CA020726007Indicator · failed(CAN) 30 MINUTES AFTER DEPARTURE, ELECTRICAL BURNING SMELL IN COCPIT, AIRCRAFT LANDED SAFELY, BURNING SMELL ORIGINATED BY WEATHER RADAR INDICATOR. INDICATOR REPLACED.Jun 17, 2002 · Boeing 737217 · Weather Radar SystemSDR TSAA0251179Stringer · crackedCRACKS BS 739, S-18R AND BS 745, S-19R. REMOVED DAMAGED AREA, VERIFIED CRACK REMOVAL USING HFEC METHOD, FABRICATED AND INSTALLED REPAIR DOUBLER.Jun 17, 2002 · N807AL · Boeing 7372T4 · Fuselage Main, Longeron/StringerSDR CA020801010Indicator · failed(CAN) FLIGHT WAS DIVERTED DUE TO BURNING SMELL IN COCKPIT FROM WEATHER RADAR INDICATOR. UNIT WAS REPLACED AND SHOP REPORT INDICATED CAUSE OF PROBLEM WAS BURNED OUT DIODES ON RECTIFIER AND FILTER ASSY.Jun 16, 2002 · Boeing 737217 · Weather Radar SystemSDR C8GA20020007Duct · blownFlt 202 from SVMI to KMIA. On take off from SVMI, the engine fire warning bell sounded with no fire light and all engine gauges checked normal. Performed engine fire loop test, #2 engine fire loop did not test. Performed emergency procedures and shut down #2 eJun 13, 2002 · N89427 · Boeing 727227 · Detection SystemSDR CA020725014Adc · failed(CAN) AUTOPILOT ENGAGED IN CRUISE,UNABLE TO UNFREEZE MANUALLY,LEFT WING LEVEL TO A SLIGHT RIGHT BANK. AILERON CONTOL LOST-FROZEN TILL AUTO PILOT RELEASED.CENTRAL AIR DATA COMPUTER REPLACED P/N HG480B13 S/N P-529Jun 13, 2002 · Boeing 737217 · Air Data ComputerSDR CA020610005Gasper Fan · failed(CAN) WHILE BOARDING PAX. SMOKE STARTED ENTERING CABIN IN MID-CABIN RIGHT SIDE AREA.(L1251724)PAX. DEPLANED VIA FWD ENTRY DOOR. FOUND GASPER FAN CONNECTOR & FUSILAGE INSULATION BLANKET BURNT. REPLACED AIR COND. MODULE & CIRCUIT BREAKER AS PER STANDARD PRACTICEJun 9, 2002 · Boeing 737275 · Air Distribution FanSDR C1HA200296015Compressor · stalledON TAKEOFF IN LAS HAD COMPRESSOR STALL, PULLED OFF RUNWAY CALLED MX CONTROL. RAN UP ENGINE, ALL ENGINE PARAMETERS NORMAL. INSPECTED ALL ENGINES AND NO DEFECTS FOUND. RAN ENGINES AT TAKEOFF POWER. ALL PARAMETERS NORMAL. OK FOR SERVICE PER M/M 71-00.Jun 8, 2002 · N696CA · Boeing 7272J4 · Turbine Engine Compressor SectionSDR C1HA200288012Filter · bypassingON TAKEOFF ROLL DURING POWER UP LOW OIL PRESSURE OR FILTER BYPASS LIGHT ILLUMINATED. REMOVED AND REPLACED NR 3 MAIN ENGINE OIL FILTER MM CHPT 79-15-00. OPS & LEAK CHECK GOOD.Jun 1, 2002 · N688CA · Boeing 7272S7 · Turbine Engine Oil SystemSDR CA020528011Circuit Breaker · failed(CAN) ON DESCENT LOST THE NR 2 AND 3 TRANSFORMER RECTIFIERS, ONE FUEL PUMP ON THE NR 1 TANK AND BOTH FUEL PUMPS ON THE NR 2 TANK ALSO F/O'S INSTRUMENTS AND NR 2 RADIO. CREW NOTICED SLIGHT ELECTRICAL SMELL AND ON BASE LEG THE TRANSFER BUS LIGHT CAME ON. CAPTAMay 22, 2002 · Boeing 737275 · AC Generation SystemSDR TSAA0232137Switch · stuckANTI-SKID