Pratt & Whitney JT8D-219
Service difficulty reports · 1,944
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 = 'JT8D219' 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 = 'JT8D219' 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 ASAA0680010Floor Panel · delaminatedC-CHECK, CABIN FLOOR PANEL DELAMINATED. REMOVED DAMAGE AREA. APPLIED GLASS CLOTH REPAIR. (K)SDR ASAA0680011Floor Panel · delaminatedC-CHECK, CABIN FLOOR PANEL DELAMINATED. REMOVED DAMAGED AREA. APPLIED GLASS CLOTH REPAIR. (K)SDR ASAA0680012Floor Panel · delaminatedC-CHECK, CABIN FLOOR PANEL DELAMINATED. REMOVED DAMAGED AREA. APPLIED GLASS CLOTH REPAIR. (K)SDR ASAA0680013Floor Panel · delaminatedC-CHECK, CABIN FLOOR PANEL DELAMINATED. REMOVED DAMAGED AREA. APPLIED GLASS CLOTH REPAIR. (K)SDR ASAA0680014Floor Panel · delaminatedC-CHECK, CABIN FLOOR PANEL DELAMINATED. REMOVED DAMAGED AREA. APPLIED GLASS CLOTH REPAIR. (K)SDR ASAA0680015Floor Panel · delaminatedC-CHECK, CABIN FLOOR PANEL DELAMINATED. REMOVED DAMAGED AREA. APPLIED GLASS CLOTH REPAIR. (K)SDR ASAA0680016Floor Panel · delaminatedC-CHECK, CABIN FLOOR PANEL DELAMINATED. REMOVED DAMAGED AREA. APPLIED GLASS CLOTH REPAIR. (K)SDR ASAA0680017Cusp Web · corrodedC-CHECK, CABIN FLOOR CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (K)SDR ASAA0680018Skin · dentedC-CHECK, FUSELAGE DENTED. REMOVED DAMAGED SECTION. INSTALLED INTERNAL DOUBLERS, FINGER DOUBLERS, AND INTERNAL STRAP. (K)SDR ASAA0680019Skin · dentedC-CHECK, FUSELAGE DENTED. REMOVED DAMAGED SECTION. INSTALLED INTERNAL DOUBLERS AND INTERNAL STRAPS. (K)SDR ASAA0680020Skin · gougedC-CHECK, LT WING OB FLAP IB VANE IS GOUGED OF LEADING EDGE. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (K)SDR ASAA0680021Skin · debondedC-CHECK, LT WING OB FLAP CENTER PREVIOUS SKIN REPAIR IS DEBONDED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (K)SDR ASAA0680022Skin · nickedC-CHECK, RT WING OB FORE FLAP CENTER DENTED ON LE PREVIOUS REPAIR. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (K)SDR ASAA0680023Skin · dentedC-CHECK, FUSELAGE SKIN DENTED. COLD-WORKED AREA BACK TO ORIGINAL CONTOUR AND INSTALLED REPAIR DOUBLER. (K)SDR ASAA0680024Torque Tube · corrodedC-CHECK, RUDDER TAB TORQUE TUBE LOWER SPLINES CORRODED. REPLACED RUDDER TAB TORQUE TUBE SHAFT ASSEMBLY. (K)SDR ASAA0680025Crank Assy · corrodedC-CHECK, RUDDER TAB TORQUE TUBE CONTROL CRANK SPLINES CORRODED. REPLACED TORQUE TUB CONTROL CRANK ASSY. (K)SDR ASAA0680026Spline · corrodedC-CHECK, RUDDER TAB TORQUE TUBE SPLINE CORRODED. REPLACED RUDDER TAB TORQUE TUBE. (K)SDR ASAA0680027Spring · corrodedC-CHECK, RUDDER LOAD FEEL AND TRIM SPRING ASSEMBLY CORRODED. REPLACED RUDDER LOAD FEEL AND TRIM SPRING ASSEMBLY. (K)SDR ASMF200601007Start Valve · failedDURING PUSHBACK, CAPTAIN REPORTED THAT THE LIGHT OF THE LEFT START VALVE TURNED ON. AIRCRAFT WAS SENT TO A REMOTE PLATFORM AND THE START VALVE WAS REPLACED IAW MM 80-10-01, TESTED CORRECT.SDR WX0600008Pin · missingCREW REPORTED THE FORWARD PAX DOOR PINS FELL OUT FROM THE GERT BAR AND SLIDE ARMAMENT. MAINTENANCE SECURED THE FORWARD ENTRY DOOR GIRT BAR LANYARD IAW MM 25-62-00. AIRCRAFT