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 KNNA200700031Shear Tie · corrodedLIGHT SURFACE CORROSION AT SHEAR TIE ON BS 787, LOWER LOBE, BETWEEN STR 27L AND STR 27R, ACO NR 075370 REV 1. PROVIDE INSTRUCTIONS ON REPAIR AT BS 787, LOWER LOBE, BETWEEN STR 27L AND STR 27R SRM 53-10-4 FIGURE 7.SDR KNNA200700027Skin · dentedDENT ON FUSELAGE SKIN BETWEEN STR 26R TO STR 25R AT BS 420 R, ACO NR 075366, PROVIDE INSTRUCTIONS ON REPAIR OF SKIN AT BS 420 R STR-25R-26R, SRM 53-30-3.SDR CA070504010Switch · intermittent(CAN) ON FINAL APPROACH, THE FLIGHT CREW SELECTED LANDING GEAR DOWN. THE LAND GEAR INDICATORS ILLUMINATED 3 GREEN AND 3 RED. THIS INDICATED A DISAGREEMENT BETWEEN LANDING GEAR HANDLE POSITION AND LANDING GEAR POSITION. THE FLIGHT CREW SELECTED GEAR UP AND ABORSDR CA070504004Skin · cracked(CAN) DURING WASHING PROCEDURE MAINTENANCE DETECTED A SKIN CRACK AT BS727, WL215, APPROXIMATELY 1.5 INCHES LONG. THIS IS KNOWN AREA ADDRESSED BY SB 737-53-1065. THE AREA WAS REPAIRED IAW THE MANUFACTURERS SRM AND RETURNED TO SERVICE (TC NR 20070504004)SDR KNNA200700029Skin · damagedLOWER LOBE/FUSELAGE SKIN, SHOWS SIGNS OF HAVING LOOSE ATTACH RIVETS FROM BS 807 TO BS 827 AT BBL-0. FOUND CORROSION AT THE TIME FASTENER REMOVAL. ACO NR 075369 PROVIDE REPAIRS INSTRUCTIONS ON SKIN REPAIR AT BS 807-827 BBL 0, SRM 53-10-4 FIGURE 6.SDR KNNA200700036Skin · dentedUPPER LOBE/SEVERAL DENTS ON FUSELAGE SKIN FROM BS 995 TO BS1000 BETWEEN S-15L TO S-16L, NEAR DOOR L2.ACO NR 075385 REV 0. PROVIDES INSTRUCTIONS ON REPAIR OF FUSELAGE SKIN AFT OF L2 DOOR, SRM 53-30-3 FIG 46 AND FIG 48 BOEING MESSAGE 1-377247518-4 WITH FAA 8100SDR KNNA200700038Skin · dentedDENT ON FUSELAGE SKIN AT BS 358/STR-17L NEAR DOOR L-1. ACO NR 075398 REV. 0, PROVIDE INSTRUCTIONS ON REPAIR OF GOUGE FWD OF BS 360 SRM 53-30-3 AND BOEING MESSAGE 1-326794229-26 AND FAA 8100-9.SDR KNNA200700039Skin · canningOIL-CAN EFFECT ON FUSELAGE SKIN AT BS 384 BETWEEN STR-16L/17L, ACO NR 0753100 REV.0, PROVIDE INSTRUCTIONS ON REPAIR OF DAMAGE SKIN, BETWEEN BS 360L TO BS 420L SRM 53-30-3 AND BOEING MESSAGE 1-326794229-28 AND FAA 8100-9.SDR SPAA0700091Power Supply · inoperativeAFT SECTION OF FLOORTRACK ESCAPE PATH LIGHTING INOP. REPLACED BATTERY POWER SUPPLY AND FUNCTIONAL CHECK SATISFACTORY IAW CMM 33-21-27.SDR SPAA0700092Power Supply · inoperativeFORWARD SECTION OF FLOORTRACK ESCAPE PATH LIGHTING INOP. REPLACED POWER SUPPLY AND FUNCTIONALLY TESTED SATISFACTORY IAW CMM.SDR NWAA071129880Manifold · crackedDURING TAKEOFF, THE TOWER REPORTED EXCESSIVE SMOKE FROM THE NR 1 ENGINE. FLIGHT CREW ALSO REPORTED HIGHER FUEL FLOW FROM THE NR 1 ENGINE. THE FLIGHT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A CRACKED PRIMARY FUEL MANIFOLD. REMOVED ANSDR C8GA20070003Blades · damagedFLT 1723 FROM BOS TO