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 DHLA200700057Pump · failedAT START OF TAKEOFF, 1.4 EPR NR 2 ENGINE FAILED COMPLETED ABNORMAL PROCEDURE. REPLACED NR 2 ENG FUEL PUMP IAW PRATT AND WHITNEY JT8D M/M GROUND RAN AND LEAK CK GOOD AT THIS TIME IAW 73-11-01. PERFORMED MPA RUN PER JRH 7.7.SDR CA071010006Turbine Wheel · failed(CAN) AT THE RUNWAY THRESHOLD THE FLIGHT CREW ADVANCED THE THROTTLES TO 1.2 EPR, STABLE ENGINES WERE CALLED. ADVANCED THRUST LEVERS AND APPROACHING TAKEOFF THRUST, BEFORE REACHING APPROXIMATELY 20 KTS, A LOUD BANG AND VIBRATION OCCURRED. THE FLIGHT CREW REJECTSDR TSAA0773051Fuel Control · failedNON-ETOPS FLIGHT 90 HNL-KOA, ON TAKEOFF ROLL, THE CREW NOTED THE NR 2 EGT CLIMBING FASTER THAN THE NR 1 EGT. ABORTED THE TAKEOFF AT 100 KTS INDICATED AIRSPEED DUE TO NR 2 ENGINE HIGH EGT. THE CREW RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE CSDR 9182007Hose · damagedNR 1 ENGINE STRUT OVERHEAT LIGHT CAME ON IN CLIMBOUT 6000 FT. LIGHT WENT OUT ON REDUCING POWER TO 1.4 EPR. THE AIRCRAFT RETURNED TO MIA. THE THRUST REVERSER FLEXIBLE HOSE WAS FOUND DAMAGED. THE HOSE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.SDR 07FDEA03235Engine · failedFL350, FELT VIOLENT SHUDDER, NR 2 EGT MAXED OUT, OIL PRESS DROPPED TO APPROX 15 PSI. SHUTDOWN ENG AND EGT DROPPED. NO FIRE INDICATIONS. REMOVED AND REPLACED NR 2 ENG PER FEDEX ENG CHANGE W/C. OPS AND LEAK CHECK OK RII:226917.SDR PCSA818200701Engine · malfunctionedFLIGHT 861 DEPARTED SJU AND DURING THE TOP OF THE CLIMB THE CREW REPORTED THE NUMBER 1 ENGINE OIL PRESSURE DROPPED TO ZERO, THE NUMBER 1 ENGINE WAS SHUTDOWN AND THE AIRCRAFT CONTINUED TO MIA AND LANDED WITHOUT INCIDENT. THE NUMBER 1 ENGINE WAS REMOVED AND REPSDR ABXA070253Engine · malfunctionedRIGHT OIL STRAINER CLOGGING ANNUNCIATOR ILLUMINATED IN FLIGHT. SECURED RIGHT ENGINE. REPLACED RIGHT ENGINE IAW JOB CARD 9090010, W/O 60027628.SDR SROM200700005Casting · brokenDURING TAKEOFF, AT APPROXIMATELY 300 FEET, CREW EXPERIENCED NR 2 ENGINE COMPRESSOR STALL WITH RAPIDLY RISING EGT. SHUTDOWN NR 2 ENGINE AND MADE UNEVENTFUL LANDING AT DEPARTURE AIRPORT. INSPECTION REVEALED THE NOSE DOME HAD SEPARATED FROM ITS MOUNT DAMAGING THESDR GAIA07007Light · inoperativeNO FLIGHT: THE COCKPIT DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED EMERGENCY COCKPIT LIGHT. OPS CHECK NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. (K)SDR CA070717017Nut · loose(CAN) ON APPROACH, CREW SELECTED FLAPS FROM 2 TO 5 AND HAD AN AMBER LIGHT INDICATION FOR THE NR 1 KRUGER FLAP INDICATING STILL RETRACTED. FELT MODERATE VIBRATION AND DECLARED AN EMERGENCY. UNEVENTFUL LANDING. MAINTENANCE CYCLED SYSTEM AND COULD NOT FAULT. FUSDR CA070608007Bypass Valve · failed(CAN) ON ARRIVAL, THE IB FLAPS FAILED TO EXTEND WHEN LANDING, CONFIGURATION SELECTED. THE CREW ELECTED TO DIVERT. THE AIRCRAFT COMPLETED A NORMAL LANDING. MAINTENANCE WAS UNABLE TO DUPLICATE THE PROBLEM AND INSPECTED