Pratt & Whitney JT8D-7A

Service difficulty reports · 262

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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 = 'JT8D7A'
  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 CA990614086Generator · failed(CAN) IN CRUISE LT AC BUS LIGHT, GENERATOR OFF LIGHT, AC BUS LIGHT AND AC CROSS-TIE LIGHT ON. AIRCRAFT GROUND RUN CROSS-TIE CHECK TRIED, LOCK-OUT LIGHT ON, GENERATOR WOULD NOT COME ON LINE AND AC CROSS-TIE LOCKOUT LIGHT STAYED ON. AUDIBLE CLACKING FROM OVEMay 24, 1999 · Doug DC932 · AC Generator-AlternatorSDR CA990614092Receptical · failed(CAN) ON GROUND, MSY CIRCUIT BREAKER FOR NR 1 GALLEY POSITION OVEN FOUND TRIPPED, WHEN RESET, CIRCUIT BREAKER TRIPPED AND VISABLE ARCING FROM OUTLET. OUTLET REPLACED.May 20, 1999 · Doug DC932 · Buffet/GalleysSDR CA990603027Controller · failed(CAN) UNABLE TO PRESSURIZE CABIN DURING TAKEOFF. CLIMBED TO 7,000 FEET, BUT CABIN PRESSURE WAS UNCONTROLLABLE IN AUTOMATIC MODE, MANUAL CONTROL NOT TRIED. BOTH NR 1 AND NR 2 CONTROLLERS REPLACED AND AIRCRAFT CHECKED SERVICEABLE.May 18, 1999 · Doug DC932 · Cabin Pressure ControllerSDR CA990603021Plate · loose(CAN) ON WALK-AROUND, FOUND SEVERAL SLICES ON SIDEWALL NR 4 TIRE. FOUND LOOSE SCREWS ON RIGHT MLG DOOR PLATE, SCREW RECOUNTERSUNK AND INSTALLED USING LOCKTIGHT.May 9, 1999 · Doug DC932 · Landing Gear DoorsSDR AU990779Plate · corroded(AUS) FRAME REINFORCEMENT PLATE LOCATED AT STN 227.8 AT THE COCKPIT SIDEWALL CORRODED.Apr 21, 1999 · Boeing 72777C · Fuselage Main, FrameSDR AU990773Skin · corroded(AUS) INTERIOR SKIN CONTAINED CORROSION IN THE FOLLOWING AREAS: 1. BS 1192 - AREA OF CORROSION 25.4 MM BY 177.8 MM (1 INCH BY 7 INCH). 2. BS 1212 - AREA OF CORROSION 38.1 MM BY 101.6 MM (1.5 INCHES BY 4 INCHES). 3. BS 1232 - AREA OF CORROSION 38.1 MM BY Apr 16, 1999 · Boeing 72777C · Fuselage Main, Plate/SkinSDR AU990780Floorbeam · corroded(AUS) FUSELAGE FLOORBEAM LOCATED AT STN 344 LBL 2 CORRODED.Apr 15, 1999 · Boeing 72777C · Fuselage Main, Floor BeamSDR AU990781Bracket · corroded(AUS) MAIN CARGO BARRIER LOWER FITTING SUPPORT BRACKET LOCATED AT STN 375 RBL 39 CORRODED.Apr 14, 1999 · Boeing 72777C · Fuselage Miscellaneous StructureSDR AU990782Flange · corroded(AUS) MAIN CARGO COMPARTMENT TIEDOWN TRACK FLANGE CORRODED AT BS 968, BS 1002, BS 1027, BS 1043 AND BS 1072 AT RBL 63.Apr 14, 1999 · Boeing 72777C · Fuselage Miscellaneous StructureSDR AU990783Flange · corroded(AUS) MAIN CARGO COMPARTMENT TIEDOWN TRACK FLANGE CORRODED AT BS 968, BS 1002, BS 1027, BS 1043 AND BS 1072 AT RBL 63.Apr 9, 1999 · Boeing 72777C · Fuselage, Seat/Cargo Attach FittingsSDR AU990784Flange · corroded(AUS) MAIN CARGO COMPARTMENT TIEDOWN TRACK FLANGE CORRODED AT STN 847 RBL 63.Apr 9, 1999 · Boeing 72777C · Fuselage, Seat/Cargo Attach FittingsSDR AU990785Bulkhead · corroded(AUS) E/E COMPARTMENT BULKHEAD LOCATED AT STN BS 