TOL, DURING CLIMB-OUT, NR 2 ENGINE BEGAN TO VIBRATE AND WAS CONFIRMED WITH THE THROTTLE. ENGINE BEGAN TO COMPRESSOR STALL, ENGINE WAS SHUTDOWN AND AIRCRAFT LANDED WITHOUT INCIDENT IN TOL. POST FLIGHT INSPECTION REVEALED FOD DAMAGE TO THESDR PCSA10520071Pump · failedDURING CLIMB FELT VIBRATION, NR 1 ENGINE EPR AND FUEL FLOW DROPPED TO ZERO. NR 1 ENGINE WAS SHUT DOWN AS A PRECAUTIONARY MEASURE. SHUTDOWN WAS LESS THAN 30 MINUTES.SDR 46504Floorbeam · corrodedFOUND CORROSION AT FLOORBEAM STA 344 LBL 62.50 TO RBL 24.75.SDR KNNA200600004Floorbeam · corrodedFOUND CORROSION AT FLOORBEAM STA 344 LBL 62.50 TO RBL 24.75.SDR C1HA200695003Valve · stuckNR 1 ENGINE WAS SHUT DOWN ON START-EGT 550 DEG AND IT APPEARED THAT IT WOULD NOT STABILIZE AT OR BELOW 550 DEG. RAN COM 2-72.9 FOUND NR 1 ENG 13 TH STAGE BLEED VALVES STUCK PER CMM 75-30-00 PAGE 603 LUBED 1 ENG. 13 TH STAGE VALVES WITH WC-393. OPS CHECKED NSDR 46503Floorbeam · corrodedFOUND CORROSION AT FLOORBEAM STA 328 BL-0 TO RBL 62.50SDR KNNA200600003Floorbeam · corrodedFOUND CORROSION AT FLOORBEAM STA 328 BL-0 TO RBL 62.50.SDR CA061117005Support · cracked(CAN) ON WALK AROUND AFTER LANDING FOUND CENTER SUPPORT ASSY OF GRAVEL DEFLECTOR CRACKED. CENTER SUPPORT ASSY CRACK REPAIRED. ASSEMBLY SUPPORT FITTING P/N69-60100-2 REPLACED AIRCRAFT RETURNED TO SERVICE.SDR ASAA0611123Battery · dischargedSMOKE BARRIER NR 8 EXIT TO REAR LIGHT DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY.SDR 06FDEA03627Spar · failedRT WING FALSE SPAR FASTENERS LOOSE AT NR 5 FLAP TRACK ATTACH AREA REMOVED DAMAGED ANGLE AND WEB, FABRICATED NEW WEB SECTION, DOUBLER AND ANGLE SECTION WITH SPLICE ANGLES IAW DWG. SR 27-57-038 REV C. AND EA 7-5750-102761. ALL PARTS ALODINED AND PRIMERED IAW SRMSDR 06FDEA03629Attach Fitting · crackedLT WING NR 4 FLAP TRACK FALSE SPAR ATTACH FITTING CRACKED AND SEVERAL FASTENERS LOOSE. FABED NEW WEB SECTION, DOUBLER, ANGLE, AND SPLICES; AND INSTALLED IAW DWG SR27-57-038 REV C AND EA 7-5750-102761, (WING SPOILER SUPPORT BEAM-REPAIR) EA ATTACHED TO SNRM N008SDR 0602249877Line · failedWHILE ON FINAL APPROACH AFTER THE LANDING GEAR AND FLAPS WERE EXTENDED THE AIRCRAFT LOSS ALL OF THE FLUID AND PRESSURE IN THE RT HYDRAULIC SYSTEM. THE CREW CONTINUED THE APPROACH AND LANDED UNEVENTFULLY. TAXI OR TOWED TO GATE WAS NOT SPECIFIED. MAINTENANCE FOUSDR CA061011008Control Unit · malfunctioned(CAN) ON TAXI FOR DEPARTURE THE CREW OBSERVED A NR 2 CARGO PIT CAUTION INDICATION. THE AIRCRAFT RETURNED TO COMPANY RAMP WHERE MAINTENANACE DETERMINED THE SMOKE DETECTOR SYSTEM CONTROL ELECTRONICS UNIT IN THE NR 2 PIT WAS AT FAULT. THE UNIT WAS REPLACED AND THSDR 06FDEA03454Frame · dentedFWD CARGO BAY DENT IN FRAME FLANGE BS 500 STR 22 RT. ** SD ** COMING. REPAIRED FWD CARGO BAY FRAME AT BS 500 STR 22 RT IAW SRM 