THE SYSTEM FOR LEAKS AND ANOMALIES. THE FLASDR CA070515003Tube · chafed(CAN) IB, HYDRAULIC A SYS PRESSURE WAS NORMAL ON APPROACH AND QUANTITY REPORTED APPROXIMATELY ZERO. UPON SELECTION OF FLAPS, QUANTITY READ ZERO AND LOW PRESSURE LIGHTS ILLUMINATED. FLIGHT CREW DECLARED AN EMERGENCY AND THE HYDRAULIC FAILURE CHECKLIST WAS CARRISDR CA070424007Blade · failed(CAN) DURING TAKEOFF ROLL AT 80KTS, THE TOWER ADVISED THE CREW THAT FLAMES WERE VISIBLE OUT OF ONE OF THE ENGINES. THE CREW REJECTED THE TAKEOFF AND ENGINES WERE SHUTDOWN. THE AIRCRAFT WAS TOWED BACK TO THE RAMP. MAINTENANCE INSPECTED THE ENGINES AND FOUND NSDR CA070427006Attach Bracket · cracked(CAN) DURING A AND B5 INSPECTION NR 7 SLAT ATTACH BRACKET UPPER MOUNT ON FRONT SPAR CRACKED. P/N TO BE DETERMINED FROM MFG ENGINEERING DRAWINGS. RDA ISSUED BY DECA ENGINEERING TO REPAIR. (TC NR 20070427006)SDR ABXA070091Power Supply · defectiveEMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW MM 33-53-02-4.SDR CA070413002Cylinder · failed(CAN) THE CREW OBSERVED AN A SYSTEM DEPLETION CONDITION AFTER EXTENDING THE LANDING GEAR. THE AIRCRAFT LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THE NOSE LANDING GEAR SYSTEM TRANSFER CYLINDER HAD FAILED. THE CYLINDER HAD FAILED AT THE LAST END CAP THRESDR ABXA070090Battery · dischargedEMERGENCY LIGHTS WOULD NOT STAY ON. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW MM 33-53-00.SDR KNNA200700019Frame · cracked3 INCH CRACK OVER BODY STATION 360 FRAME BETWEEN STRINGERS 23 TO 22. REPAIR IS IN PROGRESS IN ACCORDANCE WITH SERVICE BULLETIN B737-53A1064 AND DRAWING NUMBER 65C23267.SDR 07FDEA01167Angle · crackedAIR STAIRS AREA LT SIDE, STA 1342 INBD DUCT SUPPORT ANGLE IS CRACKED LOWER END AT LBL 40. REMOVED AND REPLACED LT SIDE STA 1342 IB DUCT SUPPORT ANGLE REF SRM 51-30-02 PAGE 1.SDR 07FDEA00537Oil System · unknownNR 1 ENG OIL QUANTITY BEGAN TO DECREASE SHORTLY AFTER T/O WITH ASSOCIATED NOTICEABLE DECREASE IN OIL TEMP, (OUT OF LIMITS) PRECAUTIONARY ENGINE SHUTDOWN. OIL QTY DECREASED TO BELOW 1 GAL. AFTER SHUTDOWN OIL QTY ROSE AGAIN TO 4 GALS. DUE TO THE FACT THAT THESDR 07FDEA00480Engine · damagedAFTER TAKEOFF AT 1000 FT, CREW FELT A VERY PRONOUNCED THUMP ACCOMPANIED BY A LOUD NOISE. AUTO PACK TRIP ILLUMINATED. ENGINE INSTRUMENTS CHECKED NORMAL. WHILE TROUBLESHOOTING THE PROBLEM AND CLIMBING THROUGH 18,000FT. ANOTHER LOUD THUMP AND NOISE OCCURRED SDR CA070213003Contact · burned(CAN) DURING CLIMB OUT ALL 4 CB`S POPPED FOR TANK 2 FUEL BOOST PUMPS, AIRCRAFT RETURNED TO AIRPORT. DETERMINED NR 3 GENERATOR VOLTAGE FLUCTUATING, (THE PUMP FAULT WAS ATTRIBUTED TO THE POWER FLUCTUATION WHICH WAS POWERING THE (ESSENTIAL POWER) AND THE (SYNC BUSDR ABXA070035Engine · damagedFLIGHT 509, ILN - JAX, AT CRUISE POWER SETTING, LEFT EPR HAD SUDDEN DROP OF .4 EPR. LOUD POPPING SOUND. MODERATE VIBRATION, THROTTLED BACK, VIBRATION WORSENED. SHUT LEFT ENGINE DOWN. AIRCRAFT LANDED WITHOUT INCIDENT AT JAX. FOUND