RETURNED TO SERVICE.SDR ASMF200601001Cadc · failedAIRCRAFT RETURNED TO PLATFORM BEFORE TAKEOFF. THE LT AIR SPEED INDICATOR WAS OUT OF SERVICE. THE LT CADC AND AIR SPEED INDICATOR WERE REPLACED IAW MM 34-16-01 AND MM 34-13-01 RESPECTIVELY, TESTED CORRECT. DURING OVERNIGHT CHECK, AIRCRAFT ARRIVED WITH REPORT OSDR ASAA0680001Door · dentedPRE-FLIGHT INSPECTION, FORWARD PAX (L-1) DOOR DENTED AT LOWER EDGE. INSTALLED EXTERNAL REPAIR DOUBLER. (K)SDR ASAA0580560Skin · dentedGATE-MAIN PAX (L-1) DOOR FORWARD CORNER DENTED BY JETWAY. REPAIRED DENT IAW SRM. (K)SDR ASMF200512024Relay · unknownAIRCRAFT RETURNED TO PLATFORM, AC CROSS TIE AND APU GENERATOR WERE OUT OF SERVICE. THE BCU, AC CROSS TIE RELAY AND GCU WERE REPLACED IAW MM 24-20-08, MM 24-20-06, MM 24-20-07 RESPECTIVELY, TESTED CORRECT.SDR ASMF200512022Pump · damagedDURING TRANSIT CHECK WAS DETECTED A FUEL LEAK BETWEEN GEAR BOX PUMP COUPLING AND THE RT ENGINE. AIRCRAFT WAS SENT TO THE HANGAR AND THE RT ENGINE FUEL PUMP WAS REPLACED IAW MM 73-12-01 PAGE 201, TESTED CORRECT.SDR ASMF200512023Pump · failedDURING TRANSIT CHECK, THE AUXILIARY HYDRAULIC PUMP DID NOT SHUT OFF. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT CHECK, THE RELAY 22-15 AND THE RT AUXILIARY HYDRAULIC PUMP WERE REPLACED IAW MM 29-21-00 AND MM 29-10-06 RESPECTIVELY, TESTED CORRECT.SDR ASMF200512021Switch · damagedDURING TRANSIT CHECK, THE AUXILIARY HYDRAULIC PUMP DID NOT SHUT OFF, DELIVERING 29 PSI WITH THE SELECTOR IN OFF POSITION. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT CHECK, THE WIRING WAS CHECKED; THE RULER S3-13 TERMINALS WERE CLEANED IAW WDM 29-21-0SDR DLM88050828Generator · burnedLEFT GENERATOR OFF LIGHT WITH CROSSTIE LOCKOUT, LEFT ENGINE FIRE INDICATION, REPLACED GENERATOR AND CSD.SDR ASAA0580558Skin · puncturedCLIMB, ENROUTE, CABIN DECOMPRESSED RAPIDLY AND UNCONTROLLABLE. ALL OXYGEN MASKS, SAME FOR ONE (TO BE REPORTED UNDER SEPARATE SDR), DROPPED PROPERLY. AN EMERGENCY DESCENT WAS MADE AND THE AIRCRAFT LANDED SAFELY BACK AT SEA. INVESTIGATION REVEALED THE CAUSE SDR ASAA0580559Hinge · failedCLIMB AT FL260, ENROUTE, FWD FLIGHT ATTENDANT OXYGEN MASK DID NOT DROP DURING CABIN DECOMPRESSION CAUSED BY FUSELAGE SKIN PUNCTURE. DETERMINED THE THE O2 MASK DOOR WAS JAMMED BY A DEBONDED O2 MASK DOOR HINGE. REBONDED O2 MASK DOOR HINGE AND ADJUSTED CLEARANCSDR ASMF200512020Csd · damagedAIRCRAFT RETURNED TO PLATFORM, DURING TAXING THE RT CSD REACHED 180 GRADES AND THE CSD SHUT OFF AUTOMATICALLY, THE RT CSD REPORT WAS DEFERRED IAW MEL 24-1. THE RT CSD AND HEAT EXCHANGE AIR OIL ENGINE WERE REPLACED IAW MM 24-10-01/-03, TESTED CORRECT. DEFERREDSDR DLM88050822Engine · overspeedSUSPECT RIGHT COMPRESSOR STALL. EPR PEGGED ABOVE 2, N1 ABOUT 108 PERCENT SHUTDOWN IN FLIGHT. FOLLOWED SEVERE DAMAGE CHECKLIST THERE WAS SOME SMELL OF SMOKE WHICH CLEARED WHEN THE ENGINE WAS SECURED. EDP SHOWED N1 109 PERCENT FOR 30 SEC. PERFORMED BORO NO DSDR ASMF200512018Door · false indicationAIRCRAFT RETURNED TO PLATFORM DURING TAKE OFF, AFTER NOSE LANDING GEAR ROTATION, THE ELECTRICAL/ELECTRONIC COMPARTMENT OPEN DOOR LIGHT TURNED ON. DURING MAINTENANCE