Pratt & Whitney JT8D-15
Service difficulty reports · 2,710
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 = 'JT8D15' 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 = 'JT8D15' 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 249TR0033Control Unit · inoperativeAUTO THROTTLE INOPERATIVE. REPLACED PDC CDU IAW MM 34-18-21 AND OPS CHECKED IAW MM 34-18-21 AND 22-31-01.SDR 2004F00316Line · overtorquedDURING CRUISE FLIGHT, ENGINE NR 3 OIL QUANTITY WENT OT ZERO FOLLOWED BY A LOSS OFF OIL PRESSURE AND INCREASE IN OIL TEMP. ACCOMPLISHED PRECAUTIONARY ENGINE SHUT DOWN PROCEDURE AND DIVERTED TO SVMI. LANDED WITH NO INCIDENT, TROUBLESHOOT AND FOUND OVERTIGHTENESDR CA040812001B-Nut · cracked(CAN) CREW REPORTED 'A' SYSTEM HYDRAULIC FLUID LOSS IN FLIGHT. MAINTENANCE FOUND LEAK AT B-NUT END FITTING AT 'A' SYSTEM MODULE. LINE REPLACED.SDR ABXA040270Engine · defectiveLEFT ENGINE LOW OIL QUANTITY 0, LOW OIL PRESSURE 35 PSI, OIL PRESSURE LIGHT ON, SHUT DOWN LEFT ENGINE. FROM PDX, MADE DIVERSION TO YAK. REMOVED AND REPLACED LEFT ENGINE IAW DC-9 JOB CARD 9090010 ON WP 600204098. OPS CHECKED GOOD IAW DC-9 MM.SDR DHL2004749006Light · inoperativeON FORWARD INSTRUMENT PANEL, LE FLAPS INDICATOR HAS RT LIGHT INOP. EMERGENCY EXIT LIGHT OVER L-1 DOOR WILL NOT ILLUMINATE. REMOVED AND REPLACED LIGHT BULB, OPS CK GOOD IAW BMM CH 33-10-0, P/N 327. REMOVED AND REPLACED LIGHT ASSY, OPS CK GOOD IAW BMM CH 33-50SDR AWXA200400802Warning Light · false indicationFALSE FIRE WARNING ON CLIMB OUT, AFTER SELECTING FLAPS UP RECEIVED FWD CARGO FIRE LIGHT AND FIRE BELL, DISCHARGED NR 1 CARGO FIRE BOTTLE AND LIGHT EXTINGUISHED, DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. MAINT MET AC AND PERFORMED A MAINT BITE TEST SDR DL73S040676Floorbeam · crackedSTA 520 FLOORBEAM CRACKED IN RADIS. REPAIR IAW ERA 091543-14.SDR CA040722002Bolt · shearedWHEN THIRD PARTY AMO WAS INSPECTING THE FWD STABILIZER FITTINGS ATTACHED TO THE AFT SPAR FOR SB737-57A1266 ON A/C 743 FOUND THE O/B FITTING CRACKED. ON FURTHER INVESTIGATION, FOUND THAT ALL FOUR BOLT HEADS ON THE AFT O/B FITTING WERE SHEARED OFF, AND THE FITTSDR DHL2004749005Overheat Loop · malfunctionedLOWER AFT BODY OVERHEAT DOES NOT TEST. RESEATED AND CYCLED SYSTEM POWER ON OVERHEAT DETECTION SYSTEM BOX. REF B727 M/M 26-14-000. TESTED LOWER AFT BODY OVERHEAT, OPS CHECKS NORMAL.SDR C8GA20040011Pitot Line · obstructedDURING TAKE-OFF ROLL, UNABLE TO REACH TARGET TAKE-OFF EPR SETTING ON NR 1 ENGINE. ABORTED TAKE-OFF AND RETURNED TO BLOCKS. UPON RETURNED TO BLOCKS, TROUBLESHOOT THE EPR SYSTEM AND FOUND THE PT-2 INLET OBSTRUCTED. CLEARED OBSTRUCTION BUT EPR READING CONTINUES ISDR SPAA0400070Battery Pack · inoperativeR2 DOOR EMERGENCY BATTERY PACK DOES NOT OPERATE. REPLACED R2 DOOR EMERGENCY BATTERY PACK IAW BMM 33-51-101, OPERATIONAL CHECK GOOD.SDR RIV2004F00000Actuator · leakingFLIGHT CREW WAS UNABLE TO EXTEND THE RT MLG ON AC. DURING INITIAL APPROACH, THE APPROACH WAS ABORTED AND THE CREW