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 CA010628001Wire · broken(CAN) WHEN LANDING GEAR EXTENDED, R/H MAIN GEAR DOOR LIGHTS DO NO ILLUMINATE. INSPECTED RT MAIN GEAR DOOR CANNON PLUG, WIRE PIN 6 BROKEN, REPAIRED WIRE TO PIN 6. IAW WDM 32-60-04, CANNON PLUG RESECURED FUNCTION CHECKED SERVICABLE.SDR C1HA200183003Oil Filter · dirtyAFTER ENGINE START NR 3 ENGINE LOW OIL PRESS/FILTER BYPASS LIGHT ILLUMINATED. REMOVED AND REPLACED MAIN OIL FILTER, RAN ENG, LEAK AND OPS CHECK GOOD.SDR C1HA200185005Filter · cloggedAFTER 17 MIN NR 2 ENG OIL PRESSURE/ FILTER BYPASS LIGHT ILLUMINATED. PRECAUTIONARY ENGINE SHUT DOWN, RETURN TO ORIGINATION POINT. REMOVED AND REPLACED MAIN OIL FILTER, RAN ENGINE, CHECKS GOOD. PLACED FILTER ON 50 HR REINSPECT.SDR CA010625028Connector · misinstalled(CAN) IN TROUBLE SHOOTING A HISTORY OF INTERMITTENT ANTI-SKID PROBLEMS IT WAS DISCOVERED THAT THE HYDRAULIC BRAKE PRESSURE LINES FROM THE AIRFRAME TO THE TOP OF THE R.H LANDING GEAR SWIVELS THE CONNECTORSTOTHE WHEEL SPEED TRANSDUCERS WERE SWAPPED TO THE OPPOSISDR 2001UALA00879Stringer · crackedSTRINGER CRACKED AT BS 1016, STR 6L. ACCOMPLISHED SPLICE REPAIR. MAJOR REPAIR ACCOMPLISHED.SDR CA010628053Start Valve · failed(CAN) #2 ENGINES START VALVE OPEN LIGHT ILLUMINATED IN FLIGHT. DEFERRED #2 ENGINE START VALVE FOR PARTS & T/S IAW MEL 80-1 CAT "C" ITEM EXPIRES 6/10/01.SDR 2001UALA00864Frame · crackedFUSE FRAME CRACKED IN RADIUS AT BS 188, WL 207, STR 17L. ACCOMPLISHED FRAME REPAIR. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00863Frame · crackedFRAME CRACKED IN RADIUS AT BS 188, WL 207. REPAIRED FRAME. MAJOR REPAIR ACCOMPLISHED.SDR CA010522003Generator · failed(CAN) 20 MINUTES AFTER DEPARTURE, APU GENERATOR DROPPED OFF LINE. RETURNED DUE #2 CSD WAS ON MEL. REPLACED #2 GENERATOR AND CSD AS PER WORK CARDS 1177-2 AND 1182-2. GROUND RUNUP COMPLETED, APU AND NR 2 GENERATOR CHECKED SERVICEABLE.SDR 2001UALA00766Doubler · crackedPREVIOUS FRAME REPAIR CRACKED AT BS 420, STR 23L. REPLACED REPAIR DOUBLER. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00767Web · crackedFLOOR PRESSURE WEB CRACKED AT BS 1004, LBL 40, WL 208. REMOVED AND REPLACED WEB. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00744Floorbeam · crackedFLOORBEAM CRACKED AT FLOOR LEVEL AT BS 663, BL 0. REMOVED DAMAGED AREA. ACCOMPLISHED SPLICE REPAIR. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00715Bulkhead · crackedBULKHEAD CRACKED AT RIVET HOLE STA 178, WL 234, LBL 18.1. MAJOR REPAIR ACCOMPLISHED. INSTALLED SKIN DOUBLER.SDR 2001UALA00692Floorbeam · crackedFLOOR BEAM WEB CRACKED IN TWO PLACES. STA 706-716 BL 0. INSTALLED DOUBLER.SDR 2001UALA00691Bulkhead · crackedBULKHEAD WEB CRACKED AT LOWER RT RADAR MOUNT. STA 178, WL200, RBL 5. REPAIR DOUBLER INSTALLED.SDR 2001UALA00639Skin · crackedFUSELAGE SKIN CRACKED BETWEEN WL 207 AND 218 AT RBL 5.7. REMOVED DAMAGE AND INSTALLED REPAIR PER SRM 53-10-11.SDR 2001UALA00614Bulkhead · crackedBS 178 BULKHEAD 2 EA CRACKS ON INBD SIDE OF LWR WX RADAR ANTENNA MOUNT. ACCOMPLISHED DOUBLER REPAIRS.SDR CA010522007Csd · unreliable(CAN) AT FL 230, NR 1 CONSTANT SPEED DRIVE LOW OIL PRESSURE LIGHT ILLUMINATED. FLIGHT ELECTED TO RETURN DUE APU ELECTRICS WERE UNRELIABLE. REPLACED NR 1 CSD AS PER WORK CARD 1182-1. APU AND NR 1 