350.2, BL RBL 36 CORRODED. AREA OF CORROSION 1935.48 SQMM (3 SQUARE INCHES).Apr 9, 1999 · Boeing 72777C · Fuselage Main, BulkheadSDR AU990772Stiffener · corroded(AUS) RIGHT WING FRONT SPAR STIFFENER CONTAINED LEVEL 2 CORROSION.Apr 8, 1999 · Boeing 72777C · Wing Miscellaneous StructureSDR AU990775Skin · corroded(AUS) LET ELEVATOR LOWER SKIN BULGED AND CORRODED BETWEEN SEVEN RIVETS AT STN 159 TRAILING EDGE.Apr 7, 1999 · Boeing 72777C · Elevator, Plate/SkinSDR AU990776Spar · corroded(AUS) RIGHT STABILIZER REAR SPAR UPPER CHORD BULGED AND CORRODED FOR APPROXIMATELY 177.8 MM (7 INCHES) BETWEEN STN 176 AND STN 186.Apr 7, 1999 · Boeing 72777C · Horizontal Stabilizer, Spar/RibSDR AU990777Beam · corroded(AUS) RIGHT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM CORRODED FOR APPROXIMATELY 127 MM (5 INCHES) BETWEEN STN 200 AND STN 209.Apr 7, 1999 · Boeing 72777C · Horizontal Stabilizer StructureSDR AU990420022Engine · malfunctioned(AU) NR 2 ENGINE HAD A PARTIAL POWER LOSS ON TAKEOFF. THE NR 1 ENGINE EPR WAS 1.95, THE NR 2 WAS 1.60, AND THE EXHAUST GAS TEMPERATURE WAS 100 DEGREES GREATER THAN THE NR 1 ENGINE. THE NR 2 ENGINE WAS REPLACED AND GROUND RUN SERVICEABLE.Apr 3, 1999 · Doug DC932 · Engine (Turbine/Turboprop)SDR AU990358Harness · failed(AUS) BURNED WIRE BUNDLE LOCATED IN THE FORWARD E/E COMPARTMENT AT STN 296-312 IN THE RT SIDE UNDER THE TOILET SERVICE DUCT. A TOTAL OF 68 WIRES REPLACED.Feb 24, 1999 · Boeing 72777C · DC Power Distribution SystemSDR CA990330070Indicator · failed(CAN) FUEL SPILL FROM RIGHT WING VENT BOX DURING RE-FUELING, PASS AND CREW EVACUATED. LEFT WING FUEL QUANTITY INDICATOR NOT WORKING. REPLACED BOTH LUGS ON FUEL QUANTITY PROBE.Feb 19, 1999 · Doug DC932 · Fuel Quantity IndicatorSDR CA990203018Combustion Can · failed(CAN) ENGINE INDUCTED IN THE SHOP FOR 12 STAGE HP COMPRESSOR DISC BEING TX'D. DISASSEMBLY OF THE ENGINE FOUND TWO COMBUSTION CANS (IGNITER CANS) WERE SHOWING SIGNS OF EXTREME BRITTLENESS AND AN EXCESSIVE NUMBER OF INTERGRANULAR CRACKS. THE TWO CANS WERE SCRAJan 12, 1999 · Doug DC932 · Turbine Engine Combustion SectionSDR CA990115019Wheel · failed(CAN) AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT, RECYCLED DOWN, ON NEXT RETRACT NOSE GEAR UNSAFE LIGHT ON WITH OBVIOUS VIBRATION, QUICK REFERENCE HANDBOOK PROCEDURE CARRIED OUT, GEAR UNSAFE LIGHT WENT OUT. AIRCRAFT RETURNED TO BLOCKS. REPLACED BOTH NOSE Dec 31, 1998 · Doug DC932 · Wheel/Ski/FloatSDR CA990111049Apu · failed(CAN) INTERMITTENT SMOKE DETECTORS ON ONLY WHEN APU PROVIDING AIR CONDITIONING ON GROUND, NOTICEABLE ODORS IN CABIN. OK WITH GROUND COOLING FAN OR ENGINE AIR USED. APU REPLACED.Dec 29, 1998 · Doug DC932 · APU Core EngineSDR CA981130013Actuator · failed(CAN) UNABLE TO ARM SPOILERS ON APPROACH, QUICK REFERENCE HANDBOOK PROCEDURE CARRIED OUT. REPLACED AUTO SPOILER ACTUATOR.Nov 9, 1998 · Doug DC932 · Leading