ALLEGEDLY ACCOMPLISHED ALL APPROPRIATE CHECKLIST ITEMS. THE RT MLG WOULD STILL NOT EXTEND USING THE MANUAL EXTENSION SYSTEM, ( THE GEAR APPEAREDSDR DHL2004746005Brake · malfunctionedBRAKES DRAGGING UNABLE TO DISENGAGE. T/S BRAKE SYST FOUND PNEUMATIC BRAKE HANDLE SLIGHTLY OFF DETENT STILL SAFETIED, BLED BRAKES, SAFETIED PNEUMATIC BRAKE HANDLE SYST. OPS CKD GOOD IAW MM 32-41-0.SDR COOSDR040010Keelbeam · corrodedAFT CARGO COMPARTMENT, STR 29L KEELBEAM, OB FLANGE CORRODED.SDR AWXA200400690Slide · unsafetiedDURING PRE-FLIGHT PREPARATION, INFLIGHT NOTICED L-2 DOOR SLIDE HAD AN UNUSUAL INSTALLATION. UPON FURTHER EVALUATION OF THE SITUATION, MAINTENANCE DETERMINED THAT THE DOOR SLIDE WAS NOT PROPERLY CONNECTED AND THE PIN HOLDING THE GIRT BAR ASSY TO THE SLIDE HAD SDR DHL2004754021Switch · out of adjustIN FLIGHT, RED "DOORS" LIGHT ON FWD PANEL ILLUMINATED WHEN GEAR HANDLE PLACED IN UP POSITION, LIGHT EXTINGUSHED INTERMITENT. UPON T/S, FOUND RT NOSE GEAR DOOR SWITCH OUT OF ADJUSTMENT. ADJUSTED SWITCH AND OPS CHECK GOOD IAW MM 32-62-11.SDR DHL2004754020Fusible Plug · meltedNR 3 MAIN TIRE FUSE PLUG MELTDOWN AT PARKING RAMP. NR 4 MAIN TIRE FUSE PLUG MELT DOWN AT PARKING RAMP. REPLACED NR 3 MAIN TIRE ASSY IAW MM 32-45-1. REPLACED NR 4 MAIN TIRE ASSY IAW MM 32-45-1.SDR DHL2004780005Indicator · intermittentRADAR PAINTS INTERMITTENT PICTURE IN ALL MODES. REMOVED AND REPLACED RADAR DISPLAY IAW B727 M/M 34-41-01. OPS CK GOOD ON GROUND.SDR AWXA200400660Turbine Blades · overheatedON TAKEOFF ROLL AT OAK EN ROUTE FOR LAS FELT A STRONG VIBRATION NR 1 ENGINE, REJECTED TAKEOFF AT 50 KTS AND PULLED OFF ONTO TAXIWAY WHERE EMERGENCY EQUIPMENT INSPECTED THE AIRCRAFT. TAXIED BACK TO GATE USING NR 2 ENGINE. MAINTENANCE REMOVED AND REPLACED NR 1SDR MYW2004F00006Generator · fluctuatesDURING TAKE OFF ROLL, GENERATOR DROPPED OFF LINE FOLLOWED BY NR 3 GEN LIGHT. REJECTED TAKE OFF AT 75 KNOTS. ACCOMPLISHED AOM PROCEDURE GENERATOR CHECKLIST ZA9-1 AND REJECTED TAKEOFF. RETURNED TO GATE WITHOUT INCIDENT. FOUND NR 3 GENERATOR FREQUENCY FLUCTUASDR AWXA200400580Battery · dischargedLAS - EEL - DURING 4-DAY CHECK THE L-1 AND R-1 DOOR EMERGENCY SLIDE LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK, OPERATIONAL CHECK WAS GOOD.SDR DHL2004780004Light · looseEMERGENCY EXIT LIGHT OVER FORWARD ENTRY REQUIRES REINSTALLATION. LIGHT WILL NOT STAY SECURED. RE-LAMPED AND REINSTALLED EMERGENCY EXIT LIGHT IAW M/M 33-50-91, OPS CHECKED GOOD. BULB P/N: 1315 (2 EA.)SDR AWXA200400577Battery · dischargedDEN - EEL - DURING 4-DAY CHECK THE OVERHEAD (CEILING) EMERGENCY EXIT LIGHT AT SEAT ROW 9 WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED CEILING MOUNTED EMERGENCY EXIT LIGHT BATTERY PACK AT BS 617, OPERATIONAL CHECK WAS GOOD.SDR FX72004F00001Warning Light · illuminatedNOSE GEAR UNSAFE LIGHTS ON FRONT AND F/E PANELS STAYED ON RETURNED WITHOUT INCIDENT. JACKED A/C AND PERFORMED GEAR SWING IAW MM. NLG SWING PERFORMES NORMALLY. AIRCRAFT RETURNED TO SERVICE