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.

SDR 72300199Stringer · corrodedA 2 X 1 INCH AREA OF CORROSION ON STRINGER.Nov 18, 2004 · N723CK · Boeing 7272H3 · Fuselage Main, Longeron/StringerSDR 72300065Stringer · corrodedSEVERAL AREAS OF CORROSION ON STRINGER.Nov 17, 2004 · N723CK · Boeing 7272H3 · Fuselage Main, Longeron/StringerSDR CA041117005Engine · failedDURING DAILY CHECK, OIL WAS FOUND IN TAILPIPE AND LAST TWO STAGES OF TURBINE SECTION COATED WITH OIL. RT ENGINE SER NR 667210. RT ENGINE REPLACED. ENGINE SER NR ON 667217. TIMES 61700.25 CYCLES 57721.Nov 16, 2004 · Boeing 7372Q9 · Engine (Turbine/Turboprop)SDR TSAA0426077Connector · damagedFLT 942, HNL-KOA: (NON-ETOPS) AFTER ENGINES WERE STARTED, THE NR 2 ENGINE FIRE WARNING SWITCH AND BELL CAME ON. FOLLOWED THE QRH AND SHUT DOWN THE ENGINE. REPLACED THE HERMETIC CONNECTORS ON THE NR 2 ENGINE LOWER FIRE DETECTION LOOP. ACCOMPLISHED HIGH POWERNov 15, 2004 · N805AL · Boeing 7372M6C · Fire Protection System WiringSDR 72300033Stringer · corrodedCORROSION ON STRINGER BETWEEN BS 600-660.Nov 13, 2004 · N723CK · Boeing 7272H3 · Fuselage Main, Longeron/StringerSDR TSAA0471076Line · obstructedFLT 840, NR 2 ENGINE PUTTING OUT LESS POWER THAN THE NR 1 ENGINE AT 1.89 EPR. SUSPECT NR 2 PT2 PROBE. REMOVED DEBRIS FROM THE PT2 SENSE TUBE BETWEEN THE ENGINE AND TRANSDUCER. ENGINE RUN-UP AND EPR CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE.Nov 11, 2004 · N816AL · Boeing 7372X6C · Engine ControlsSDR TSAA0426075Fire Loop · malfunctionedFLT 922, (NON-ETOPS) HAD ENGINE NR 2 FIRE INDICATION ON CLIMBOUT. SHUTDOWN ENGINE NR 2 AND FIRED BOTH ENGINE FIRE EXTINGUISHER BOTTLES. RETURNED TO HNL. REPLACED THE NR 2 ENGINE LOWER FIRE DETECTION LOOP. SYSTEM CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.Nov 9, 2004 · N805AL · Boeing 737800* · Fire DetectionSDR 72300034Bulkhead · corroded1.5 INCH BY 1.5 INCH AREA OF CORROSION ON WEB.Nov 9, 2004 · N723CK · Boeing 7272H3 · Fuselage Main, BulkheadSDR CA041108010Skin · cracked(CAN) FUSELAGE CRACK FOUND ON OUTER SKIN AT STN 767 STR 18L, 0.875 INCHES LONG. CRACK REPAIRED IAW SRM 53-30-3 FIG 48 SHEET 32 DETAIL X REV.90. TIMES 61643.42 CYCLES 57682.Nov 6, 2004 · Boeing 7372Q9 · Fuselage Main, Plate/SkinSDR 72300064Stringer · corrodedSMALL AREAS OF CORROSION ON STRINGER.Nov 6, 2004 · N723CK · Boeing 7272H3 · Fuselage Main, Longeron/StringerSDR CA041108009Isolation Valve · malfunctioned(CAN) ON TAKEOFF, GEAR HANDLE INITIALLY WOULD NOT COME UP AND ASSOCIATED OVERHEAD ISOLATION VALVE ILLUMINATED. AFTER FLAP RETRACTION TOCWS SOUNDED FOR TWO MINUTES, THEN STOPPED AND GEAR CAME UP NORMAL.AIR SAFETY SENSOR REPLACED AND TESTED SERV. GROUND SPOILER Nov 4, 2004 · Boeing 737201 · Landing Gear Retraction/Extension SystemSDR 72300031Door Frame · corroded3 INCH BY 5 INCH AREA OF CORROSION ON FUSELAGE DOOR FRAME.Nov 2, 2004 · N723CK · Boeing 7272H3 · Fuselage Main, StructureSDR 72300036Stringer · corroded1 INCY BY 3 INCH AREA OF CORROSION ON STRINGER.Nov 2, 2004 · N723CK · Boeing 7272H3 · Fuselage Main, Longeron/StringerSDR 72300063Fitting · corrodedCORROSION ON END FITTING APPROX 2.5 INCH BY 6 INCH BY 4 INCH.Nov 2, 2004 · N723CK · Boeing 7272H3 · Fuselage Main, Attach FittingsSDR 72300149Floorbeam · corrodedTWO 1 X 1 INCH AREAS OF CORROSION ON FLOORBEAM CHORD.Nov 2, 2004 · N723CK · Boeing 7272H3 · Fuselage Main, Floor BeamSDR 72300180Frame · corroded1 INCH BY 1 INCH AREA OF CORROSION ON LOWER CHORD.Nov 2, 2004 · N723CK · Boeing 7272H3 · Fuselage Main, FrameSDR 72300181Frame · corroded1 INCH BY 9 INCH AREA OF CORROSION ON LOWER CHORD.Nov 2, 2004 · N723CK · Boeing 7272H3 · Fuselage Main, FrameSDR CA041105002Pump · failedDURING CLIMB, THE NR 2 ENGINE FLAMED OUT. THE AIRCRAFT RETURNED TO THE AIRPORT. MAINTENANCE TROUBLESHOOTING FOUND THAT METERED FUEL WAS NOT BEING DELIVERED TO THE ENGINE, BUT FUEL WAS PRESENT UP TO THE FCU/FUEL PUMP ASSY. THE FCU/FUEL PUMP ASSY WAS REPLACEDNov 1, 2004 · Boeing 737201 · Engine Fuel PumpSDR CA041108004Control Cable · frayedDURING AN 'A' CHECK INSPECTION, FOUND THE CONTROL CABLE FOR NR 7 FLT SPOILER FRAYED, AS A RESULT OF CHAFING THROUGH A FAIRLEAD. CABLE WAS REPLACED, FAIRLEAD RE-POSITIONED, FUNCTION CHECKED. AIRCRAFT RETURNED TO SERVICE. NO OTHER PROBLEMS OR ACTIONS.Oct 30, 2004 · Boeing 737210C · Drag Control SystemSDR CA050120002Balance Weight · misinstalled(CAN) DURING HEAVY MAINTENANCE THE RT AILERON WAS DISCOVERED IN AN IMPROPER CONFIGURATION. THE BALANCE WEIGHT ASSOCIATED WITH A COMPOSITE UNIT WAS FOUND TO BE INSTALLED WHEN THE AILERON WHICH WAS REMOVED FOR REPAINT COULD NOT BE BALANCED AT REINSTALLATION. THEOct 28, 2004 · Boeing 737248C · AileronsSDR 72300056Frame · corroded3 INCH BY 5 INCH AREA OF CORROSION ON FRAME WEB.Oct 28, 2004 · N723CK · Boeing 7272H3 · Fuselage Main, FrameSDR 72300074Frame · corroded2 INCH BY 8 INCH AREA OF CORROSION ON FRAME.Oct 28, 2004 · N723CK · Boeing 7272H3 · Fuselage Main, FrameSDR 72300084Spar · corrodedA 3 X 3 INCH AREA OF CORROSION ON SPAR CHORD VERT FLANGE.Oct 28, 2004 · N723CK · Boeing 7272H3 · Wing SparSDR 72300148Stringer · corrodedA 1 X 1 INCH AREA OF CORROSION ON STRINGER.Oct 28, 2004 · N723CK · Boeing 7272H3 · Fuselage Main, Longeron/StringerSDR 72300169Frame · corroded2 INCH BY 3 INCH AREA OF CORROSION ON FRAME WEB.Oct 28, 2004 · N723CK · Boeing 7272H3 · Fuselage Main, FrameSDR XNOA1204Position Switch · out of adjustNR 6 LED FAILED TO RETRACT. ADJUSTED NR 6 LEADING EDGE FLAP POS SWITCH IAW MM CH. 27-82-11.Oct 27, 2004 · N76753 · Boeing 727227 · Leading Edge Slat Position Indicating SystemSDR XNOA1205Switch · damagedNR 6 LED FAILED TO RETRACT AFTER T/O. FOUND PUSHED PIN AT NR 6 LED FLAP POS SWITCH. RESEATED PIN IAW MM CH. 20-11-07. OPS CHECKS GOOD IAW MM CH. 27-82-11.Oct 27, 2004 · N76753 · Boeing 727227 · Leading Edge Slat Control SystemSDR 72300077Keelbeam · corroded1.5 INCH BY 2.5 INCH AREA OF CORROSION ON BOTH SIDES OF KEEL BEAM EXTENSION.Oct 27, 2004 · N723CK · Boeing 7272H3 · Fuselage Main, KeelSDR 72300078Keelbeam · corroded2 INCH BY 2.5 INCH AREA OF CORROSION ON BOTH SIDES OF KEEL BEAM EXTENSION.Oct 27, 2004 · N723CK · Boeing 7272H3 · Fuselage Main, KeelSDR 0401939153Pulley · wornON FINAL APPROACH FOR LANDING AFTER SELECTING FLAPS TO 30 DEGREES DOWN, THE CREW FELT A SLIGHT ROLL AND NOTICED THAT THE LT FLAP INDICATOR WAS AT 20 