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.

SDR ASAA0680010Floor Panel · delaminatedC-CHECK, CABIN FLOOR PANEL DELAMINATED. REMOVED DAMAGE AREA. APPLIED GLASS CLOTH REPAIR. (K)Jan 15, 2006 · N969AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680011Floor Panel · delaminatedC-CHECK, CABIN FLOOR PANEL DELAMINATED. REMOVED DAMAGED AREA. APPLIED GLASS CLOTH REPAIR. (K)Jan 15, 2006 · N969AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680012Floor Panel · delaminatedC-CHECK, CABIN FLOOR PANEL DELAMINATED. REMOVED DAMAGED AREA. APPLIED GLASS CLOTH REPAIR. (K)Jan 15, 2006 · N969AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680013Floor Panel · delaminatedC-CHECK, CABIN FLOOR PANEL DELAMINATED. REMOVED DAMAGED AREA. APPLIED GLASS CLOTH REPAIR. (K)Jan 15, 2006 · N969AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680014Floor Panel · delaminatedC-CHECK, CABIN FLOOR PANEL DELAMINATED. REMOVED DAMAGED AREA. APPLIED GLASS CLOTH REPAIR. (K)Jan 15, 2006 · N969AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680015Floor Panel · delaminatedC-CHECK, CABIN FLOOR PANEL DELAMINATED. REMOVED DAMAGED AREA. APPLIED GLASS CLOTH REPAIR. (K)Jan 15, 2006 · N969AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680016Floor Panel · delaminatedC-CHECK, CABIN FLOOR PANEL DELAMINATED. REMOVED DAMAGED AREA. APPLIED GLASS CLOTH REPAIR. (K)Jan 15, 2006 · N969AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0680017Cusp Web · corrodedC-CHECK, CABIN FLOOR CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (K)Jan 15, 2006 · N969AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0680018Skin · dentedC-CHECK, FUSELAGE DENTED. REMOVED DAMAGED SECTION. INSTALLED INTERNAL DOUBLERS, FINGER DOUBLERS, AND INTERNAL STRAP. (K)Jan 15, 2006 · N969AS · Doug DC983 · Fuselage Main, Plate/SkinSDR ASAA0680019Skin · dentedC-CHECK, FUSELAGE DENTED. REMOVED DAMAGED SECTION. INSTALLED INTERNAL DOUBLERS AND INTERNAL STRAPS. (K)Jan 15, 2006 · N969AS · Doug DC983 · Fuselage Main, Plate/SkinSDR ASAA0680020Skin · gougedC-CHECK, LT WING OB FLAP IB VANE IS GOUGED OF LEADING EDGE. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (K)Jan 15, 2006 · N969AS · Doug DC983 · Trailing Edge FlapsSDR ASAA0680021Skin · debondedC-CHECK, LT WING OB FLAP CENTER PREVIOUS SKIN REPAIR IS DEBONDED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (K)Jan 15, 2006 · N969AS · Doug DC983 · Trailing Edge FlapsSDR ASAA0680022Skin · nickedC-CHECK, RT WING OB FORE FLAP CENTER DENTED ON LE PREVIOUS REPAIR. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (K)Jan 15, 2006 · N969AS · Doug DC983 · Trailing Edge FlapsSDR ASAA0680023Skin · dentedC-CHECK, FUSELAGE SKIN DENTED. COLD-WORKED AREA BACK TO ORIGINAL CONTOUR AND INSTALLED REPAIR DOUBLER. (K)Jan 15, 2006 · N969AS · Doug DC983 · Fuselage Main, Plate/SkinSDR ASAA0680024Torque Tube · corrodedC-CHECK, RUDDER TAB TORQUE TUBE LOWER SPLINES CORRODED. REPLACED RUDDER TAB TORQUE TUBE SHAFT ASSEMBLY. (K)Jan 15, 2006 · N969AS · Doug DC983 · Rudder Tab Control SystemSDR ASAA0680025Crank Assy · corrodedC-CHECK, RUDDER TAB TORQUE TUBE CONTROL CRANK SPLINES CORRODED. REPLACED TORQUE TUB CONTROL CRANK ASSY. (K)Jan 15, 2006 · N969AS · Doug DC983 · Rudder Tab Control SystemSDR ASAA0680026Spline · corrodedC-CHECK, RUDDER TAB TORQUE TUBE SPLINE CORRODED. REPLACED RUDDER TAB TORQUE TUBE. (K)Jan 15, 2006 · N969AS · Doug DC983 · Rudder Tab Control SystemSDR ASAA0680027Spring · corrodedC-CHECK, RUDDER LOAD FEEL AND TRIM SPRING ASSEMBLY CORRODED. REPLACED RUDDER LOAD FEEL AND TRIM SPRING ASSEMBLY. (K)Jan 15, 2006 · N969AS · Doug DC983 · Rudder Control SystemSDR 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.Jan 13, 2006 · N861LF · Doug MD83 · Engine CrankingSDR 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.Jan 7, 2006 · N862GA · Doug MD83 · Escape SlideSDR 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 OJan 2, 2006 · N204AM · Doug DC987 · Rate of Climb IndicatorSDR ASAA0680001Door · dentedPRE-FLIGHT INSPECTION, FORWARD PAX (L-1) DOOR DENTED AT LOWER EDGE. INSTALLED EXTERNAL REPAIR DOUBLER. (K)Jan 1, 2006 · N944AS · Doug DC983 · Passenger/Crew DoorsSDR ASAA0580560Skin · dentedGATE-MAIN