Edge Slat ActuatorSDR CA981230053Spacer · fractured(CAN) NR 2 ENGINE HAD HIGH VIBRATION AFTER TAKEOFF. ENGINE WAS SHUT DOWN AT 16,000 FEET. POST-FLIGHT INSPECTION FOUND THE SPACER BETWEEN THE 3-4 STAGE OF THE TURBINE WITH A 4 PIECE MISSING. THE DAMAGE INITIATED FROM A CRACK IN THE TIE ROD BOLT HOLE INNER THNov 4, 1998 · Doug DC932 · Turbine SectionSDR CA981019023Regulator · failed(CAN) IN-FLIGHT AIRCRAFT CROSS TIE LOCKOUT LIGHT CAME ON. CARRIED OUT QRH CK LIST WITH ONE RESET. LIGHTS STAYED ON, AIRCRAFT RETURNED. LT VOLTAGE REGULATOR AND GENERATOR REPLACED. GROUND RUN SERVICEABLE.Oct 3, 1998 · Doug DC932 · DC Generating SystemSDR 98ZZZX3970Valve · malfunctionedFUEL HEAT VALVE, WHITTAKER CONTROLS P/N 320115, VALVE INSTALLED ON THE NR 3 ENGINE. FUEL HEAT VALVE PREVIOUSLY PLACED ON MEL, VALVE VIBRATED PARTIALLY OPEN, OIL TEMP HIGH, CREW MADE PRECAUTIONARY ENGINE SHUT DOWN. AIRCRAFT DIVERTED TO ATLANTA. REMOVED AND ROct 2, 1998 · N286US · Boeing 727251 · Fuel HeaterSDR CA981019022Controller · failed(CAN) DURING CLIMB THROUGH LEVEL 280, CABIN PRESSURE RED WARNING LIGHT CAME ON. RAPID DEPRESSURIZATION DRILL CARRIED OUT, BUT CABIN REACHED 11,000 FEET. FLIGHT RETURNED TO BLOCKS. BOTH CONTROLLERS REPLACED SERVICEABLE.Oct 2, 1998 · Doug DC932 · Cabin Pressure ControllerSDR CA981019025Combustion Case · cracked(CAN) DURING ENGINE DISASSEMBLY THE COMBUSTION OUTER CASE WAS FOUND CRACKED IN THE REAR FLANGE AT THREE DIFFERENT LOCATIONS. THE CRACKS WERE FROM THE HOLES AT THE INNER DIAMETER AND CONTINUED TOWARDS THE OUTER CASE WALL. THE COMBUSTION OUTER CASE WAS REPLACESep 28, 1998 · Doug DC932 · Turbine Engine Combustion SectionSDR CA981019028Controller · failed(CAN) AIRCRAFT RETURNED TO AIRPORT WITH RIGHT PACK OVERHEAT AND SMOKE AND BURNING SMELL. RIGHT PACK TEMP CONTROL VALVE WENT TO FULL HOT, WHEN COLD SELECTED VALVE RESPONDED CORRECTLY. TEMPERATURE CONTROLLER REPLACED.Sep 24, 1998 · Doug DC932 · Cabin Temperature ControllerSDR CA981019029Controller · failed(CAN) ON DEPARTURE AT 2,500 FEET, THE RIGHT AIR CONDITION PACK OVERHEATED THEN FORWARD FIRE DETECTORS ANNUNCIATED, FLIGHT ATTENDANT REPORTED SMOKE IN CABIN, DECLARED EMERGENCY AND RETURNED TO BLOCKS . REPLACED AUTOMATIC CABIN TEMPERATURE CONTROLLER.Sep 22, 1998 · Doug DC932 · Cabin Temperature ControllerSDR CA981001007Actuator · failed(CAN) DURING TAKEOFF WHEN POWER APPLIED PRESSURIZATION CONTROL WAS HUNTING FOR PROPER POSITION. DURING CLIMB-OUT CABIN WAS MAX CLIMB, CABIN ALT SHOWED 2,500 FEET. LEVELLED OFF AT 7,000 FEET BUT NO CONTROL OVER PRESSURIZATION SYSTEM. REPLACED NR 1 CABIN CONTRSep 20, 1998 · Doug DC932 · Pressure Regulator/Outflow ValveSDR CA981019030Door · jammed(CAN) AT ARRIVAL GATE, FOUND LEFT MLG DOOR HANGING DOWN. FOUND DOOR JAMMED AND GEAR DOOR FOLLOW-UP EANCO CABLE JAMMING, AND FOLLOW-UP TORQUE TUBE RIVET SHEARED. PARTS REPLACED/REPAIRED. SYSTEM SERVICEABLE.Sep 