53-10-4.SDR 06FDEA03455Frame · dentedAFT CARGO BAY FRAME DENTED BS 950F STR 25-26L. REMOVED DAMAGE ON FRAME BS 950F STR 25L-26L AND REPARIED IAW SRM 51-40-3.SDR 06FDEA03450Frame · crackedINTERIOR CABIN, BS 800 FRAME IS CRACKED AT STR 14R, AT RADIUS AREA. REMOVED FRAME SECTION BS 800 STR 14R TO 18R AND REPLACED IAW SRM 51-30-5 AND 51-30-2.SDR 06FDEA03451Angle · corrodedLT WHEEL WELL, ANGLE IS CORRODED AT STR 18A SHELF, BS 879, LBL 69. REMOVED CORRODED ANGLE BS 879, LBL 69 AND REPLACED IAW SRM 51-10-2, 51-30-5 AND 51- 30-2.SDR 06FDEA03452Bulkhead · crackedFWD SIDE 178 BULKHEAD HAS DRILL START ON STRAP UNDER UPPER RT RADAR MOUNT BRACKET. REPAIRED DAMAGE ON 178 BULKHEAD STRAP IAW SRM 51-40-3.SDR 06FDEA03453Skin · chafedRT AFT EMERGENCY EXIT HAS CHAFE ON LOWER SKIN. REMOVED DAMAGE ON RT AFT EMERGENCY EXIT AND REPAIRED IAW SRM 52-00-3.SDR 06FDEA03458Skin · dentedEXTERIOR SKIN IS DENTED ON AIRSTAIR, AFT LT EDGE. REMOVED DAMAGE ON AIRSTAIR AND REPAIRED IAW SRM 51-40-2.SDR 06FDEA03459Frame · dentedFWD CARGO BAY DENTS IN FRAME STA 600 BETWEEN STR 22L-25L. REMOVED DAMAGE ON FRAME BS 600 BETWEEN STR 22L - 25L AND REPAIRED IAW SRM 51-40-3.SDR 06FDEA03460Frame · dentedFWD CARGO BAY DENT IN FRAME INNER FLANGE STA 660 BETWEEN STR 23R - 24R. REMOVED DAMAGE ON FRAME STA 660 BETWEEN STR 23R - 24R AND REPAIRED IAW SRM 51-40-3 AND 53-10-1.SDR 06FDEA03457Module · crackedSHORTLY AFTER LEVELOFF AT FL310, SYS A HYDRAULIC PUMP LIGHTS FLICKERED AND QUANTITY RAPIDLY DROPPED TO (ZERO). COMPLIED W/QRH AND LANDED IN MEM. FOUND HYD PRESS. LINE FROM NR 1 ENG TO "A" SYS MODULE CRACKED. INSTALLED NEW HYDRAULIC LINE AT "A" SYSTEM MODSDR 06FDEA03433Floorbeam · corrodedMAIN CARGO DECK, FLOORBEAM UPPER SURFACE CORRODED, BS 1070, RBL 25-45, WL 208. REMOVED CORROSION ON FLOORBEAM UPR SURFACE BS 1070 RBL 25-45 WL 208 AND REPAIRED IAW SRM 53-10-8.SDR 06FDEA03434Stringer · crackedVERTICAL STAB, CRACK IN STR 8R, AT RIB NR 2. REMOVED DAMAGE ON VERTICAL STA STR 8R AT RIB NR 2 AND REPAIRED IAW SRM 55-30-4 FIG 1.SDR 06FDEA03435Frame · dentedFWD CARGO BAY DENT IN I/B FLANGE OF FRAME STA 520 BETWEEN STR 24L - 25L. REMOVED DAMAGE IB FLANGE OF FRAME STA 520 BETWEEN STR 24L - 25L AND REPAIRED IAW SRM 51-40-03.SDR 06FDEA03436Structure · crackedRT WING IB MIDFLAP LOWER AFT STRUCTURE IS CRACKED AT IB AFT FLAP TRACK CUTOUT ** SD** COMING REPARIED RT WING IB MIDFLAP LOWER AFT STRUCTURE IAW SRM 51-40-4.SDR 06FDEA03438Web · chafedINTERIOR CABIN, MCD CUTOUT RESTRAINT WEB SKIN IS CHAFED AT BS 640, WL 255. REPAIRED INT CABIN MCD CUTOUT RESTRAINT WEB IAW SRM 51-40-2.SDR CA061018005Seal · torn(CAN) ON CLIMB OUT, NOSE GEAR RED WARNING LIGHT STAYED ON; GEAR CYCLED TWICE, NIL CURE. AIRCRAFT PROCEEDED TO AIRPORT, LANDING WAS NORMAL. ON GROUND, NOSE GEAR SERVICED, SUBSEQUENT TAKEOFF NORMAL. ON RETURN