WITHOUT FURTHER INCIDENTS.SDR CA040521008Sequence Valve · crackedAFTER T/O AND GEAR RETRACTION, CREW NOTICED HYDRAULIC QUANTITY LOW. CREW MONITORED HYDRAULIC LEVEL FOR DURATION OF FLIGHT WITH NO CHANGE. UPON GEAR EXTENSION, HYDRAULIC QUANTITY DROPPED FURTHER, REQUIRING THE A/C TO BE TOWED TO RAMP FROM THE ACTIVE TAXIWAY. SDR CA040521001Module · failed(CAN) ON CLIMB OUT, CREW NOTICED NOSE (GEAR UNSAFE) LIGHT DID NOT EXTINGUISH. AFTER DUMPING FUEL, CREW RETURNED TO MAINTENANCE FACILLITY WHERE THE LANDING GEAR ACCY UNIT WAS REPLACED AND GEAR SWINGS PERFORMED. A/C RETURNED TO SERVICE.SDR AUS20040438Door Frame · cracked(AUS) NR 1 CARGO DOOR FRAME CRACKED IN AREAS ADJACENT TO DOOR STOP NR 5 AND NR 6. FOUND DURING INSPECTION IAW AD/B727/165 AND MFG SB727-53A0219.SDR FX72004F00000Valve · defectiveNR 2 ENGINE SHUT-DOWN DURING FLIGHT DUE TO HIGH OIL TEMP IN YELLOW ARC. TROUBLESHOT AND FOUND FUEL HEAT VALVE OPEN. CLOSED MANUALLY AND SAFETY WIRED SHUT. RAN ENGINE ALL PARAMETERS NORMAL AND AIRCRAFT RETURNED TO SERVICE WITH FUEL HEAT VALVE ON DMI. NO FURSDR AUS20040376Bearing · seized(AUS) IB FLAP SELECTOR VALVE INPUT ROD SELF ALIGNING BEARING BINDING DUE TO LACK OF LUBRICATION.SDR GAIA04071Coupler · malfunctionedDEPARTURE, FLIGHT, WITH AIRSPEED CHANGES, AIRCRAFT YAW CHANGES NOTICEABLY. AFTER RUDDER IS RETRIMMED AIRCRAFT DUTCH ROLLS A FEW TIMES IN A JERKING MANNER. WITH INCREASING SPEEDS MORE RT TRIM IS REQUIRED. CREW RETURNED TO DEPARTURE AIRPORT, WHERE A LANDING WSDR CA040423009Quick Disconnect · leaking(CAN) AC LANDED, ON ROLL-OUT, WAS OBSERVED TO HAVE SMOKE ISSUING FROM UNDERSIDE OF AC. TOWER ADVISED CREW AND CALLED OUT AFF. RT MAIN GEAR WAS FULLY ENGULFED IN HEAVY SMOKE. SMOKE WAS BROUGHT UNDER CONTROL AND AC PASSENGERS AND CREW EVACUATED ONTO RUNWAY. MAISDR DHL2004752002Compressor · stalledREJECTED TAKEOFF FOR INFORMATIONAL PURPOSES ONLY WT=152,000 LBS, TEMP=12.6, PRESS ALT=SEA LEVEL, AIRSPEED=60 KNOTS. SUSPECTED COMPRESSOR STALL WITH AN AUTO PACK TRIP. WIND WAS 89 AT CROSSWIND AT 10 KNOTS. ALSO FOR INFORMATIONAL PURPOSES ONLY. INSPECTED ENGSDR 04FDEA00849Duct · crackedCOMPLY WITH EA 7-7254-77153 ENGINE - FAN EXHAUST OUTER DUCT NR 6 OIL SUPPLY TUBE EGRESS BOSS WELD REPAIR. COMPLIED WITH EA 7-7254-77153 ENGINE - FAN EXHAUST OUTER DUCT NR 6 OIL SUPPLY TUBE EGRESS BOSS WELD REPAIR AT MAE.SDR DL73S040314Engine · malfunctionedABORTED T/O DCA DUE TO NR 2 ENG EPR HUNG AT 1.6, N1, N2, EGT, FF LOWER THAN NR 1. CLEARED RUNWAY, RAN ENG TO FULL POWER OK. SUSPECT CROSSWIND FOR THE LEFT AFFECTED NR 2. DID STATIC RUNUP PRIOR TO 2ND T/O, NR 2 SLOWER TO ACCEL TO T/O THAN NR 1, BUT DID REACHSDR CA040401008Bearing · contaminated(CAN) WHILE LANDING THE FLIGHT CREW NOTICED A SHIMMY IN THE LANDING GEAR. BELIEVING THAT THEY HAD BLOWN A TIRE, THEY STOPPED ON A TAXIWAY AND CONTACTED MAINTENANCE. MAINTENANCE DROVE TO THE AIRCRAFT AND INSPECTED THE LANDING GEAR. FINDING NO OBVIOUS FAULTS, MSDR AUS20040211Nut · missing(AUS) RT IB FLAP CARRIAGE