INOPERATIVE LIGHT ILLUMINATED ON BOTH SYSTEMS DURING FLIGHT. DUE TO WEATHER CONDITIONS, RUNWAY LENGTH AND AIRCRAFT WEIGHT FOR THE AIRPORT, THE AIRCRAFT RETURNED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED A DEFECTIVE LANDING GEAR LEVER UP SWITCHMay 12, 2002 · N819AL · Boeing 73725A · Landing Gear SelectorSDR 0201619883EngineDURING TAKEOFF, THE CREW REPORTED SMOKE IN THE AFT CABIN AREA WITH ASSOCIATED LEFT LAV SMOKE DETECTOR WARNING. AIRCRAFT RETURNED TO FAR AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE. AIRCRAFT RETURNED TO SERVICE.May 9, 2002 · N571MC · Doug DC951 · Powerplant SystemSDR TSAA0233136Battery Pack · dischargedREPLACED NR 6, EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE.May 9, 2002 · N824AL · Boeing 737282 · Emergency LightingSDR CA020429003A/C Pack · smoke(CAN) SHORTLY AFTER TAKOFF, F/A NOTIFIED CREW BOTH SMOKE DETECTORS HAD ACTIVATED AND THERE WAS A SMELL OF SMOKE IN THE CABIN. AIRCRAFT IMMEDIATELY RETURNED TO YYC AND DID AN OVERWEIGHT LANDING - MAINTENANCE INSPECTION FOUND CAUSE OF ODOUR FRON LEFT HAND AIR COApr 29, 2002 · Boeing 737281 · Cabin Cooling SystemSDR CA020429002Tie Bolt · sheared(CAN) DURING AIRCRAFT SERVICE CHECK FOUND NR 3 MAIN WHEEL ASSEMBLY WITH ONE SHEARED TIE BOLT NR 3 MAIN WHEEL ASSEMBLY. REPLACED IAW MM 32-45-1. MAIN WHEEL ASSEMBLY TO BE SENT TO OVERHAUL FACILITY FOR INVESTIGATION AND TEAR DOWN REPORT. FURTHER REPORT(S) TO FApr 26, 2002 · Boeing 727260 · Wheel/Ski/FloatSDR CA020422005Bolt · broken(CAN) DURING SERVICE CHECK, NR 2 MAIN WHEEL TIRE FOUND DEEPLY CUT AND ONE TIE BOLT BROKEN ON MAIN WHEEL HUB ASSY. NR 2 MAIN WHEEL ASSY REPLACED PER MM. MAIN WHEEL ASSY TSO: 472.9 HRS. CSO: 354 CYCLES MAIN WHEEL ASSY TO BE SENT TO OVERHAUL FACILITY FOR TEAR DApr 18, 2002 · Boeing 727260 · Wheel/Ski/FloatSDR CA020422006Structure · damaged(CAN) DURING REGULAR SCHEDULED MAINTENANCE INSPECTION (AD:02-01-01)THE RT ELEVATOR FAILED THE TAB HINGE FREEPLAY CHECK AT THE NR 2 ELEVATOR TAB HINGE POSITION - SUSPECTED CRACK AT ELEVATOR REAR SPAR. EDDY CURRENT INSPECTION CARRIED OUT ON RT ELEVATOR REAR SPARApr 15, 2002 · Boeing 737281 · Elevator, Tab StructureSDR CA020412013Hinge Pin · loose(CAN) DURING B CHECK INSPECTION, MAIN CARGO DOOR HINGE PIN WAS FOUND MIGRATING AFT APROX. 6 INCHES. HINGE PIN REPOSITIONED AND SAFETIED.Apr 8, 2002 · Boeing 727260 · Cargo/Baggage DoorsSDR P2EA2002V0032Link · looseDURING EVALUATION FLIGHT AFTER Q1 AND Q2 INSPECTION, NR 1 ENGINE OIL QUANTITY STARTED DECREASING AFTER TAKEOFF, ENGINE NR 1 SHUTDOWN UPON TOUCHDOWN WITH 0.750 GALS. PRESSURE LINK TIGHTENED AT OIL FILTER BYPASS SW IAW MM 20-50-11 PAGE 211, ENGINE OIL SERVICED Apr 6, 2002 · N239TA · Boeing 73725A · Engine Oil Storage (Airframe Furnished)
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