N119DL

Service difficulty reports not matched to an aircraft · 33

They name N119DL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. Newest first.

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 n_number = 'N119DL' AND registry_match IS NULL
  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 DL76S050813Bowl · strippedLOST CENTER SYSTEM HYD. FOUND ADP FILTER MODULE BOWL STRIPPED OFF THE HOUSING. REPLACED MODULE.Dec 20, 2005 · N119DL · Boeing 767332 · Hydraulic System, MainSDR DL76S041062Cap · crackedCENTER HYDRAULIC SYSTEM DUMPED ALL FLUID WHILE MOVING FLAPS TO 15 DEGREES ON TAXI OUT SLC. FOUND CAP CRACKED AND SEPARATED FROM MODULE ON UPPER PART ABOVE HANDLE ON RT GND CHECKOUT MODULE. REPLACED RT CHECKOUT MODULE. LK AND OP CK GOOD. REMOVED, INSPECTED Nov 25, 2004 · N119DL · Boeing 767332 · Hydraulic System, MainSDR DL76S040425Skin · crackedTHE LOWER AFT CORNER OF THE L1 DOOR CUTOUT WAS FOUND WITH A CRACK IN THE SKIN AND UNDERLYING BEARSTRAP AT FS 340. THE CRACK WAS REMOVED WITH A 4 X 5 INCHES CUTOUT THROUGH BOTH MEMBERS. THE CUTOUT WAS REPAIRED WITH 3 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 0May 8, 2004 · N119DL · Boeing 767332 · Fuselage Main, Plate/SkinSDR DL76S040408Skin · crackedCRACK REPAIR THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT WAS FOUND WITH A CRACK IN THE SKIN AND UNDERLYING BEARSTRAP. THE CRACK WAS REMOVED WITH A 5 X 4 INCHES CUTOUT THROUGH BOTH LAYERS. THE CUTOUT WAS REPAIRED WITH 3 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ERMay 6, 2004 · N119DL · Boeing 767332 · Fuselage Main, Plate/SkinSDR DL76S031113Bulkhead · bird strikeTHE WEB OF THE FWD PRESSURE BULKHEAD AT FS 132.5 WAS PUNCTURED AS A RESULT OF A BIRD STRIKE BETWEEN LBL 10.6 & 16. THE VERTICAL BEAMS AT LBL 10.6 & 16 WERE DENTED. THE DAMAGED AREA OF WEB WAS REMOVED WITH A CUTOUT AND THE DENTED FLANGES OF THE BEAMS TRIMMED Dec 18, 2003 · N119DL · Boeing 767332 · Fuselage Main, BulkheadSDR DL76S030650Support Beam · corrodedWING LT INBD FLAP OUTBD SUPPORT BEAM NR 3 SUPPORT : CORROSION IN AFT ATTACH HOLE BORES. THE AFT 4 ATTACH HOLES FOR THE OUTBD SUPPORT BEAM AT THE INBD FLAP ATTACH LOCATION WERE FOUND CORRODED. THE HOLES WERE REAMED TO REMOVE CORROSION, HFEC INSPECTED, OVERSIJul 12, 2003 · N119DL · Boeing 767332 · Wing, Control Surface Attach FittingsSDR DL76S030649Support Beam · corrodedWING LT INBD FLAP OUTBD SUPPORT BEAM NR 3 SUPPORT : FWD FLAP ATTACH HOLE CORROSION, THE 2 FWD FLAP ATTACH HOLES ON THE OUTBD SUPPORT BEAM NR 3 SUPPORT FOR THE INBD FLAP LOCATION WERE FOUND CORRODED. THE CORROSION WAS REMOVED BY OVERSIZING THE BORES, HFEC INSJul 12, 2003 · N119DL · Boeing 767332 · Wing, Control Surface Attach FittingsSDR DL76S030648Support Beam · corrodedWING / LT / INBD FLAP / INBD SUPPORT BEAM / SUPPORT NR 4 : FLAP ATTACH HOLE CORROSION THE LT INBD FLAP INBD SUPPORT BEAM WAS FOUND WITH CORROSION IN THE AFT INBD AND AFT OUTBD ATTACH LUG HOLES. THE HOLES WERE REAMED TO REMOVE CORROSION, HFEC INSPECTED, OVJul 12, 2003 · N119DL · Boeing 767332 · Trailing Edge FlapsSDR DL76S020671Smoke · detectedAFTER T/O SMOKE IN MID CABIN WITH SMOKE