20, 1998 · Doug DC932 · Landing Gear DoorsSDR TWAA9815101Engine · bird strikeSHORTLY AFTER TAKEOFF, SMELLED INITIAL ODOR IN COCKPIT AND CABIN. RESEMBLED BURNING IN OVENS BUT MORE ACRID. LATER DESCRIBED AS CHEMICAL ELECTRICAL SMELL. FLT RETURNED TO STL. FOUND BIRD HAD BEEN INJESTED IN LT ENGINE AFFECTING THE PNEUMATIC SYSTEM. ACCOMSep 16, 1998 · N490SA · Doug DC915 · Engine (Turbine/Turboprop)SDR CA981001010Apu · leaking(CAN) ON ENGINE START, OIL SMELL REPORTED, AFT CABIN SMOKE ALARM CAME ON. AIR CYCLE MACHINE OIL LEVEL FOUND LOW. LEFT AIR CYCLE MACHINE AND APU REPLACED, SYSTEM SERVICEABLE.Aug 28, 1998 · Doug DC932 · Heating SystemSDR CA980706027Outflow Valve · failed(CAN) ON CLIMB-OUT, AT 26,000 FEET, FLOW LIGHT ILLUMINATED, CABIN DIFFERENTIAL AT MAXIMUM 8 POUNDS PER SQUARE INCH. LEVELED OFF AT 280 WITH CABIN ALTITUDE AT 4,000 ABOUT 1,400 BELOW SCHEDULE, NO STANDBY LIGHT ON. SELECTED MANUAL TO REGAIN SCHEDULE, WHEN AUTOJun 16, 1998 · Doug DC932 · Pressure Regulator/Outflow ValveSDR CA980706030Oven Socket · failed(CAN) DURING APPROACH, AN ELECTRICAL BURNING SMELL WAS DETECTED COMING FROM THE GALLEY. THE GALLEY POWER WAS TURNED OFF, SMELL DISSIPATED AND A/C LANDED SAFELY. MAINTENANCE FOUND OVEN POSITION NR 17 SOCKET BURNT. OVEN POSITION NR 17 SOCKET WAS REPLACED.Jun 9, 1998 · Doug DC932 · Buffet/GalleysSDR CA980629019Control Cable · stiff(CAN) ON LANDING ROLL, GEAR DOOR OPEN LIGHT ON, LT GEAR DOOR OPEN CONFIRMED BY TOWER. MAINTENANCE CHECK FOUND CABLE OF LT MAIN GEAR DOOR SEQUENCE STIFF AND TORQUE TUBE RIVET SHEARED. CABLE CLEANED AND LUBRICATED, REPLACED DOOR AND RIVET, FOLLOW-UP CABLE RIGGJun 3, 1998 · Doug DC932 · Landing Gear Door Retract SectionSDR CA980629018Spacer · cracked(CAN) DURING DISASSEMBLY OF A TIME EXPIRED ENGINE, THE FRONT COMPRESSOR ROTOR THIRD TO FOURTH STAGE SPACER WAS FOUND CRACKED. THERE WERE 8 CRACKS EXTENDING FROM THE TIE ROD SLEEVE HOLES TO THE INSIDE, AND THERE WAS ONE SMALL CRACK STARTING FROM THE TIE ROD SLEJun 1, 1998 · Doug DC932 · Turbine Engine Compressor SectionSDR CA980608021Apu · leaking(CAN) DURING CLIMB OUT, AN OILY SMELL WAS DETECTED IN BUSINESS CLASS SECTION OF PASSENGER COMPARTMENT. SMELL DISSIPATED AFTER LEFT HAND AIR CONDTIONER PACK TURNED OFF. MAINTENANCE CHECK REVEALED AUXILIARY POWER UNIT WAS CONTAMINATING LEFT AIR CONDITIONER PACMay 19, 1998 · Doug DC932 · Airborne Auxiliary Power Unit (APU) SystemSDR CA980608036Audio Panel · inoperative(CAN) LOSS OF VHF COMMUNICATION ON APPROACH TO AIRPORT, SOME TRANSMISSIONS TOO WEAK TO BE READ BY AIR TRAFFIC CONTROL CENTER. MAINTENANCE REPAIRED THREE BROKEN WIRES ON CAPTAIN'S AUDIO CONTROL PANEL CONNECTOR.May 1, 1998 · Doug DC932 · Audio Integrating SystemSDR CA980512017Receptacle · malfunctioned(CAN) ELECTRICAL SHOCK FELT WHEN REMOVING OVEN GALLEY TROLLEY FROM RECEPTACLE, POSITION NR 17. TROLLEY REMOVED FOR FURTHER TESTING AT