REVISION, THE DOOR WAS DETECTED OPEN WITH THE SAFETY PINS ACTIVATED. THE ELECTRICAL/ELECTRONICSDR DLM88050809Line · contaminatedRIGHT ENG EPR INDICATION STUCK AT 1.06, DRAINED WATER FROM PT7 LINES.SDR ASAA0580536Longeron · corrodedC-CHECK, LONGERON CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPLACEMENT SECTION WITH 2 REPAIR SPLICES. (K)SDR ASMF200512017Blade · damagedDURING TRANSIT CHECK, A BLADE OF THE RT ENGINE WAS DETECTED WITH DAMAGE AND THE NOISE SUPPRESSOR LINER HAD INCRUSTED A FOD. INSPECTION WAS PERFORMED, DETECTING A DENT OF 0.75 X 0.25 AND .1875 OF LENGTH IAW MM 72-00-00. THE RT ENGINE BLADE WAS REWORKED IAW 72-0SDR GTIA050290Slide · detachedFWD ENTRY DOOR SLIDE PACK CAME OFF. REINSTALLED SLIDE PACK. (K)SDR ASMF200512016Csd · failedCAPTAIN REPORTED THAT DURING FLIGHT THE LT CSD REACHED 180 GRADES FOR A MINUTE, OVER TEMPERATURE LIGHT TURNED ON AND THE RT ENGINE EGT WAS OUT OF LIMITS AFTER STARTED. THE OPERATIONAL PROCEDURE WAS PERFORMED, THE LT CSD REPORT WAS DEFERRED IAW MEL 24-14-1, THESDR GTIA050289Powerpack · inoperativeOVERHEAD EMERGENCY LIGHTS IN TAIL COMPARTMENT INOPERATIVE. REMOVED AND REPLACED POWER PACK FOR EMERGENCY LIGHTS IN TAIL COMPARTMENT OVERHEAD. (K)SDR ASMF200512014Warning Light · illuminatedAIRCRAFT RETURNED TO PLATFORM (SPOILER DEPLOYED) LIGHT TURNED ON. THE REPORT WAS DEFERRED IAW MEL 27-32 CAT B. IN THE NEXT TRANSIT CHECK AT GDL, THE SPOILER SYSTEM WAS CHECKED AND TESTED IAW MM 27-00-00, BEING CORRECT. DEFERRED REPORT WAS CLOSED.SDR ASMF200512013Blade · fodDURING TRANSIT CHECK, A BLADE OF THE LT ENGINE WAS DETECTED WITH DAMAGE BY FOD. INSPECTION WAS PERFORMED, DETECTING A CRACK OF 0.125 X 0.250 BEING WITHIN LIMITS IAW MM 72-00-00. THE LT ENGINE BLADE WAS REWORKED IAW 72-00-00 PAGE 618, TESTED CORRECT.SDR GTIA050288Control Valve · warpedBRAKES WERE SPONGY AND SLOW TO STOP AC. REMOVED AND REPLACED LT POWER BRAKE CONTROL VALVE ASSY. (K)SDR GTIA050274Seat Track · corrodedSTA 1136, LT IB SEAT TRACK TANG DIMENSION BELOW 0.90. REMOVED DAMAGED AREA DRILLED NEW TRACK, TREATED, PRIMED AND INSTALLED SPLICE. (K)SDR ASMF200512012Shutoff Valve · malfunctionedAIRCRAFT RETURNED TO PLATFORM DURING RT ENGINE STARTING, IT DID NOT HAVE TURN IN N1 AND N2 AND OIL PRESSURE INDICATION. THE RT STARTER AND SHUTOFF VALVE WERE REPLACED IAW MM 80-10-02 AND MM 80-00-00 RESPECTIVELY, TESTED CORRECT.SDR ASAA0580537Fitting · corrodedC-CHECK, R-1 DOOR FLOOR MOUNTED GIRT BAR FITTING CORRODED. REPLACED CORRODED FITTING. (K)SDR ASAA0580538Frame · puncturedC-CHECK, FUSELAGE FRAME WEB PUNCTURED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (K)SDR ASAA0580539Intercostal · crackedC-CHECK, INTERCOSTAL CRACKED AT RADIUS. REPLACED INTERCOSTAL. (K)SDR ASAA0580540Web · corrodedC-CHECK, CABIN FLOOR WEB CORRODED. REPLACED WEB. (K)SDR ASAA0580541Web · corrodedC-CHECK, L-1 DOOR JAMB LOWER SILL WEB CORRODED. REMOVED DAMAGED SECTION OF WEB. INSTALLED REPAIR DOUBLER. (K)SDR ASAA0850542Floor Panel · corrodedC-CHECK, CABIN FLOOR PANEL HAS CORRODED INSERTS AND DELAMINATED AROUND INSERTS. REPLACED FLOOR PANEL. (K)
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