DETECTOR GOING OFF IN MID CABIN. RETURNED TO LAND. LT PACK TRIPPED AND LT ENG BLEED LIGHT ILLUMINATED. ON GROUND SMOKE DISSIPATED. COMPRESSOR WASH NUMBER 1 ENGINE. AFTER WASH - RUN ENG 5 MINS AT IDLE, RUN PACKS/CYCLJun 15, 2002 · N119DL · Boeing 767332 · Air Distribution SystemSDR DL76S020257Beam · crackedNR 5 LEADING EDGE SLAT NOSE BEAM WAS FOUND DAMAGED AT STA 439. REPAIR PER ER/A 402159-14.Mar 4, 2002 · N119DL · Boeing 767332 · Leading Edge DevicesSDR DL76S020060Switch · malfunctionedDURING THE BOARDING OF FLIGHT 706 FROM SEA/ATL CREW REPORTED SMOKE IN THE COCKPIT. CAUSE OF SMOKE WAS FOUND TO BE THE RT AFT FUEL PUMP SWITCH IN P5 PANEL. REPLACED SWITCH ASSY, PART WAS REPLACED.Jan 18, 2002 · N119DL · Boeing 767332 · Aircraft Fuel Distribution SystemSDR DL76S020919Light · inoperativeFOUND ON L/O CHECK, DOOR R1 EXT EMERGENCY SLIDE LIGHT INOP. REPLACED LIGHT ASSY, CHECK GOOD.Aug 7, 2001 · N119DL · Boeing 767332 · Emergency LightingSDR DL76S002047Bottle · dischargedON LAYOVER FOUND RT WING OVERWING SLIDE BOTTLE PRESS LOW. REPLACED BOTTLE.Oct 17, 2000 · N119DL · Boeing 767332 · Escape SlideSDR DL76S000211Skin · crackedSKIN CRACKED AT VHF ANTENNA CUTOUT AT STA 1197 + 99 AND BL 0. DAMAGE REMOVAL RESULTED IN A RECTANGULAR CUTOUT MEASURING 3 I/B-O/B BY 14 FWD/AFT. ER/A 334036-14 REV A.Jan 21, 2000 · N119DL · Boeing 767332 · Fuselage Main, Plate/SkinSDR DL76S992707Megaphone · brokenON L/O, FOUND FWD CLOSET MEGAPHONE BROKEN. REPLACED MEGAPHONE.Dec 10, 1999 · N119DL · Boeing 767332 · Emergency EquipmentSDR DL76S991504Oven · dirtyACRID FUMES IN COCKPIT AND CABIN COULD NOT ISOLATE. POSSIBLY STRONGER IN FWD GALLEY AND FC AREA. INSPECTED E & E, ALL CARGO COMPARTMENTS, NOTHING FOUND. REMOVED ALL FC GALLEY OVENS AND COFFEEMAKERS, NOTHING FOUND. CHECKED OVERHEAD AREA OF FC CABIN, NOTHINGJul 3, 1999 · N119DL · Boeing 767332 · Buffet/GalleysSDR DL76S991075Retract Mech · malfunctionedRT MAIN GEAR REMAINED EXTENDED AFTER T/O, ALT GEAR EXTENSION WORKED OK. MTC IN WORK ON GEAR RETRACTION AT TOC. NO NOTICEABLE DAMAGE TO GEAR. GEAR PINS INSTALLED FOR MTC.May 16, 1999 · N119DL · Boeing 767332 · Landing Gear Retraction/Extension SystemSDR DL76S981272Skin · delaminatedUPPER SKINS ON THE TRAILING EDGE WEDGES OF THE NR 9, 10, AND 12 SLATS WERE FOUND WITH DELAMINATED AREAS. REPAIRED PER ERA 365048-14AD.Jun 16, 1998 · N119DL · Boeing 767332 · Leading Edge DevicesSDR DL76S980069Light · inoperativeFOUND ON LAYOVER, LT OVERWING EMERGENCY LIGHTS INOP. RELAMPED, CHECKS GOOD.Jan 10, 1998 · N119DL · Boeing 767332 · Emergency LightingSDR DL76S972328Floorbeam · corrosionCORROSION WAS FOUND ON THE UPPER CAP AT FS 1480 AT LBL 30 AND ENTIRE RT SIDE. REPAIRED PER ERA330975-14.Nov 11, 1997 · N119DL · Boeing 767332 · Fuselage Main, Floor BeamSDR DL76S972327Floorbeam · puncturedA NEW UPPER TEE CHORD WAS ADDED TO THE BEAM EXTRUSION PER SRM. DURING ACCOMPLISHMENT THE FLOORBEAM WEB WAS PUNCTURED. REPAIRED PER ERA 330971-14.Nov 11, 1997 · N119DL · Boeing 767332 · Fuselage Main, Floor BeamSDR DL76S972326Seat Tracks · crackedSEAT TRACKS AT LBL AND RBL 54 WERE FOUND CRACKED IN THE VERTICAL WEB OF THE UPPER CHORD AT