TO BASE, ONE SEAL FOUND TORN, ALL SEALS REPLACED, FULSDR 0602029886Skin · crackedDURING LINE MAINTENANCE OPERATIONS, TUG MADE CONTACT WITH THE FUSELAGE AND CAUSED CRACK AND TEAR IN SKIN AT BS 206 L26R. REPAIRED IAW EA 98-207520.SDR 06FDEA03131Indicator · inoperativeDURING RUNUP FOR T/O WITH INOP EPR GAUGE NEITHER N1 OR EPR WOULD GET APLC CALCULATED PARAMETERS. REJECTED T/O CALCULATED NR 2 ENG. EPR WAS 2.18 ACHIEVED ONLY 2.03 EPR. CALCULATED N1 WAS 100.6 ONLY ACHIEVED 97.0 N1. ENGINE NOT MAKING ENOUGH POWER.SDR 06FDEA2924Compressor · stalledAS WE APPLIED T/O POWER (STD POWERS) HEARD A LOUD BANG (COMPRESSOR STALL) AND REJECTED T/O BEFORE T/O POWER WAS SET. MAX SPEED 20KTS WIND 12KT X-WIND. SAT CONFIRMED NR 2 ENGINE COMPRESSOR STALL. C/W AMM 71-00-000-6 3.B. CENTER ENG COMPRESSOR STALL INSPESDR TSAA0626056Element · failedON TAKEOFF, FWD ANNUNCIATOR OVERHEAT LIGHT & NR 2 ENGINE OVERHEAT LIGHT BEGAN FLICKERING ON & OFF. 1ST OFFICER IDENTIFIED ENGINE & CALLED ALL ENGINE NORMAL. REQUESTED A RETURN TO FIELD FROM TOWER & ON LEVEL OFF BRINGING POWER LEVERS BACK OVERHEAT LIGHTS EXTINGSDR PCSA6130601Compressor · stalledFLIGHT 721 PREPARED TO TAKEOFF FROM MIA; THE CREW REPORTED NR 2 ENGINE COMPRESSOR STALLING AS POWER WAS APPLIED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE BLOCK. AMERIJET MAINTENANCE ACCOMPLISHED AN ENGINE RUN ON NR 2 ENGINE AND WAS ABLE TO DUSDR 06FDEA1420Fitting · looseNR 1 ENGINE FAILED TO MAKE STANDARD EPR ON TAKEOFF ROLL TARGET EPR 2.08, MADE ONLY 1.8 WITH THRUST LEVER AT FORWARD STOP. ENGINE WAS VERY SLOW TO ACCELERATE. NO OTHER PARAMETERS EXCEEDED. RUNWAY 27, WEATHER: 190/4KTS, 1ONM VIS, TEMP19*C, DEW POINT 11*C, 30.SDR PCSA033006Engine · damagedFLIGHT 848 AFTER PUSHBACK FROM PAP, THE CREW REPORTED WHEN POWER WAS ADDED THE NUMBER ONE ENGINE EXPERIENCED A VIBRATION. THE AIRCRAFT RETURNED TO THE GATE WITHOUT ANY FURTHER INCIDENT. FURTHER INSPECTION OF THE NUMBER ONE ENGINE INLET FOUND THE C-1 BLADES HSDR SROM200600003Flap · dentedDURING HEAVY MAINTENANCE VISIT FOUND DENT ON UPPER SURFACE OF LT IB MIDFLAP. REPAIRED FLAP BY INSTALLING INTERNAL DOUBLER AND FLUSH PART IN IAW SRM 57-50-4, FIG. 4 PG. 8 AND 9.SDR CA060316005Circuit Breaker · failedCREW REPORTED ON DEPARTURE/CLIMB-OUT, ALL FUEL TANK NR 1 AND NR 2 BOOST PUMP CB'S POPPED. EXTENSIVE VISUAL INSPECTION OF PUMPS, WIRING CONNECTORS, ELECTRICAL HARNESSES AND SPLICES CARRIED OUT. THE FOLLOWING COMPONENTS REPLACED: NR 2 GENERATOR HARNESS FROM FISDR CA060316006Relay · failedALL 4 FUEL BOOST PUMP CIRCUIT BREAKERS POPPED IN FUEL TANK NR 2. RECTIFICATION: 1 RELAY 109 ESS NR 2 BUS REPLACED. MAINTENANCE DETERMINED L1 AND L2 TERMINALS SHORTED TOGETHER CAUSING INTERNAL DAMAGE. LEFT AFT BOOST PUMP RELAY REPLACED.
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