Pratt & Whitney JT8D-17
Service difficulty reports · 1,680
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 = 'JT8D17' 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 = 'JT8D17' 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 ASAA0510175Stringer Clip · corrodedAFT CARGO B-STA 747, STR 21L TIE CLIP CORRODED. REMOVED AND REPLACED TIE CLIP IAW SRM. (K)SDR ASAA0510176Stiffener · corrodedCORROSION FOUND ON VERTICAL STIFFENER LOCATED AT BS 328, RBL 14, WL 150, IN E AND E BAY. REMOVED AND REPLACED VERTICAL STIFFENER IAW SRM. (K)SDR ASAA0510177Splice · corrodedCORROSION ON STRINGER 26L END SPLICE AT BS 540. REMOVED AND REPLACED END SPLICE IAW SRM. (K)SDR ASAA0510178Skin · corrodedFUSELAGE SKIN BULGING AT BS 535, STR 28 LT KEELBEAM. KEELBEAM REPLACED AND SKIN REPAIRED. (K)SDR ASAA0510179Shear Tie · corrodedAFT CARGO PIT B-STA 807 IB OF STRINGER 27L FRAME TO SKIN SHEAR TIE AFT FACE CORROSION FOUND AS MARKED. REMOVED AND REPLACED SHEAR TIE IAW SRM. (K)SDR ASAA0510180Splice · corrodedFRAME SPLICE AT BSTA 847, STRINGER 27R FOUND CORRODED. FRAME SPLICE AT BSTA 847, STRINGER 27R REPLACED WITH MADE REPAIR PART IAW SRM. (K)SDR ASAA0510181Bracket · corrodedA BRACKET AT B-STA 847, STRINGER 18R FOUND CORROED. BRACKET REPLACED WITH THE REPAIR PART AT BSTA 847 STRINGER 18R IAW SRM. (K)SDR ASAA0510182Web · dentedDENT ON WEB ON LT WING RSS 497 APPROX 10 INCHES AFT OF REAR SPAR. REPAIRED IAW SRM. (K)SDR ASA0510184Door Frame · crackedDOOR FRAME ON FUSELAGE IS CRACKED (AFT END FWD FRAME. REPLACED IAW SRM. (K)SDR ASAA0510185Stringer · corrodedOB SIDE OF STR 26L AT B-STA 986 CORRODED. REMOVED AND REPLACED STRINGER 26L IAW SRM. (K)SDR ASAA0510138Keelbeam · corrodedKEELBEAM, BS 647-663 LT LWR CHORD CORROSION FOUND UPPER AND LOWER FACE. LT KEELBEAM REPLACED IAW SRM. (K)SDR ASAA0510141Stringer · corrodedSTRINGER CORRODED AT BS 967-986. REMOVED AND REPLACED STRINGER IAW SRM. (K)SDR ASAA0510143Frame · scratchedAFT CARGO PIT BS 787, RBL 8 HAS SCRATCHED FRAME. FOUND BEYOND LIMITS AND REPAIRED IAW SRM. (K)SDR ASAA0510154Stringer · crackedCRACKED STRINGER AT B-STA 789, STRINGER 26R. REMOVED AND REPLACED STRINGER IAW SRM. (K)SDR ASAA0510155Skin · mismanufacturedSKIN PANEL BETWEEN KEELBEAMS BSTA 727 TO S-STA 663 HAS LOW EDGE MARGIN AT FASTENER HOLES. REMOVED AND REPLACED PANEL IAW SRM. (K)SDR ASAA0510157Keelbeam · corrodedKEELBEAM B-STA 707-747 LT LOWER CHORD CORRODED. REMOVED AND REPLACED KEELBEAM IAW SRM. (K)SDR DHL2005741609Doubler · crackedMAIN CARGO DOOR CUTOUT SURROUNDING EXTERNAL DOUBLER HAS 3EA CRACKS AT STA: 561 (MATING SURFACE FOR MCD HINGE) TRIMMED-OUT 3.45 INCH X .440 INCH SECTION OF AEI-38 EXTERNAL SURROUND DOUBLER AT STA 561 TO REMOVE ALL 3 CRACKS IAW AEI EO 1448 FABRICATED FILLER FOSDR CA050620003Starter · separated(CAN) CREW REPORTED NR 2 ENGINE HEAVY VIBRATION, GAUGES FLUCTUATING, ENGINE SHUT