Pratt & Whitney JT8D-219

Service difficulty reports · 1,944

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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 DALA1014030995Shear Tie · corrodedDURING HMV3, STA 1309 LONG 26R-26L AFTER REMOVAL OF FRAME FOUND SHEAR TIE TO BE CORRODED. REMOVED CORROSION ON STA 1309 SHEAR TIE L26R-26L IAW SRM 51-10-3 ORIG MAT.050, REMOVED .012, .038 REMAINING. FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG1, SH3. DRILLEDJun 21, 2010 · N995DL · Doug MD88 · Fuselage Internal Mounting StructureSDR DALA1014050995Attach Angle · corrodedDURING HMV3, AFT ACCESSORY COMPT STA 1380 L26L TO L26R ATTACHMENT ANGLE HAS CORROSION. REMOVED CORROSION STA 1380 L28L TO L26R FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG1, SH33 REMOVED APU FIRE EX LINE, FAN AIR SUPPLY LINE FUEL FEED LINE IAW AMM 26-26-04, 53Jun 21, 2010 · N995DL · Doug MD88 · Fuselage Main, Attach FittingsSDR DALA1014060995Attach Angle · corrodedDURING HMV, AFT CARGO STA1211 LONG 28R AND 29R FLOOR ATTACH ANGLE CORRODED. CORROSION OUT OF LIMITS REMOVED, FAB NEW ANGLE IAW DWG 5956705. INSTALLED NEW ANGLE IAW SRM 51-30-2,51-30-5. (DLM88101566)Jun 21, 2010 · N995DL · Doug MD88 · Fuselage Main, Attach FittingsSDR DALA1014070995Channel · corrodedDURING HMV, AFT CARGO STA 1155 AT L28R-L29R CHANNEL CORRODED. CORROSION WAS OUT OF LIMITS. REMOVED CHANNEL,FAB NEW CHANNEL IAW DWG 5936660, INSTALLED NEW CHANNEL IAW SRM 51-30-2, 51-30-5 (DLM8801567)Jun 21, 2010 · N995DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA1014080995Skin · corrodedDURING HMV3, AFT CARGO LOWER DOOR JAMB UNDER STRUCTURE STA 1175-1190 BELLY SKIN CORRODED. REQUIRES FURTHER INSP AFTER JAMB REMOVAL. REMOVED CORROSION FROM INNER SKIN STA 1117 TO STA 1231 BTW L28R AND L29R AND AROUND DOOR CUTOUT IAW SRM 51-30-3 ORIG MAT .069 IJun 21, 2010 · N995DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA1014280995Longeron · corrodedDURING HMV, AFT CARGO LONGERON 23L STA 1287 TO 1328 CORRODED. R & R LONGERON STRIP IAW SRM 51-10-4, 51-10-3 AND 51-30-5. (DLM88101587)Jun 21, 2010 · N995DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA1014290995Floor Panel · crackedDURING HMV, AT MAIN CABIN FLOOR PANEL NR 886C RT SIDE OF PANEL, CLOSE OUT PANEL STRIP BROKEN, REMOVED BROKEN STRIP, FOUND SUPPORT CRACKED IN 3EA PLACES. REMOVED CRACKED CLOSE OUT STRIP, REMOVED CRACKED SUPPORT, REPLACED EACH, FABBED STRIP (.025-7075T6), SUPPOJun 21, 2010 · N995DL · Doug MD88 · Fuselage Floor PanelSDR DALA1014300995Floor Support · corrodedDURING HMV, AFT CARGO COMPARTMENT FLOOR SUPPORT STA 1117-1255 L29R BOTTOM LEG OF BEAM CORRODED. R & R FLOOR SUPPORT PN 5936037501 IAW SRM 51-10-4, 51-30-5.Jun 21, 2010 · N995DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA1014310995Cusp Web · corrodedDURING HMV, MAIN PASSENGER CABIN STA 693 TO STA 712 LT CUSP WEB CORRODED TOP AND BOTTOM AND SKIN CRACKED. REMOVED DAMAGED SECTION OF CUSP WEB AND INSTALLED DOUBLER IAW EA 53-05D SH 1 & 3 DWG 53-1060.Jun 21, 2010 · N995DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA1014320995Attach