FS 786. REPAIRED PER ERA330946-14.Nov 11, 1997 · N119DL · Boeing 767332 · Fuselage, Seat/Cargo Attach FittingsSDR DL76S972325Keel Beam · corrodedLT KEEL BEAM HAD CORROSION AT STA 917. REPAIRED PER ERA 330983-14.Nov 11, 1997 · N119DL · Boeing 767332 · Fuselage Main, KeelSDR DL76S972324Floorbeam · crackedFS 246 FLOORBEAM WEB WAS FOUND WITH VERT CRACK APPROX 3 LONG AT RBL 20. THE OVERLYING STIFFENER WAS ALSO CRACKED. REPAIRED PER ERA 330992-14.Nov 11, 1997 · N119DL · Boeing 767332 · Fuselage Main, Floor BeamSDR DL76S972265Frame · crackedFORWARD CARGO COMPARTMENT STA 544 FRAME UPPER CHORD HAD AN 8 INCH CRACK IN THE RADIUS OF THE HORIZONTAL FLANGE AT RBL 16. REPLACED FLANGE.Oct 26, 1997 · N119DL · Boeing 767332 · Fuselage Main, FrameSDR DL76S970885Wedge · delaminatedTHE NR 9 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE THE UPPER SKIN DELAMINATED 4 FROM THE T/E AND 34 FROM THE INB'D END. THE DAMAGE AREA MEASURES 6 FWD-AFT AND 5.5 INBD-OUTBD. THE TRAILING EDGE WEDGE IS M/F 0.016 5052-H38 FACE SHEETS WITH A METAMay 8, 1997 · N119DL · Boeing 767332 · Leading Edge DevicesSDR DL76S970750Sensor · out of adjustAFTER T/O OUT OF ATL, GEAR HANDLE FAILED TO COME UP. ACARS DID NOT SENSE AIRBOURN AND LATER GOT TAIL SKID LIGHT, RETURN TO ATL. SHIMMED TRUCK TILT SENSORS S245/S246 ON RT MLG. RAN GEAR CHECKS, OK. SENSORS S238/S260 OK ON LT MLG.Apr 24, 1997 · N119DL · Boeing 767332 · Landing Gear Position and WarningSDR DL76S970335Idg · reqd serviceLOST LEFT ENG GEN AT ABOUT 200 FT AFTER T/O, LOST RT GEN AT APPROX 1,000 FT. RETURNED TO BOS. RT IDG BPCU FAULTS LOW OIL PRESS, IDG HI DELTA TEMP/IDG/PMG WIRING PER 24-20-00. FOUND RT DPI EXTENDED, REQUIRES IDG REPLACEMENT. CHECKED SERV OK. FWD TO MCO ANFeb 24, 1997 · N119DL · Boeing 767332 · AC Generator-AlternatorSDR DL76S962120Hyd Line · chafedL HYD QTY EICAS MSG. LT ENG HYD QTY 0.46 RF. LT ENG PRIMARY AND DEMAND PUMPS OFF. REPLACED HYDRAULIC LINE AT #1 ENGINE HYDRAULIC PUMP. SYSTEM CHECKS NORMAL.Sep 16, 1996 · N119DL · Boeing 767332 · Hydraulic System, MainSDR DL76S960772Mec · malfunctionedTAKEOFF ABORTED AT 80 KTS, RT ENG ONLY 88 PERCENT, N1 ACC WAS ALSO SLOW. REPLACED RT ENG, MEC LEAK CHECKED PERFORMED, ENG RUN PER PFHB AND ALL IND NORMAL.Apr 5, 1996 · N119DL · Boeing 767332 · Fuel Control/Turbine EnginesSDR DL76S954306Bulb · failedDURING L/O, FOUND AFT RT DOOR EMERGENCY LIGHT INOP AND LT WING SLIDE LIGHT INOP. RELAMPED BOTH, CKS GOOD.Nov 8, 1995 · N119DL · Boeing 767332 · Emergency LightingSDR DL76S951720Trunnion · fracturedAFTER ARRIVAL AT GATE WHILE AIRCRAFT WAS MOTIONLESS, THE LEFT MAIN LANDING GEAR TRUNNION OUTER CYLINDER FRACTURED AT THE AFT TRUNNION BORE. THE LOWER 180 OF THE AFT END SEPARATED REMOVING A 6 INCH LONG PIECE. INITIAL VISUAL EXAMINATION REVEALS SEVERE CORROSIApr 21, 1995 · N119DL · Boeing 767332 · Main Landing Gear Attach SectionSDR DL76S950387Wedge · delaminationFOUND DURING J-2 LETTER CHECK, DELAMINATION AREA ON LOWER SKIN OF NR 4 FLAP T/E WEDGE. REPAIRED PER SRM 51-70-07, AND PAINTED AREA.Jan 26, 1995 · N119DL · Boeing 767332 · Trailing Edge Flaps
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