PAX (L-1) DOOR FORWARD CORNER DENTED BY JETWAY. REPAIRED DENT IAW SRM. (K)Dec 29, 2005 · N947AS · Doug DC983 · Passenger/Crew DoorsSDR 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.Dec 28, 2005 · N169PL · Doug MD88 · Electrical Power SystemSDR 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.Dec 27, 2005 · N881LF · Doug MD83 · Engine Fuel PumpSDR 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.Dec 27, 2005 · N204AM · Doug DC987 · Hydraulic System, AuxiliarySDR 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 29-21-0Dec 26, 2005 · N204AM · Doug DC987 · Hydraulic System, MainSDR DLM88050828Generator · burnedLEFT GENERATOR OFF LIGHT WITH CROSSTIE LOCKOUT, LEFT ENGINE FIRE INDICATION, REPLACED GENERATOR AND CSD.Dec 26, 2005 · N985DL · Doug MD88 · Electrical Power SystemSDR 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 Dec 26, 2005 · N979AS · Doug MD83 · Fuselage Main, Plate/SkinSDR 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 CLEARANCDec 26, 2005 · N979AS · Doug MD83 · Fuselage, Door HingeSDR 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. DEFERREDDec 25, 2005 · N838AM · Doug DC983 · Alternator-Generator DriveSDR 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 DDec 23, 2005 · N918DE · Doug MD88 · Engine (Turbine/Turboprop)SDR 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/ELECTRONICDec 21, 2005 · N501AM · Doug DC982 · Door Warning SystemSDR DLM88050809Line · contaminatedRIGHT ENG EPR INDICATION STUCK AT 1.06, DRAINED WATER FROM PT7 LINES.Dec 20, 2005 · N919DE · Doug MD88 · Engine Pressure Ratio (EPR)SDR ASAA0580536Longeron · corrodedC-CHECK, LONGERON CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPLACEMENT SECTION WITH 2 REPAIR SPLICES. (K)Dec 20, 2005 · N934AS · Doug DC982 · Fuselage Main, Longeron/StringerSDR 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 72-0Dec 19, 2005 · N160PL · Doug MD88 · Engine (Turbine/Turboprop)SDR GTIA050290Slide · detachedFWD ENTRY DOOR SLIDE PACK CAME OFF. REINSTALLED SLIDE PACK. (K)Dec 18, 2005 · N822NK · Doug MD83 · Escape SlideSDR 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, THEDec 17, 2005 · N169PL · Doug MD88 · Alternator-Generator DriveSDR GTIA050289Powerpack · inoperativeOVERHEAD EMERGENCY LIGHTS IN TAIL COMPARTMENT INOPERATIVE. REMOVED AND REPLACED POWER PACK FOR EMERGENCY LIGHTS IN TAIL COMPARTMENT OVERHEAD. (K)Dec 16, 2005 · N830NK · Doug DC982 · Emergency LightingSDR 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.Dec 15, 2005 · N160PL · Doug MD88 · Drag Control SystemSDR 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.Dec 14, 2005 · N1075T · Doug DC987 · Engine (Turbine/Turboprop)SDR GTIA050288Control Valve · warpedBRAKES WERE SPONGY AND SLOW TO STOP AC. REMOVED AND REPLACED LT POWER BRAKE CONTROL VALVE ASSY. (K)Dec 14, 2005 · N822NK · Doug MD83 · Landing Gear Brake SystemSDR 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)Dec 13, 2005 · N802NK · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR 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.Dec 12, 2005 · N216AM · Doug DC987 · Engine Starting SystemSDR ASAA0580537Fitting · corrodedC-CHECK, R-1 DOOR FLOOR MOUNTED GIRT BAR FITTING CORRODED. REPLACED CORRODED FITTING. (K)Dec 12, 2005 · N973AS · Doug DC983 · Emergency EquipmentSDR ASAA0580538Frame · puncturedC-CHECK, FUSELAGE FRAME WEB PUNCTURED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (K)Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Main, FrameSDR ASAA0580539Intercostal · crackedC-CHECK, INTERCOSTAL CRACKED AT RADIUS. REPLACED INTERCOSTAL. (K)Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0580540Web · corrodedC-CHECK, CABIN FLOOR WEB CORRODED. REPLACED WEB. (K)Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0580541Web · corrodedC-CHECK, L-1 DOOR JAMB LOWER SILL WEB CORRODED. REMOVED DAMAGED SECTION OF WEB. INSTALLED REPAIR DOUBLER. (K)Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0850542Floor Panel · corrodedC-CHECK, CABIN FLOOR PANEL HAS CORRODED INSERTS AND DELAMINATED AROUND INSERTS. REPLACED FLOOR PANEL. (K)Dec 12, 2005 · N973AS · Doug DC983 · Fuselage Floor Panel
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