DEAD WEIGHT ROLLER NUT AND LOCK WASHER MISSING. BOLT WAS STARTING TO MIGRATE FROM POSITION. SUSPECT CAUSED BY FAILURE OF LOCK WASHER TAB.SDR 2004F00287Line · leakingON CLIMB-OUT FROM MEM, NR 2 ENGINE OIL PRESSURE DROPPED TO 12 PSI. FOLLOWED AOM ABNORMAL PROCEDURES 2-A-19-10. SHUT DOWN NR 2 ENGINE AND RETURNED TO MEM. TROUBLESHOT NR 2 ENGINE. DISCOVERED OIL LINE BETWEEN FUEL OIL COOLER AND GEAR BOX CHAFING WITH OIL PRESDR AUS20040179Panel · faulty(AUS) SMOKE AND BURNING ODOR COMING FROM TOP SECTION OF P18 CIRCUIT BREAKER PANEL.SDR CA040315010Collar · worn(CAN) THE TAKE-OFF WAS REJECTED AT 70KTS DUE TO NLG SHIMMEY. BOTH NLG WHEELS REPLACED AND STEERING COLLAR ADJUSTMENT CHECKED. AIRCRAFT WAS RETURNED TO SERVICE.SDR AUS20040157O-Ring · failed(AUS) HYDRAULIC SYSTEM A PRESSURE MODULE SUPPLY LINE O-RING SEAL FAILED. LOSS OF HYDRAULIC FLUID.SDR 04FDEA00525Engine · vibrationEXCESSIVE VIBRATION AND GRINDING SOUND ON NR 3 ENG POWER LEVER, INCREASES WITH SPEED AND ALTITUDE. ENGINE NR 3 USED 1 GALLON OF OIL DURING THE 1 HOUR PLUS 15 MIN FLIGHT. C/W ENGINE BORESCOPE PER W/C 7200-5005. NO DEFECTS NOTED.SDR 237TR0002Transmitter · inoperativeDURING TAKE OFF AT 90KTS. NR 1 ENGINE OIL PRESSURE DROPPED SLOWLY OUT OF THE GREEN ARC TO MID YELLOW. T/O ABORTED. OIL PRESSURE STABILIZED AT THE BOTTOM OF THE YELLOW ARC. 35PSI AT IDLE. REPLACED NR 1 ENGINE OIL PRESSURE TRANSMITTER IAW MM. OPS AND LEAK CHSDR P762004F00000Bracket · crackedLT NR 3 ELEVATOR BALANCE PANEL AREA. FORWARD BRACKET THAT HOLDS THE FORWARD HINGE ATTACH POINT. STIFFENER BRACKETS AND ANGLES CRACKED AND BENT.SDR P762004F00001Bracket · crackedLT NR 3 ELEVATOR BALANCE PANEL AREA. FORWARD BRACKET THAT HOLDS THE FORWARD HINGE ATTACH POINT. STIFFENER BRACKETS AND ANGLES CRACKED AND BENT.SDR P762004F00002Bracket · crackedLT NR 3 ELEVATOR BALANCE PANEL AREA. FORWARD BRACKET THAT HOLDS THE FORWARD HINGE ATTACH POINT. STIFFENER BRACKETS AND ANGLES CRACKED AND BENT.SDR P762004F00003Bracket · crackedLT NR 3 ELEVATOR BALANCE PANEL AREA. FORWARD BRACKET THAT HOLDS THE FORWARD HINGE ATTACH POINT. STIFFENER BRACKETS AND ANGLES CRACKED AND BENT.SDR P762004F00004Bracket · crackedLEFT NR 3 ELEVATOR BALANCE PANEL AREA. FORWARD BRACKET THAT HOLES THE FORWARD HINGE ATTACH POINT. STIFFENER BRACKETS AND ANGLES AND CRACKED AND BENT.SDR DHL2004780002Lock · out of adjustFORWARD ENTRY DOOR LIGHT ILLUMINATED AFTER LANDING. PREVIOUS WRITE-UP ON LOG PAGE NR 370580. RII REQUIRED. ADJUSTED DOOR LOCK MECHANISM TO ROLL OVER CENTER PAST LOCK FURTHER LOCK AND LIGHT SYSTEM. OPS CHECKED NORMAL ON GROUND IAW MM 52-11-01.SDR AUS20040111Switch · out of adjust(AUS) MAIN CARGO DOOR NR 1 AND NR 7 LATCH INDICATOR MICROSWITCHES OUT OF ADJUSTMENT.SDR GAIA04009OPRelay · inoperativeDURING TAXI OUT, IT WAS DISCOVERED THAT THE TAKE OFF WARNING HORN WOULD NOT TEST. REMOVED AND REPLACED THE TIME DELAY RELAY. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
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