TURBINE DAMAGED. REMOVEDSDR 0700219953Compressor · stalledDURING TAKEOFF ROLL, AT APPROXIMATELY 100KTS, NR 1 ENGINE COMPRESSOR STALLED. TAKEOFF WAS ABORTED AND THE AIRCRAFT SKIDDED OFF THE RUNWAY. THE AIRCRAFT IS BEING REPAIRED AND THE NR 1 ENGINE IS BEING REPLACED.SDR SROM200700001Duct · rupturedUPON TAKEOFF A POP WAS WAS HEARD FOLLOWED BY PERCEIVED SMOKE (DUST) IN THE CABIN. PACS WERE SELECTED TO OFF AND A IMMEDIATE LANDING MADE AT THE DEPARTURE AIRPORT. ALL COCKPIT INDICATIONS NORMAL. FOUND LT AIR CONDITIONING PAC MIXING CHAMBER AND HOT AIR SUPPLSDR BMAC06013Csd · overspeedAN ELECTRICAL MALFUNCTION OCCURRED CAUSED BY THE NR 1 AC GEN ISOLATED THE (3) BUS TIES AND DISCONNECTED THE NR 1 CSD. ALSO, NOTED ALL (8) BOOST PUMP CB'S HAD OPENED. MAINT DEFERRED THE NR 1 GEN AND CSD. LATER REPLACED NR 1 AC GEN AND CSD, OPS CHECKED GOOSDR SROM200600022Carriage · crackedDURING ROUTINE ACCOMPLISHMENT OF ULTRASOUND INSPECTION OF THE SPINDLES ON THE OB FLAPS IAW AD 2003-24-08 FOUND THE RT IB SPINDLE TO SHOW A CRACK INDICATION. LAST ULTRASONIC INSPECTION PERFORMED 46 CYCLES AGO. REPLACED SPINDLE AND CARRIAGE ASSEMBLY WITH NEW PSDR USAABB06088Wire · damagedMAINTENANCE FOUND EMERGENCY LIGHTS INOPERATIVE IN THE FIRST CLASS CABIN AREA, RT SIDE. ALSO FOUND INOPERATIVE EMERGENCY LIGHTS MID LT CABIN. WIRING REPAIRS WERE ACCOMPLISHED TO BOTH SECTIONS. NO FURTHER FAULTS NOTED.SDR CA061219003Disc · detached(CAN) WHILE TOWING AIRCRAFT TO LINE IT WAS REPORTED THAT NR 1 BRAKE WAS TRYING TO LOCK UP. UPON REMOVAL OF BRAKE ASSEMBLY THE DISC RING WAS FOUND DETACHED FROM THE ASSEMBLY. A RIVET WAS FOUND SHEARED AND THE DISC RING CAME APART. FURTHER TO FOLLOW AFTER STRIPSDR 06FDEA03986Seat Track · corrodedEXPANSION LINK, BS 740-760, LBL 45 CORRODED AROUND FWD ATTACH BOLT. REMOVED AND REPLACED EXPANSION LINK BS 740-760 LBL 45 IAW SRM 53-10-1.SDR 06FDEA03932Shear Tie · corrodedAFT CARGO BAY CORROSION ON SHEAR TIE BS 1148 LBL 16. REMOVED AND REPLACED SHEAR TIE AT BS 1148 LBL 16 IAW SRM 53-10-4.SDR 06FDEA03933Shear Tie · corrodedAFT CARGO BAY CORROSION ON SHEAR TIE BS 1148 LBL 10. REMOVED AND REPLACED SHEAR TIE BS 1148 LBL 10 IAW SRM 53-10-4.SDR 06FDEA03934Shear Tie · corrodedAFT CARGO BAY CORROSION ON SHEAR TIE BS 1148 LBL 3. REMOVED AND REPLACED SHEAR TIE BS 1148 LBL 3 IAW SRM 53-10-4.SDR 06FDEA03935Floorbeam · damagedDRILL START IN UPPER CHORD OF BS 870 FLOORBEAM AT LBL 50, WL 208. REPAIRED BS 870 FLOORBEAM AT LBL 50, WL 208 IAW FED EX EA 7-5310- 105909.SDR 06FDEA03931Frame · dentedFRAME FLANGE DENTED STA 680 STR 23L - 25L. REMOVED DAMAGE ON FRAME BS 680 STR 23L-25L AND IAW SRM 51-40-3.SDR 06FDEA03936Frame · damagedFWD CARGO COMPARTMENT, DAMAGE TO STA 520 FRAME BETWEEN STR 22L AND 25L. REMOVED DAMAGE ON FRAME BS 520 BETWEEN STR 22L AND 25L AND REPAIRED IAW SRM 53- 10-1.SDR TSAA0629097Transmitter · failedNON-ETOPS FLT 68 HNL-ITO: DURING CLIMB, THE CREW NOTED THAT THE HYDRAULIC A-SYSTEM PRESSURE GAUGE READ 800 