CSD CHECKED SERVICEABLE DURING GROUND RUN.SDR 01FDEA00295Engine · leakingNR 3 ENG DURING CLIMBOUT, LOW OIL PRESS/FILTER BYPASS LIGHT ILLUM. FOLLOWED RED TAB THRU ENG SHUTDOWN. PREVIOUS WRITE-UP ON NR 3 OIL PRESS. *S/D* REMOVED AND REPLACED NR 3 ENG PER WORK CARD 70T0001-03.SDR C1HA200184004Engine · stalledENG NR 2 COMPRESSOR STALL DURING POWER REDUCTION ON DESCENT FROM FL350 AT APPROX 1.8-1.7 EPR. REMOVED AND REPLACED NR 2 ENGINE.SDR 2001UALA00513Angle · crackedT ANGLE CRACKED ON THE FORWARD BULKHEAD OF THE LEFT WHEEL-WELL AT STA 663 LBL 54. REPLACED 12 INCH T ANGLE STIFFENER. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00442Skin · damagedAFT CARGO DOOR AFT DOOR FRAME LIP EXTERIOR SKIN APPROXIMATELY 19 INCHES FROM THE BOTTOM IS DEFORMED AND HAS A GOUGE. REPAIRED DAMAGED AREA. MAJOR REPAIR ACCOMPLISHED.SDR ASAA0110192O-Ring · nickedANC - FLT 64 - FLIGHT ATTENDANT REPORTED CHEMICAL ODOR ON CLIMBOUT WHICH DISSIPATED AFTER A FEW MINUTES. NO OTHER REPORTS WERE NOTED. AIRCRAFT LANDED IN JNU WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND ENGINES FOR FERRY FLIGHT TO SEA FOR TROUBLESHOOSDR 2001UALA00394Skin · damagedRT FUSELAGE HAS EXISTING INTERIM REPAIR FROM BS 178 TO BS 191 AND FROM WL 190 TO WL 199. ACCOMPLISHED FINAL REPAIR. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00395Skin · damagedLT FUSELAGE HAS EXISTING INTERIM REPAIR FROM BS 178 TO BS 191 AND FROM WL 190 TO WL 199. ACCOMPLISHED FINAL REPAIR. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00380Generator · failedNR 2 GENERATOR DROPPED OFF LINE. DRAINED THE CSD OIL TO PROPER LEVEL, AND CHECKED THE MAGNETIC OIL PLUG / FOUND CLEAN OF DEBRIS. FUNCTIONAL TEST ACCOMPLISHED. AIRCARFT RETURNED TO SERVICE.SDR 2001UALA00369Keelbeam · damagedDAMAGED AREAS AT KEEL BEAM STA 680 AND STA 708. REPLACES FASTENERS AT DAMAGED AREAS. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00321Floor Support · corrodedFLOOR SUPPORT HAS CORROSION AROUND FASTENER HOLES AT RBL 20 AND BETWEEN STA 967 AND STA 986. REMOVED CORRODED FLOOR SUPPORT. FABRICATED, ALODINED, PRIMED, AND INSTALLED NEW FLOOR SUPPORT. MAJOR REPAIR ACCOMPLISHED.SDR CA010406005Connector · damaged(CAN) THE AIRCRAFT WAS DEPARTING WHEN THE CREW EXPERIENCED AN APU FIRE INDICATION. THEY FOLLOWED PROCEDURES INCLUDING DISCHARGING THE EXTINGUISHER BOTTLE THEN RETURNED TO BASE. THE APU WAS INSPECTED BY MAINTENANCE AND THERE WAS NO INDICATION OF FIRE DAMAGE. THSDR C1HA200194010Engine · overtempNR 1 ENG AT CRUISE ENG TEMP CLIMBED TO 145C OIL QUANTITY DROP TO UNDER 1 GAL. ENG SHUT DOWN ENG OIL TEMP WENT PAST RED LINE. AIRCRAFT RETURNED TO ORIGINATING STA. REMOVED AND REPLACED NR 1 ENG.SDR CA010404008Windshield · leaking(CAN) CLIMBING THROUGH 13,000 FEET, APPROXIMATELY 4 PSI CABIN PRESSURE, CAPTS WINDSHIELD POPPED WITH A NOTICEABLE PRESSURIZATION LEAK. RETURNED. WINDOW INSPECTED, NO DEFECTS NOTED. WINDOW ATTACHED BOLTS WERE RETORQUED. AIRCRAFT PRESSURIZED TO 3 PSI, NO PRESSURSDR CA010322012Compressor · making metal(CAN) THE AIRCRAFT WAS CLIMBING OUT OF VANCOUVER WHEN THE APU DID AN AUTO SHUT DOWN AND THE APU FIRE HANDLE ILLUMINATED. THE FIRE HANDLE WAS PULLED BUT THE BOTTLE WAS NOT DISCHARGED DUE TO THE FIRE INDICATION GOING OUT. THE AIRCRAFT RETURNED TO VANCOUVER WHERESDR DHL2001742001Engine · leakingON GROUND PRIOR TO TAKEOFF ROLL, LOW OIL PRESSURE LIGHT ILLUMINATED, OIL QUANTITY WENT TO ZERO, AND OIL PRESSURE INDICATED-20 PSI ON NR 2 ENG. PERFORMED ENG FAILURE EMERGENCY CHECK LIST. SHUTTING DOWN NR 2 ENG IMMEDIATELY AFTER BLOCK IN VISUAL INSPECTION SHOSDR SROM200100016Skin · crackedDURING C CHECK INSPECTION, FOUND A SKIN CRACK AT AFT ENTRY DOOR (L2) CUTOUT (LOWER).SDR SROM200100014Skin · crackedDURING C CHECK INSPECTION, FOUND SKIN DAMAGE/CRACK AT THE FORWARD APU DOOR HINGE CUTOUT.SDR 2001UALA00231Collar · out of adjLEFT GEAR UNSAFE LIGHT ILLUMINATED. SUPPLEMENTAL DATA UPDATE FOUND UPLOCK BELL CRANK RETAINING COLLAR OUT OF ALIGNMENT AND CONTACTING MANUAL RELEASE LEVER. RE-ALIGNED AND SECURED COLLAR. OPERATIONAL CHECK AND MANUAL EXTENSION OF LANDING GEAR CHECKED NORMAL.SDR SROM200100013Skin · crackedDURING C CHECK INSPECTION, FOUND A CRACK IN SKIN AT UPPER HINGE CUTOUT ON THE FORWARD GALLEY DOOR.SDR SROM200100012Skin · crackedDURING C CHECK INSPECTION, FOUND A CRACK IN THE FORWARD GALLEY DOOR (R1) EXTERIOR SKIN AT LOWER HINGE CUTOUT CRACKED AT UPPER CORNER.SDR 2001UALA00229Collar · out of adjLEFT GEAR UNSAFE LIGHT ILLUMINATED. SUPPLEMENTAL DATA UPDATE FOUND UPLOCK BELLCRANK RETAINING COLLAR OUT OF ALIGNMENT AND CONTACTING MANUAL RELEASE LEVER. RE-ALIGNED AND SECURED COLLAR. OPERATIONAL CHECK AND MANUAL EXTENSION OF LANDING GEAR CHECKED NORMAL.SDR COOSDR02016Fitting · corrodedFITTING, LEFT WING, OUTBOARD MID-FLAP INBOARD/OUTBOARD FITTINGS FLAP CARRIAGE WITH CORROSION.SDR SROM200100011Beam · corrodedDURING C CHECK INSPECTION, FOUND THE LEFT MLG BEAM HAS SEVERAL AREA OF LEVEL 1 CORROSION ON LOWER SURFACE AT PANEL MOUNTING HOLES.SDR SCNA01017Engine · failedTHE NUMBER TWO ENGINE FAILED ON TAKEOFF FROM PVR AT LOW SPEED.SDR 2001UALA00158Skin · crackedSEVERAL FATIGUE CRACKS WERE FOUND IN THE FUSELAGE SKIN JUST AFT OF THE FORWARD GALLEY DOOR AND FORWARD OF THE STA 360 PRODUCTION JOINT. *S/U* FASTENER HOLE CRACKED AT STR 15R WAS REPAIRED PER SRM 53-30-3, FIGURE 43. FASTENER HOLES CRACKED AT STR 16R WERE RESDR 0100719855Switch · dirtyDURING TAKEOFF, THE LEFT ENGINE REVERSER UNLOCK INDICATION LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AT 120 KTS WITHOUT INCIDENT. MAINTENANCE CLEANED THE UPPER AND LOWER REVERSER INDICATING SWITCHES. OPERATIONAL CHECK NORMAL.SDR SROM200100007Frame · corrodedDURING C CHECK INSPECTION, FOUND CORROSION ON FRAME.SDR SROM200100008Shear Tie · corrodedDURING C CHECK, FOUND CORROSION ON SHEAR TIE.SDR SROM200100009Angle · corrodedDURING C CHECK INSPECTION, FOUND LEVEL 1 CORROSION ON ANGLE.SDR SROM200100010Stringer · corrodedDURING C CHECK INSPECTION, FOUND CORROSION ON STRINGER.SDR 2001UALA00131Check Valve · restrictedRETURNED TO FIELD DUE TO LOSS OF THE B-SYSTEM HYDRAULICS. *S/D* FOUND B-SYSTEM RESERVOIR CHECK VALVE FAILED AND RESTRICTING FLOW. REPLACED BOTH RESERVOIR CHECK VALVES. SERVICED HYDRAULICS TO FULL AND LEAKED CHECKED GOOD.SDR CA010307011Bracket · cracked(CAN) NOSE LANDING GEAR FORWARD DOORS ACTUATING BRACKET WHICH ATTACHES TO THE NOSE GEAR. THE ACTUATING ROD END ATTACH POINT WAS FOUND CRACKED DURING AIRCRAFT SERVICING. THE BRACKET WAS REMOVED AND REPLACED WITH SERVICEABLE PART I.A.W. BOEING 727 MM 32-22-1.
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