DEGREES AND THE RT FLAP INDICATOR WAS AT 30 DEGREES. CREW EXECUTED MISSED APPROACH PROCEDURES TO ALLOW TIME FOOct 26, 2004 · N8912E · Doug DC914 · Trailing Edge Flap Control SystemSDR 72300028Stringer · corrodedCORROSION ON STRINGER BETWEEM BS 670 AND 720.Oct 26, 2004 · N723CK · Boeing 7272H3 · Fuselage Main, Longeron/StringerSDR 72300062Skin · corroded1 INCH BY 1 INCH AREA OF CORROSION ON SKIN DOUBLER.Oct 26, 2004 · N723CK · Boeing 7272H3 · Fuselage Main, Plate/SkinSDR 72300011Shear Tie · corroded.5 INCH BY 2 INCH AREA OF CORROSION ON SHEAR TIE.Oct 26, 2004 · N723CK · Boeing 7272H3 · Fuselage Internal Mounting StructureSDR 72300013Shear Tie · corrodedCORROSION ON SHEAR TIE.Oct 26, 2004 · N723CK · Boeing 7272H3 · Fuselage Internal Mounting StructureSDR 72300190Frame · corrodedTWO 3 X 3 INCH AREAS OF CORROSION.Oct 26, 2004 · N723CK · Boeing 7272H3 · Fuselage Main, FrameSDR 72300049Stringer · corroded.5 INCH BY 1 INCH AREA OF CORROSION IN CENTER OF S-26R.Oct 25, 2004 · N723CK · Boeing 7272H3 · Fuselage Main, Longeron/StringerSDR 72300005Shear Tie · corroded1 INCH BY 2.5 INCH AREA OF CORROSION ON SHEAR TIE.Oct 25, 2004 · N723CK · Boeing 7272H3 · Fuselage Internal Mounting StructureSDR 72300009Shear Tie · cracked2 INCH CRACK IN SHEAR TIE RADIUS.Oct 25, 2004 · N723CK · Boeing 7272H3 · Fuselage Internal Mounting StructureSDR 72300222Shear Tie · crackedCRACK IN SHEAR TIE RADIUS.Oct 25, 2004 · N723CK · Boeing 7272H3 · Fuselage Internal Mounting StructureSDR 72300032Frame · corroded1 INCH BY 1 INCH AREA OF CORROSION ON FRAME.Oct 24, 2004 · N723CK · Boeing 7272H3 · Fuselage Main, FrameSDR 72300044Stringer · corroded1 INCH BY 10 INCH AREA OF CORROSION ON BOTTOM OF STRINGEROct 24, 2004 · N723CK · Boeing 7272H3 · Fuselage Main, Longeron/StringerSDR 72300006Shear Tie · corroded1 INCH BY 4 INCH AREA OF CORROSION ON SHEAR TIE.Oct 24, 2004 · N723CK · Boeing 7272H3 · Fuselage Internal Mounting StructureSDR 72300007Shear Tie · cracked1 INCH CRACK IN PREVIOUS SHEAR TIE REPAIR ANGLE RADIUS.Oct 24, 2004 · N723CK · Boeing 7272H3 · Fuselage Main, Attach FittingsSDR 72300010Shear Tie · corroded1.25 INCH BY 3 INCH AREA OF CORROSION ON BOTTOM OF SHEAR TIE.Oct 24, 2004 · N723CK · Boeing 7272H3 · Fuselage Internal Mounting StructureSDR 72300131Stringer · corrodedA 5 X 2 INCH AREA OF CORROSION ON STRINGER.Oct 24, 2004 · N723CK · Boeing 7272H3 · Fuselage Main, Longeron/StringerSDR 72300004Shear Tie · corroded.75 INCH BY 3 INCH AREA OF CORROSION ON SHEAR TIE.Oct 23, 2004 · N723CK · Boeing 7272H3 · Fuselage Internal Mounting StructureSDR 72300027Stringer · corrodedCORROSION ON BOTTOM OF S-24 LT.Oct 21, 2004 · N723CK · Boeing 7272H3 · Fuselage Main, Longeron/StringerSDR 72300058Frame · crackedCRACKED FRAME UPPER FLANGE 1 INCH IN LENGTH.Oct 21, 2004 · N723CK · Boeing 7272H3 · Fuselage Main, FrameSDR 72300059Attach Fitting · corrodedCORROSION IN BORE OF LT STAB HINGE BEARING LUG.Oct 21, 2004 · N723CK · Boeing 7272H3 · Vertical StabilizerSDR 72300060Attach Fitting · corrodedCORROSION IN BORE OF RT STAB HINGE BEARING LUG.Oct 21, 2004 · N723CK · Boeing 7272H3 · Vertical Stabilizer
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