PSI. THE CREW RETURNED TO FIELD AND LANDED IN WITHOUT FURTHER INCIDENT. MAINTENANCE PLACED THE HYDRAULIC A-SYSTEM PRESSURE INDICATION ON MEL 29-3-1. AIRSDR DHL2006780007Skin · crackedNR 077407, LT WING TIP UPPER SURFACE, WBL 638, AFT OF NAV LIGHT LENS COVER, PREVIOUS REPAIR CRACKED. REMOVED PREVIOUS REPAIR IAW SRM 51-30-2. FAB DOUBLER FROM 7075-T6, 0.050, PO NR 6149108, DIM. 4 BY 3. FILLER FROM 7070-T6 0.040, PO NR 9003839, DIM. 2.50 BY SDR 06FDEA03817Skin · gougedWHILE WORKING CUSTOMER CARD NR N00224, FOUND OUT OF LIMITS GOUGE IN EXTERIOR SKIN BS 538 1.5 INCH BELOW STR 25 RT. REMOVED DAMAGE IN EXTERNAL SKIN BS 538 BELOW STR 25R AND REPAIRED IAW SRM 53-30-3 FIG 1.SDR 06FDEA03818Skin · corrodedCORROSION ON WING LOWER SKIN SURFACE, AT NR 2 AFT FLAP TRACK MOUNT. REMOVED CORROSION ON WING LWR SURFACE AT NR 2 FLAP TRACK MOUNT AND REPAIRED IAW FED EX EA 7-5710-100598.SDR 06FDEA03819Flap Track · corrodedNR 2 FLAP TRACK, AFT MOUNT HOLE IS CORRODED. REMOVED AND REPLACED NR 2 FLAP TRACK IAW FED EX W/C 27X5706-03.SDR ASAA0611156Start Valve · stuckNR 2 START VALVE OPEN LIGHT CAME ON DURING CLIMBOUT. SHUT DOWN NR 2 ENGINE. REPLACED NR 2 ENGINE STARTER VALVE.SDR 06FDEA03683Floorbeam · corrodedFOUND CORROSION ON LONGITUDINAL FLOORBEAM AROUND NUTPLATE HOLES, LBL 25, BS 760 THROUGH 848, WL 208. REPLACED LONGITUDINAL FLOOR BEAM IAW SRM 53-10-1, 51-30-5 AND 51-30-2.SDR 06FDEA03684Floorbeam · corrodedFOUND LONGITUDINAL FLOORBEAM CORRODED AT NUTPLATE HOLES, RBL 45, BS 823 - 848, WL 208. FOUND CORROSION OUT OF LIMITS ON FLOOR BEAM IAW SRM 53-10-1 FIG 8 AND SRM 51-10-6. REMOVED AND REPLACED BEAM IAW SRM 51-30-2 AND SRM 51-30-5.SDR 06FDEA03685Floorbeam · corrodedFOUND LONGITUDINAL FLOORBEAM CORRODED AT NUTPLATE HOLE, RBL 45, BS 782, WL 208. LONGITUDINAL FLOORBEAM WAS REPLACED ON N01170.SDR 06FDEA03628Tire · unknownREJECTED TAKEOFF 40-50 KTS, DUE TO AIRCRAFT SHUDDER SUSPECTED COMPRESSOR STALLS. NO ABNORMALS NOTED ON ANY ENGINES AFTER THROTTLES RETARDED. RAN APPROPRIATE QRH PROCEDURES. INSPECTED ENG'S FOR HIGH PWR STALL IAW MM 71-00-000-6 1 WITH NO FAULTS FOUND. DUSDR 06FDEA03632Frame · crackedFRAME AT BS 1352 INNER STRUCTURE CRACKED AT 8:00 POSITION FOUND UPON REMOVAL OF OUTER CHORD. REPAIRED INNER STRUCTURE ON FRAME STA 1352 IAW SRM 51-40-3.SDR 06FDEA03633Indicator · malfunctionedON T/O ROLL F/O'S AIRSPEED INDICATION ON THE PFD DID NOT BREAK UNTIL THE THE CAPTAINS AIRSPEED REACHED 70KTS. (30 KT DIFFERENCE) IN WORK.SDR ABXA060280Control Box · defectiveRT MAIN GEAR UNSAFE LIGHT WITH ASSOCIATED RT LANDING GEAR GREEN LIGHT. ALTERNATE MAIN GEAR INDICATION OPERATES NORMAL. REPLACED PROXIMITY SWITCH CONTROL BOX IAW MM 32-60-01-2.SDR 06FDEA03605Structure · vibrationIN CLIMB THRU FL190 (300 KNOTS) A-FRAME BUFFET. CYCLED SPEED BRAKE (NO HELP). DISCONNECTED A/P AND SLOWED TO 280 KNTS WITH CONTINUAL BUFFET. AT FL 240 A-FRAME BUFFET STOPPED, VIBRATION IN NR 1 THROTTLE.
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