ACCESSORY SHOP. VISUAL INSPECTION OF RECEPTACLE CARRIED OUT, NO ARCING SIGNS PRESENT. RE-INSPECTED IN APRIL AND FOUND 3 PHAApr 21, 1998 · Doug DC932 · Buffet/GalleysSDR CA980417014Switch · failed(CAN) DURING TAXIING OUT FOR TAKEOFF, SMOKE AND FIRE OBSERVED COMING FROM OVERHEAD ELECTRICAL PANEL IN COCKPIT. EMERGENCY EVACUATION DRILL CARRIED OUT AND PORTABLE FIRE EXTINGUISHER DISCHARGED INTO FIRE AREA AND FIRE EXTINGUISHED. MAINTENANCE INVESTIGATION RMar 27, 1998 · Doug DC932 · Ignition SwitchingSDR CA980424015Oven · malfunctioned(CAN) ELECTRICAL FUMES DETECTED ON CLIMB-OUT. ELECT FIRE DRILL CARRIED OUT. GALLEY POWER SWITCHED OFF. SMELL DISSIPATED WITHIN ONE MINUTE. GALLEY OVEN 16 FOUND TO BE THE CAUSE. FAULTY RECEPTACLE CHANGED.Mar 27, 1998 · Doug DC932 · Buffet/GalleysSDR CA990203014Compressor · damaged(CAN) ON TAKEOFF, POWER LEVERS BROUGHT TO 1.4 EPR FOR RUN-UP, ALL OKAY. AT APPROXIMATELY 85-95 KNOTS, THE NR 2 ENGINE HAD A POWER LOSS. EGT INITIALLY AT 700 CELCIUS, ON SHUTDOWN EGT AT 800 CELSIUS. FIRE TRUCKS CALLED. INSPECTION FOUND HEAVY DAMAGE TO THE HMar 15, 1998 · Doug DC932 · Turbine Engine Compressor SectionSDR CA980402007Engine · power loss(CAN) ON TAKEOFF POWER LEVERS BROUGHT TO 1.4 EPR FOR RUN-UP, ALL OKAY. AT APPROXIMATELY 85-95 KNOTS, NR 2 ENGINE HAD A POWER LOSS AND THE EGT INITIALLY AT 700C, WENT TO 800 C. ENGINE WAS SHUTDOWN AND FIRE TRUCKS WERE CALLED. THE NR 2 ENGINE WAS REPLACED. RESULMar 15, 1998 · Doug DC932 · Engine (Turbine/Turboprop)SDR CA980305013Control Valve · inoperative(CAN) AIRCRAFT RETURNED DUE TO PRESSSURIZATION FAULT. CABIN CONTINUED TO CLIMB PAST 11,000 FEET, OXYGEN MASKS DEPLOYED. LEFT PACK WATER SEPARATOR TEMPERATURE CONTROL VALVE FOUND INOPERATIVE WHEN PACK IN OPERATION. VALVE REPLACED AND CHECKED SERVICEABLE.Feb 19, 1998 · Doug DC932 · Cabin Temperature Control SystemSDR AU971497Sensor · fod(AUS) NO1 ENGINE P2 INLET BLOCKED BY A WASP.Nov 19, 1997 · Boeing 72777C · Fuel Control/Reciprocating EnginesSDR CA971208009Windshield · failed(CAN) DURING FLIGHT, FIRST OFFICER'S WINDSHIELD SHATTERED. VISION WAS OBSTRUCTED AND ELECTRICAL ARCING WAS OBSERVED. MAINTENANCE ACTION INVOLVED REPLACING WINDSHIELD AND HEAT CONTROLLER.Nov 19, 1997 · Doug DC932 · Flight Compartment WindowsSDR CA971125009Air Cyc Machine · inoperative(CAN) AFTER TAKEOFF, FLIGHT ATTENDANT REPORTED SMOKE IN CABIN. QUICK REFERENCE HANDBOOK (QRH) DRILL CARRIED OUT AND SMOKE CLEARED WITHIN ONE MINUTE. RT PACK REMAINED OFF FOR REMAINDER OF FLIGHT. MAINTENANCE ACTION INVOLVED CHANGING RT CYCLING MACHINE AND CONov 2, 1997 · Doug DC932 · Cabin Cooling SystemSDR CA971113030Door Frame · corroded(CAN) AFT CARGO DOOR FRAME AT BS 1110 STRINGER 26 RIGHT TO 27 RIGHT WAS FOUND CORRODED. REPAIRED. AIRCRAFT TT: 43,882 HOURS.Oct 23, 1997 · Boeing 727171C · Fuselage Miscellaneous Structure
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