Angle · damagedDURING HMV, AT STA 1120 L-28R SILL PLATE ATTACH ANGLE HOLES ELONGATED. R & R WITH NEW ANGLE FABRICATED IAW SRM 51-00 & DWG 593660 INSTALLED ANGLE IAW SRM 51-30-05, 51-30-01.Jun 21, 2010 · N995DL · Doug MD88 · Fuselage Main, Attach FittingsSDR DALA1014330995Door Frame · corrodedDURING HMV, AFT CARGO WEB AT LOWER DOOR JAMB CORRODED END TO END. CORROSION OUT OF LIMITS R & R WEB WITH PN 5936442-3 IAW SRM 51-10-4, 51-30-5, 51-30-2, DPS 900-2-4-1. RESTORED AREA IAW SRM 51-30-5, 51-30-2.Jun 21, 2010 · N995DL · Doug MD88 · Fuselage Main, StructureSDR DALA1014190995Stringer · crackedDURING HMV, MAIN CABIN RT AFT LAV STA 1338 L7R END FITTING IS CRACKED. REMOVED DAMAGED STRINGER END FITTING OBTAINED NEW FITTING PN 4912515-501N INSTALLED IAW SRM 51-10-4, 51-30-5.Jun 21, 2010 · N995DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA1013500995Skin · corrodedLT SIDE AFT OF FUEL BOOST PUMP ACCESS CORROSION ON SKIN. R & R LT WING HEATER BLANKET AND PERFORMED SUCCESSFUL TESTING IAW AMM 30-80-02 AND EA 09-070683-03AD REV L.Jun 20, 2010 · N995DL · Doug MD88 · Wing, Plate/SkinSDR DALA1013510995Frame · corrodedAFT CARGO STA 1287 L29R FRAME CORRODED. REMOVED CORROSION ON FRAME STA 1287 ORG MAT .063. REMOVED .030. REMAINING .033 TOOL USED H6458 CAL 15JUN10 FOUND OUT OF LIMITS IAW SRM 53-01 CUT AND REMOVED DAMAGE FRAME AT LBL 4 TO RBL 15 INSTALLED FRAME REPAIR SR95300Jun 20, 2010 · N995DL · Doug MD88 · Fuselage Main, FrameSDR DALA1013520995Shear Tie · corrodedAFT CARGO STA 1287 L27L - L27R SHEAR TIE CORRODED, BELLY SKIN REQUIRES INSP UNDER SHEAR TIE. REMOVED SHEAR TIE AT 1287 L27L TO L27R CORROSION WAS 100 PERCENT MAT LOSS OUT OF LIMITS IAW SRM 53-01. RECEIVED, LOCATED, DRILLED AND INSTALLED NEW SHEAR TIE AT STA 12Jun 20, 2010 · N995DL · Doug MD88 · Fuselage Internal Mounting StructureSDR DALA1013530995Cargo Track · corrodedDURING HMV, MID CARGO COMPARTMENT FROM STA 693-788 RT CARGO TRACK HAS CORROSION AROUND SEVERAL FASTENERS & FASTENER HOLES. CORROSION WAS OUT OF LIMITS R & R TRACK PN 5936594-527. (DLM88101546)Jun 20, 2010 · N995DL · Doug MD88 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1013540995Strap · corrodedDURING HMV3, AFT CARGO DOOR STA 1155-1164 STRAP ON BELLY SKIN CORRODED. REMOVED CORROSION IAW SRM 51-10-3 (6"X1") ORG MAT .063 MAT REMOVED .016 REMAINING MAT .047 OUT OF LIMITS IAW SRM 53-01. REPLACED STRAP BETWEEN STA 1155 AND STA 1164 L28R TO L29R MAT. .063Jun 20, 2010 · N995DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA1013890995Intercostal · corrodedDURING HMV, NR 2 CARGO COMPT AIRFRAME 769-B/H WALL LT 28 LONGERON INTERCOSTAL CORROSION AROUND FASTENER TO SURFACE. CORROSION HAD 100 PERCENT MAT LOSS R & R INTERCOSTAL.Jun 20, 2010 · N995DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA1013900995Frame · damagedAFT CARGO STA 1255 L/R 29L-29R HAS CORROSION ON BOTH SIDES OF FRAME. REMOVED EXISTING REPAIR, CUT OUT IS 15.5" X 4" NDT VERIFIED DAMAGE IS CONTAINED. LOCATED, FIT, DRILLED AND INSTALLED FRAME REPAIR FROM PN