DOWN. LANDED WITHOUT INCIDENT. UPON ARRIVAL, INSPECTION OF ENGINE FOUND THE STARTER WAS SEPARATED AT SPLIT LINE, CSO OFF PRESSURE FILTER POPPED. CSD QUAD RING BOLT LOOSE, OIL IN SDR ASAA0510118Keelbeam · corrodedCORROSION ON RT KEELBEAM AT B-STA 618. REPLACED KEELBEAM. (K)SDR ASAA0510127Bracket · corrodedAFT CARGO PIT B-STA 727B FRAME TO KEELBEAM (STA 27R) ATTACH ANGLE HAS CORROSION. REPLACED ATTACH ANGLE. (K)SDR ASAA0510128Attach Angle · corrodedAFT CARGO PIT B-STA 727B FRAME TO KEELBEAM (STA 27L) ATTACH ANGLE HAS CORROSION. REPLACED ATTACH ANGLE. (K)SDR C8GA20050014Fcu · contaminatedFLT 722 FROM TOL TO RDU. IN CRUISE AT FL310, CREW NOTED POWER LOSS OF NR 2 ENGINE ACCOMPANIED BY EPR FLUXUATION, COMPRESSOR STALL, AND VIBRATION. CREW REDUCED POWER SETTING TO IDLE AND PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN. THE AIRCRAFT RETURNED TO TOL ASDR ASAA0510111Support Angle · corrodedCORROSION FOUND ON SUPPORT ANGLE AT BAST 622 BETWEEN LT AND RT KEELBEAMS. REPLACED SHEAR TIE. (K)SDR ASAA0510112Support Angle · corrodedSUPPORT ANGLE CORRODED AT B-STA 520 RT KEELBEAM. REPLACED SUPPORT ANGLE. (K)SDR ASAA0510113Support Bracket · crackedBS 670 AT LT KEELBEAM SUPPORT BRACKET CRACKED. REPLACED SUPPORT BRACKET. (K)SDR ASAA0510114Keelbeam · corrodedKEELBEAM CORRODED AT B-STA 535, STR 28 RT. REPLACED KEELBEAM . (K)SDR ASAA0510115Skin · corrodedB-STA 597 TO B-STA 618 BETWEEN LT AND RT KEELBEAMS PANEL CORRODED. REPLACED KEELBEAM PANEL. (K)SDR ASAA0510105Keelbeam · damagedKEELBEAM WEB B-STA 702 LT ONE HOLE BELOW MINIMUM EDGE MARGIN. REPLACED STRUCTURE, LOW EDGE MARGIN AREA CUTOUT AND REPAIR ANGLE INSTALLED. (K)SDR ASAA0510107Keelbeam · corrodedKEELBEAM CORRODED B-STA 516 TO 535 STR 28L. REPAIRED WITH MADE REPAIR PART. (K)SDR ASAA0510108Stringer · crackedSTRINGER CRACKED AT B-STA 868, STR 25R. REPAIRED IAW SRM WITH MADE REPAIR PARTS. (K)SDR ASAA05101109Shear Tie · corrodedAFT CARGO PIT AND AFT SHEAR TIE HAS CORROSION AT B-STA 727A BETWEEN STR 27L AND 26L. SHEAR TIE REPLACED. (K)SDR ASAA0510110Support Angle · corrodedSUPPORT ANGLE CORRODED AT BSTA 630 BETWEEN LT AND RT KEELBEAMS. REPLACED SUPPORT ANGLE. (K)SDR ASAA0510103Keelbeam · corrodedKEELBEAM AT B-STA 648-662 RT LOWER SECTION CORROSION FOUND AT UPPER GATE. REPLACED KEELBEAM. (K)SDR ASAA0510106Stiffener · corrodedCORROSION FOUND ON VERTICAL STIFFENER. VERTICAL STIFFENER REPLACED. (K)SDR ASAA0510102Structure · corrodedAFT CARGO AREA B-STA 940 TO 947, STA 22L CORRODED. CORRODED STR 22L AT B-STA 947 REPLACED WITH FABRICATED REPAIR PART. (K)SDR ASAA0510100Floorbeam · corrodedAFT CARGO FLOOR SUPPORT BEAM ANCHOR NUTS HOLES HAS CORROSION AFT OF B-STA 767, RBL 3. AFT CARGO PIT FLOOR SUPPORT BEAM AFT OF B-STA 767, RBL 3 REPAIRED WITH FABRICATED REPAIR PARTS. (K)SDR PCSA0518051Cover · leakingDURING CLIMB CREW REPORTED LOSS OF HYDRAULIC (A) SYSTEM. AIRCRAFT WAS