Pratt & Whitney JT8D-9A
Service difficulty reports · 1,388
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 = 'JT8D9A' 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 = 'JT8D9A' 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 72300067Shear Tie · corrodedAPPROX 1 INCH BY 2 INCH AREA OF CORROSION ON SHEAR TIE.SDR SE28102004Charger · failedDURING B-CHECK MAINTENANCE FOUND THE AFT HALF OF THE EMERGENCY PATH TRACK WOULD NOT COME ON. REMOVED AND REPLACED EMERGENCY PATH LIGHTING BATTERY AND BATTERY CHARGER IAW MM 33-53-1. OPS CHECKS GOOD.SDR 72300045Stringer · corroded1 INCH AREA OF CORROSION ON S-26R.SDR 72300075Stiffener · corroded2 INCH BY .5 INCH AREA OF CORROSION ON STIFFENER.SDR 72300008Shear Tie · corroded1 INCH BY 3 INCH AREA OF CORROSION ON SHEAR TIE.SDR 72300012Shear Tie · corrodedCORROSION ON SHEAR TIE.SDR 72300081Stringer · corrodedSEVERAL AREAS OF CORROSION ON BOTTOM OF STRINGER.SDR 72300082Stringer · corrodedSEVERAL AREAS OF CORROSION ON STRINGER.SDR 72300083Stringer · corroded2 INCH BY 4 INCH AREA OF CORROSION ON BOTTOM OF STRINGER.SDR 72300147Stringer · corrodedA 1 X 2 INCH AREA OF CORROSION ON STRINGER.SDR 72300156Stringer · corrodedA 1.5 X 5 INCH AREA OF CORROSION ON STRINGER BOTTOM.SDR 72300158Stringer · corrodedA 1 X 2 INCH AREA OF CORROSION ON STRINGER BOTTOM.SDR 72300168Frame · corroded2 INCH BY 2 INCH AREA OF CORROSION ON FRAME WEB.SDR 72300196Fitting · corrodedA 1 X 1 INCH AREA OF CORROSION OF FITTING.SDR 72300197Skin · corrodedA 3 X 5 INCH AREA OF CORROSION ON SKIN.SDR 72300015Shear Tie · corroded1 INCH BY 2 INCH AREA OF CORROSION ON SHEAR TIE.SDR 72300160Frame · corrodedA 3 X 6 INCH AREA OF CORROSION ON FRAME WEB.SDR 72300217Threshold · corrodedCORROSION ON DOOR THRESHOLD ATTACHMENT ANGLES, WEB STIFFENERS, WEB REPLACEMENT.SDR 72300035Angle · corroded1 INCH BY 1.5 INCH AREA OF CORROSION ON CHORD.SDR 72300057Reinforcement · corroded1 INCH BY 1 INCH AREA OF CORROSION ON REINFORCEMENT CHORD.SDR 72300165Stringer · corroded3 INCH BY 12 INCH AREA OF CORROSION ON STRINGER.SDR 72300030Stringer · corrodedSTRINGER FLANGE CORRODED 20 INCH IN LENGTH.SDR 72300041Stringer · corroded1 INCH BY 16 INCH AREA OF CORROSION ON BOTTOM OF STRINGERSDR 72300042Stringer · corroded1 INCH BY 13 INCH AREA OF CORROSION ON BOTTOM OF STRINGERSDR 72300043Stringer · corroded1 INCH BY 15 INCH AREA OF CORROSION ON BOTTOM OF STRINGERSDR 72300046Stringer · corroded2.5 INCH BY 5 INCH AREA OF CORROSION ON STRINGER.SDR 72300047Stringer · corroded3 INCH BY 16 INCH AREA OF CORROSION ON STRINGER.SDR 72300061Skin · corrodedAPPROX 2 INCH BY 2 INCH AREA OF CORROSION AROUND ANTENNA MOUNT ON FUSE SKIN.SDR 72300014Shear Tie · corroded1 INCH BY 3 INCH AREA OF CORROSION ON SHEAR TIE.SDR 72300173Stringer · corrodedA 1 X 2 INCH AREA OF CORROSION ON BOTTOM OF STRINGER END FITTING.SDR CA041020002Fitting · cracked(CAN) DURING ROUTINE MAINTENANCE A CRACK WAS FOUND IN THE LEFT HAND MLG UPLOCK FITTINGIN THE FORWARD RADIUS. NDT CONFIRMED THE CRACK. FITTING WAS REPLACED AND GEAR RETRACTIONS CARRIED OUT.SDR 72300029Shear Tie · corroded1 INCH BY 3 INCH AREA OF CORROSION ON SHEAR TIE.SDR 72300037Shear Tie · corroded1 INCH BY 4 INCH AREA OF CORROSION ON SHEAR TIE.SDR 72300038Shear Tie · corroded1 INCH BY 1.5 INCH AREA OF CORROSION ON SHEAR TIE.SDR 72300079Shear Tie · corroded1.5 INCH BY 2 INCH AREA OF CORROSION ON SHEAR TIE.SDR 72300080Skin · corrodedSEVERAL AREAS OF CORROSION ON INTERIOR OF SKIN.SDR 72300019Shear Tie · corroded.5 INCH BY 1 INCH AREA OF CORROSION ON SHEAR TIESDR 72300216Skin · corrodedCORROSION ON INTERIOR DOOR SKIN.SDR CA041013010Actuator · cracked(CAN) A SYSTEM HYDRAULIC LIGHTS ILLUMINATED, A SYSTEM QTY READ ZERO. NR 8 SPOILER ACTUATOR FOUND CRACKED. ACTUATOR REPLACED MM 27-62-91. CARRIED OUT RII INSPECTION.SDR 72300163Stringer · corrodedSEVERAL AREAS OF CORROSION ON BOTTOM OF STRINGER.SDR 72300195Flange · crackedA 1 INCH CRACK IN UPPER FLANGE.SDR CA041012002Hydraulic System · inoperative(CAN) LOSS OF SYSTEM A-HYDS AT FL270, INDICATED BY SYSTEM A-FLT CONTROL LOW PRESSURE & FEEL DIFF PRESSURE LIGHT AND A-QTY AT .5 GALLONS. ACRFT RETURNED TO AIRPORT. FLT CONTROL MODULE A-SYS REPLACED. ALSO BOTH A & B CASE DRAIN FILTERS & BOTH A-SYS HYD EDPS RESDR CA041007001Wire · chafed(CAN) JUST PRIOR TO ENGINE START AT AN OUTBASE, THE A/C APU SHUT DOWN ON ITS OWN. GROUND EQUIPMENT WAS USED TO POWER AND START THE A/C, AND THE FLIGHT CONTINUED. AT THE TERMINATING BASE, MAINTENANCE PERSONNEL FOUND 2 WIRES AT THE APU THAT HAD CHAFED AND SHORTSDR 0401809607Skin · crackedDURING M-CHECK FOUND CRACKED IN RT WING TRAILING EDGE FLAP UPPER STRINGER AT WING STATION 235. REPAIRED IAW EA 96-200350.SDR TSAA0475073Line · looseNR 1 ENGINE WILL NOT REACH TAKEOFF POWER; REPORTED BY CREW. MAINTENANCE TROUBLE SHOOTING FOUND THE AFT PT7 LINE LOOSE. SECURED THE LINE; RAN ENGINE TO POWER. ALL PARAMETERS, OPS AND LEAK CHECK GOOD. SYSTEM CHECK OK. AIRCRAFT RETURNED TO SERVICE.SDR C8GA20040020Engine · defectiveFLT 1721 FROM FLL TO TOL, AT FL140, AT CLIMB POWER THE NR 1 ENG LOW OIL PRESSURE FILTER BYPASS LIGHT ILLUMINATED. FOLLOWED AOM PROCEDURES A2-10 AND THE NR 1 ENG IN-FLIGHT SHUTDOWN AS A PRECAUTIONARY AND AIR TURN BACK TO FLL. A/C WAS INSPECTED AND THE LOW OIL PSDR C8GA20040019Engine · damagedFLT 727 FROM DFW TO TOL. ON TAKEOFF, THE NR 3 ENGINE HAD STRONG VIBRATION. IN-FLIGHT SHUTDOWN OF THE NR 3 ENGINE AS A PRECAUTIONARY ADVISED ATC DECLARED EMERGENCY AND AIR TURN BACK TO DFW. AIRCRAFT WAS INSPECTED AND FOUND FAILURE OF TURBINE SECTION PER EVIDESDR CA040922002Rod End · sheared(CAN) DURING ROUTINE OPENING OF THE CARGO DOOR FOR LOADING OF THE AIRCRAFT, A WIND GUST BLEW THE DOOR FULLY OPEN, AND SHEARED ALL FOUR ACTUATOR LINK RODS. THE DOOR ENDED UP IN A VERTICAL POSITION. THE WIND VELOCITY AND GUSTS WERE CHECKED WITH THE CONTROL TOWERSDR TSAA0473068Fcu · malfunctionedON TAKEOFF UNABLE TO OBTAIN MAX-POWER ON NR 1 ENGINE, ENGINE POWER ADVANCED NORMALLY UNTIL 1.96-1.97 EPR INDICATION. MAX-POWER OBTAINED WAS 1.97 EPR WITH N1 AT 94 PERCENT; FURTHER THRUST LEVER MOVEMENT HAD NO EFFECT. REMOVED AND REPLACED THE NR 1 ENGINE FCU SDR TSAA0477066Engine · malfunctionedON TAKEOFF UNABLE TO OBTAIN MAX-POWER ON NR 1 ENGINE, MAX-EPR INDICATION OF 1.96. RETURNED TO HNL. CLEANED DEBRIS FROM PT2 LINE AND VERIFIED SECURITY OF ALL EPR LINES. PERFORMED ENGINE RUN FOR TAKEOFF POWER VERIFICATION, OPS CHECK OK. AIRCRAFT RETURNED TO S
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