SR09530057-5 SPLICE, -13 PLATE, -9 ANGLE AND -25 FRAMJun 20, 2010 · N995DL · Doug MD88 · Fuselage Main, FrameSDR DALA1013910995Frame · crackedDURING HMV3, AFT ACCESSORY COMPT STA 1446 L17R CANTED FRAME HAS APPROX .1250" CRACK. REMOVED RT PYLON T/E WEDGE FOR FASTENER ACCESS. TRIMMED OUT DAMAGED AREA 1.0" X .75" FABRICATED AND INSTALLED REPAIR DOUBLER AND INSTALLED T/E WEDGE IAW SRM 51-30-1, 51-30-2 Jun 20, 2010 · N995DL · Doug MD88 · Fuselage Main, FrameSDR DALA1013920995Longeron Splice · corrodedDURING HMV, AFT CARGO STA 1287, LONG 25L, SPLICE CORRODED. CORROSION WAS OUT OF LIMITS FABRICATED AND INSTALLED NEW SPLICE ON TRAVELER 2030N01458.Jun 20, 2010 · N995DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA1014040995Cargo Track · corrodedDURING HMV, AFT CARGO STA 1212-1322 RT TIE DOWN TRACK CORRODED. CORROSION WAS OUT OF LIMITS R & R TIE DOWN TRACK PN 5936667-505 IAW SRM 51-30-5,51-30-1.Jun 20, 2010 · N995DL · Doug MD88 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1013940995Longeron · corrodedDURING HMV,AFT CARGO LONGERON 24L AFT END FITTING CORRODED. CORROSION WAS OUT OF LIMITS R & R END FITTING PN 3914590-501. (DLM88101554)Jun 20, 2010 · N995DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA1013970995Frame · corrodedDURING HMV3, AFT CARGO STA 1309 L27L-27R CORROSION ON FRAME. FOUND FRAME STA 1309 L27-27L TO BE OUT OF LIMITS DUE TO EXFOLIATION IAW SRM 51-10-3. REMOVED AND CUT FRAME BTW L25R-26R AND L25L-26L. DRILLED, TRIMMED AND INSTALLED FRAME REPAIR PARTS IAW SRM 53-03DJun 20, 2010 · N995DL · Doug MD88 · Fuselage Main, FrameSDR DALA1013990995Attach Angle · corrodedDURING HMV, AFT CARG LOWER DOOR CUTOUT ATTACH ANGLE CORRODED. CORROSION OUT OF LIMITS FABED ANGLE IAW DWG NR 5936070 ON TRAVELER 2030N01668 INSTALLED ANGLE IAW SRM 51-30-5 & 51-10-9.Jun 20, 2010 · N995DL · Doug MD88 · Fuselage Main, Attach FittingsSDR DALA1014000995Longeron · crackedDURING HMV3, L14R END FITTING CRACKED AT STA 1338. R & R END FITTING AT STA 1338 L14R.Jun 20, 2010 · N995DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA1014010995Attach Angle · corrodedDURING HMV, AFT CARGO STA 1211, LONG 28R AND 29R FLOOR ATTACH ANGLE CORRODED. CORROSON OUT OF LIMITS, REMOVED, FAB NEW ANGLE IAW DWG 5956705 INSTALLED IAW SRM 51-30-2, 51-30-5.Jun 20, 2010 · N995DL · Doug MD88 · Fuselage Main, Attach FittingsSDR AALA20100620DFW14Nose Cone · defectiveDFW - CREW REPORTED AUTOPILOT AND AUTO THROTTLE KICKED OFF AND BOTH ENGINES EXPERIENCED LOW EPR INDICATIONS. EMERGENCY DECLARED RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE NOSE CONE ASSEMBLY AND TWO PT7 LINES OJun 20, 2010 · N9630A · Doug DC983 · Turbine Engine Air Inlet SectionSDR DALA1013490995Attach Angle · crackedAFT ACCESSORY COMPT STA 1485 L9R CANTED FRAME FWD SIDE RAIN DRAIN PAN ATTACHMENT ANGLE IS CRACKED. R & R ATTACH ANGLE IAW SRM 51-10-4 AND 51-30-05. FABRICATED NEW ATTACH CLIP OUT OF .040 2024-T3 RECEIVED ON PO NO 0922117 IAW DAC DWG PL4967110 REVA. INSTALLED Jun 18, 2010 · N995DL · Doug MD88 · Fuselage Main, Attach FittingsSDR DALA1014140965Connector · not seatedMX FOUND THE EMERGENCY LIGHTS AT SEAT ROWS 12 AND 21 TO BE INOPERATIVE. MX REPLACED THE LIGHT ASSY AT ROW 21 AND RESEATED THE CONNECTOR AT SEAT 12. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE. (DLM88101583)Jun 16, 2010 · N965DL · Doug MD88 · Light System WiringSDR DALA1014090919Wire Harness · damagedMX FOUND THE SEAT 13D EMERGENCY LIGHT TO BE INOPERATIVE. (SAV EMPLOYEE NR 225052) MX REPLACED THE SEAT HARNESS. (DLM88101575)Jun 15, 2010 · N919DL · Doug MD88 · Light System WiringSDR DALA1014100950Wire · brokenMX FOUND THE EMERGENCY PATH LIGHTS AT 30DE TO BE INOPERATIVE. MX FOUND BROKEN WIRES AND SPLICED IN CONNECTORS. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.Jun 15, 2010 · N950DL · Doug MD88 · Light System WiringSDR YYFA201000017Cover · brokenEMERENCY EXIT PLASTIC COVER AT ROW 23F IS BROKEN.Jun 14, 2010 · N120MN · Doug MD83 · Emergency LightingSDR DALA1013010926Inlet · contaminatedAFTER TAKEOFF FLIGHT CREW NOTICED ODOR IN THE CABIN, F/A REPORTED GRAY HAZE IN THE PASSENGER CABIN WITH AFT LAVATORY SMOKE DETECTOR SOUNDING. FLIGHT CREW RETURNED ACFT TO MSP. FOUND APU INLET SOAKED WITH OIL PLACED APU ON MCO. ACCOMPLISHED FULL DUCT BURN OUTJun 13, 2010 · N926DL · Doug MD88 · APU Core EngineSDR DALA1013020926Unknown · odorINITIALLY AFTER TAKEOFF, CREW REPORTED SMOKE IN THE CABIN, THEN STATED IT HAD DISSIPATED AND WOULD CONTINUE. SMOKE LATER RETURNED AND DECISION WAS MADE TO DIVERT. MX ACCOMPLISHED DUCT BURN OUT IAW OPS 5089. (DLM88101485)Jun 13, 2010 · N926DL · Doug MD88 · Air Distribution SystemSDR DALA1012410934Engine · flamed outDURING TOP OF DESCENT AT FL320, THE FLIGHT CREW NOTICED THAT THE NR 1 ENGINE HAD FLAMED OUT. FLIGHT CREW DECLARED AN EMERGENCY, CONTINUED DESCENT, AND WAS ABLE TO RESTART THE NR 1 ENGINE AT FL220. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE Jun 7, 2010 · N934DL · Doug MD88 · Engine (Turbine/Turboprop)SDR DALA1013200934Fuel Control · inoperativeLEVEL AT CRUISE ALTITUDE OF FL 340 DESCENDED TO FL 320 UPON LEVELING ENGINE ROLLBACK AND SHUTDOWN. ENGINE WAS RESTARTED APPROX 15 MIN AFTER SHUTDOWN AT 22000 FT. C/W FLAMEOUT T/S. REPLACED FUEL FILTER. C/W LOW IDLE N2 T/S. NEEDS BOROSCOPE. REPLACED MAIN ENJun 7, 2010 · N934DL · Doug MD88 · Fuel Control/Turbine EnginesSDR DALA1013230934Engine · flamed outDURING TOP OF DESCENT AT FL320, THE FLIGHT CREW NOTICED THAT THE NR 1 ENGINE HAD FLAMED OUT. FLIGHT CREW DECLARED AN EMERGENCY, CONTINUED DESCENT, AND WAS ABLE TO RESTART THE NR 1 ENGINE AT FL220. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GAJun 7, 2010 · N934DL · Doug MD88 · Engine (Turbine/Turboprop)SDR DALA1013210909Coffeemaker · odorDURING PHASE OF FLIGHT F/A'S NOTICED BURNED ODOR BY AFT GALLEY. CREW TURNED PACKS OFF AND ON TO DISSIPATE ODOR. ACTION DIDN'T MAKE DIFFERENCE IN ODOR ONCE ON GROUND MX INSPECTED AFT GALLEY AND AFT LAVATORIES NO TROUBLE FOUND. ON CONTROL NR C06050773, OPN 5088,Jun 5, 2010 · N909DE · Doug MD88 · Buffet/GalleysSDR DALA1014860945Pan · corrodedON 02JUN10, THE MID CARGO