DIVERTED AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND FEEL COMPUTER FILTER COVER LEAKING HYDRAULIC FLUID. REMOVED AND REPLACED FEEL COMPUTER FILTER CAP AND O-RING IAW MM CH 20-10SDR ASAA0510096Splice · corrodedAFT CARGO PIT BS 907 BUTT SPLICE HAS CORROSION AT STR 27R. REMOVED AND REPLACED STRINGER SPLICE. (K)SDR ASAA0510097Shear Tie · corrodedSKIN TO FRAME ATTACHMENT AT B-STA 614 BETWEEN LT AND RT BEAM DAMAGED. REMOVED AND REPLACED SKIN TO FRAME ATTACHMENT. (K)SDR ASAA0510098Shear Tie · corrodedSKIN TO FRAME ATTACHMENT AT B-STA 572 BETWEEN LT AND RT BEAM DAMAGED. REMOVED AND REPLACED SKIN TO FRAME ATTACHMENT. (K)SDR ASAA0510095Stringer Clip · corrodedAFT CARGO B-STA 907 CORRODED TIE CLIP AT STR 21L. REMOVED AND REPLACED TIE CLIP. (K)SDR CA050512004Controller · failedDURING DESCENT FROM FL290 TO FL270, THE 'OFF SCHEDULE' DESCENT LIGHT ILLUMINATED. CABIN ALTITUDE WAS QUICKLY INCREASING WITH CABIN DIFFERENTIAL QUICKLY DECREASING. CREW SWITCHED TO STANDBY, MANUAL DC AND MANUAL AC BUT CABIN CONTINUED TO DE-PRESSURIZE. ATC WSDR DHL2005762003Oil Cooler · leakingAT 10,000FT, THE CREW OBSERVED THE NR 3 ENGINE PARAMETERS FLUCTUATING,FOLLOWED SPECIAL PROCEDURES SHUT DOWN THE ENGINE,DECLARED AN EMERGENCY AND DIVERTED BACK TO PHOENIX. AFTER TAKE OFF, NR 3 ENGINE PARAMETERS BEGAN FLUCTUATING. PERFORMED ABNORMAL PROCEDURE PSDR CA050506004Duct · separated(CAN) DUCT ASSEMBLY (13TH STAGE BLEED AIR) SEPARATED FROM FLANGE.SDR PCSA05041401Housing · strippedFLT 8414 ON APPROACH TO MIA CREW REPORTED NR 1 ENGINE LOST OIL, ENG. NR 1 WAS SHUTDOWN AS A PRECAUTION. A/C LANDED AT INTENDED DESTINATION WITHOUT FURTHER INCIDENT. MX INSPECTION OF THE NR 1 ENGINE FOUND OIL FILTER & GEARBOX CHIP DETECTORS HAD NO METAL, INSPECSDR FX7A200500004Window · crackedR-2 WINDOW OUTER PANE CRACKED.SDR 05FDEA00848Engine · malfunctionedDURING DESCENT FOR APPROACH FROM 8000-4000 FT., REDUCED THROTTLES TO IDLE NR 1 ENG DID NOT RESPOND APPROPRIATELY. NR 1 ENG PARAMETERS WERE 1.09 EPR, N1 46.8, EGT 450, N2 72.5, FF 2000 PPH. RAN RED TABS FOR LOSS OF THROTTLE CONTROL. ENGINE WOULD ACCELERATE BSDR C7WA200400082Switch · intermittentNR 2 KRUGER FLAP EXTEND LIGHT REMAINED ON AFTER TAKEOFF. REMOVED AND REPLACED NR 2 KRUGER FLAP SWITCH IAW MM.SDR DHL2005740522Skin · dentedNR 1 SLAT EXTERNAL SKIN DENTED AT W STA 738. REMOVED PANELS AND WEB FROM SLAT NR 1 FOR ACCESS. CUTOUT DAMAGED AREA FROM EXT SKIN 3.25 INCH BY 3.125 INCH, TRIMMED OUT SKIN AND ACCESS TO DOUBLER IAW SRM. FAB PARTS FILLER 3 .125 INCH BY 3.0625 MAT 2024 2024 T3SDR C1HA200593002Engine · overtempON TAKEOFF AFTER V1 THE NUMBER 1 ENGINE HAD SEVERE FLUCTUATIONS IN ALL INSTRUMENTS WITH VIBRATIONS ON NUMBER ONE SIDE. HEARD THREE LOUD POPS NR 1 EGT WENT TO 700 DEGREES C, THREE DIFFERENT TIMES IN RAPID SUCCESSION. DUMPED FUEL RETURNED FOR LANDING. FOLLOWE
Back to Pratt & Whitney JT8D-17