LOWER DOOR SILL PAN, LOWER FLANGE WAS CORRODED BEYOND SRM LIMITS AT THE AFT DOOR STOP FTG. REPAIRED IAW SRM 53-05 P.Jun 2, 2010 · N945DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA1011480910Engine · failedNR 1 ENGINE FAIL INFLIGHT. LOUD BANG WITH ROLLBACK AND ENGINE LOSS OF POWER. DISCOVERED METAL IN TAILPIPE.May 30, 2010 · N910DL · Doug MD88 · Engine (Turbine/Turboprop)SDR DLM88101294Power Supply · inoperativeMX FOUND THE EMERGENCY LIGHTS LT AND RT OVER THE ROW 2 CEILING PANEL TO BE INOPERATIVE. MX REPLACED THE POWER SUPPLY AT ROW 6C. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.May 23, 2010 · N978DL · Doug MD88 · Emergency LightingSDR DLM88101293Power Supply · inoperativeMX FOUND THE AFT CABIN EMERGENCY FLOOR LIGHTS TO BE INOPERATIVE. MX REPLACED THE AFT CABIN EMERGENCY FLOOR LIGHTS POWER SUPPLY B5-212. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.May 22, 2010 · N945DL · Doug MD88 · Emergency LightingSDR DLM88101284Thermal Switch · arcedWINDSHIELD ANTI-FOG SWITCH TURNED ON DURING DESCENT AND ABOUT 5 MIN AFTER A WHITE SMOKE CAME FROM THE CTR WINDSHIELD SENSOR. THE ANTIFOG WAS TURNED OFF AND PROBLEM STOPPED. FOUND ARCING ON CTR WINDSHIELD THERMAL SWITCH. REPLACED SWITCH, S1-221 AND TERMINALS IMay 21, 2010 · N992DL · Doug MD88 · Windshield/Door Rain/Ice RemovalSDR DALA1013460999Skin · corrodedCORROSION BTW DOUBLER AND FUSELAGE SKIN ON LAV SERVICE PNL STAY=1312 TO Y=1322 BTW LONGS 19LH AND 22LH. REPAIR WAS ACCOMPLISHED IAW ERA 482821-14 REV ORIG. (DLM88101535)May 11, 2010 · N999DN · Doug MD88 · Fuselage Main, Plate/SkinSDR DLM88101159Beam · corrodedEXFOLIATION CORROSION ON MID CARGO COMPT LOWER DOOR JAMB BEAM BTWN ST Y=636 AND 693. REPAIRED IAW SRM 53-05, FIG 123.May 9, 2010 · N997DL · Doug MD88 · Fuselage Main, StructureSDR DLM88101145Attach Angle · crackedDURING HMV3 DHN FOUND AFT ACCESSORY STA 1437 L3R ATTACHMENT ANGLE CRACKED IN RADIUS. REMOVED AND REPLACED NEW ANGLE.May 8, 2010 · N993DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DLM88101147Angle · crackedDURING HMV3 DHN FOUND AFT ACCESSORY CANTED FRAME STA 1497 TO STA 1510 L12R TO L13R ATTACH ANGLE CRACKED IN RADIUS. REMOVED ANGLE, FABBED AND INSTALLED NEW ANGLE IAW DWG 9953956 AND SRM 51-30-5.May 8, 2010 · N993DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DLM88101149Pan · corrodedDURING HMV3, FOUND FWD CARGO COMPT DOOR JAMB LOWER JAMB CORROSION BETWEEN PAN AND SKIN CAUSED PAN TO CRACK. REMOVED THRESHOLD WEB AND CUT OUT SECTION OF DOOR JAMB WEB PAN AT STA 370-STA 427 IAW SRM 53-05D, 51-30-5, FAB -5, -7, -6 & -8 SPLICES FROM 2024T4 .040.May 8, 2010 · N993DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DLM88101150Frame · crackedDURING HMV3, FOUND AFT ACCESSORY AFT SIDE STA 1464 CANTED FRAME WEB HAS 2 EA CRACKS. CUTOUT DAMAGE 1.5 X 2 INCHES NDT VERIFIED DAMAGE REMOVED. FABRICATED AND INSTALLED FILLER FROM .025 & 075T6 AND REPAIR DOUBLER FROM .032 7075T6 IAW SRM FIG 4, SH 4.May 8, 2010 · N993DL · Doug MD88 · Fuselage Main, Frame
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