N994DL
Service difficulty reports · 236
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 = 'N994DL' AND registry_match = 'registration' 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 n_number = 'N994DL' AND registry_match = 'registration' 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 DALA2016031602021Cusp Web · corrodedCORROSION ON LT CUSP WEB X=55 TO X=60 BETWEEN BS 1036 TO BS 1038 AT FLOOR CABIN STRUCTURE. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-14, 51-30-5, 51-10-3 PAR 21, 14 AND 38.SDR DALA2016031602006Membrane · corrodedCORROSION FOUND ON MEMBRANE, X -52 TO -56, BS 210 - 218. REPAIRED IAW SRM 51-10-3, PAR 26, 14, 21 AND 38 AND ER/A 511165-14MA, REV C.SDR DALA2016031301896Cusp Web · corrodedDUE TO EXCESSIVE CORROSION ON CUSP WEB X=-54 TO X=-60 BETWEEN BS 806 AND 817. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-13, FIG 131A-2, 51-10-3 PAR 14 AND 21, 51-30-2.SDR DALA2016031201891Skin · damagedLIGHTNING STRIKE ON LT FUSELAGE SKIN WINDOW BELT LOWER EDGE AND LOWER CORNER BETWEEN BS 389 TO BS 408. DAMAGE WAS BLENDED OUT, IAW SRM 53-05, FIG 111. AREA WAS MEASURED: BLENDED OUTS WERE FOUND IN ZONE 3 AND NO CRITICAL ZONE THEREFORE ALL ARE WITHIN LIMITS ISDR DALA2016031101871Doubler · wornWEAR ON FWD/AFT DOUBLERS ON LOWER CORNERS AT FWD CARGO COMPARTMENT DOOR. DOUBLERS WERE REMOVED, NEW DOUBLERS WERE FABRICATED, TREATED, PAINTED AND INSTALLED IAW SRM 51-30-2, 51-10-3, PAR 21 AND 14, ER/A 486624-14MA, REV ORIGINALSDR DALA2016031101867Spar · damagedDURING NDT INSPECTION A DISCREPANT AREA WAS FOUND 7 DIFFERENT FASTENERS OF THE PSE AT LT LOWER WING SKIN REAR SPAR BETWEEN BS XRS =162 TO XRS=168. THIS NRC WILL BE ATTENDED BY THE ER/A 543200-14AD. REV ORIGINAL. FROM THE SECTION II.SDR DALA2016031101866Spar · damagedDURING NDT INSPECTION A DISCREPANT AREA WAS FOUND 7 DIFFERENT FASTENERS OF DE PSE AT RT LOWER WING SKIN REAR SPAR BETWEEN XRS=162 TO XRS=168. REPAIRED IAW ER/A 543200-14AD. REV, ORIGINAL FROM THE SECTION II.SDR DALA2016031101865Seat Track · corrodedCORROSION ON PLUG AT RT SEAT TRACK, X=-54 BS 506-509 AT FLOOR STRUCTURE. PLUG WAS REMOVED, NEW PLUG WAS INSTALLED IAW SRM 51-30-1, 53-10-3, PAR 21, 14, 53-05, FIG 4A.SDR DALA2016031101864Pan · crackedCRACK ON LT RING PAN UPPER FWD CORNER BETWEEN BS 579 TO 598. RING PAN WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 53-05, FIG 122, 51-10-3, PAR 14,21 AND ER/A 487747-14MA, REV A AND ER/A 493648-14MA, REV A. LONG OF CRACK IS 0.450".SDR DALA2016031101863Seat Track · corrodedCORROSION ON LT PLUG SEAT TRACK, X=54, BS 579. PLUG WAS REMOVED, NEW PLUG WAS INSTALLED IAW SRM 51-30-1, 53-10-3, PAR 21, 14, 53-05, FIG 4A.SDR DALA2016031101862Seat Track · corrodedCORROSION ON LT PLUG SEAT TRACK X=22, BS 579-826. PLUG WAS REMOVED, NEW PLUG WAS INSTALLED IAW SRM 51-30-1, 53-10-3 PAR 21, 14, 53-05 FIG 4A.SDR DALA2016031101861Pan · crackedCRACK ON LT RING PAN UPPER FWD CORNER BETWEEN BS 927 TO 946. RING PAN WAS REPAIRED IAW SRM 51-30-2, 51-30-5 53-05, FIG 122, 51-10-3, PAR 14,21 AND ER/A 487747-14MA REV A AND ER/A 493648-14MA, REV A.SDR DALA2016031101860Pan · crackedCRACK ON LT RING PAN UPPER AFT CORNER BETWEEN BS 984 TO 1003. RING PAN WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 53-05, FIG 122, 51-10-3, PAR 14, 21 AND ER/A 487747-14MA REV A AND ER/A 493648-14MA, REV A.SDR DALA2016031101859Pan · crackedCRACK ON LT RING PAN LOWER FWD CORNER BETWEEN BS 750 TO 769. RING PAN WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 53-05, FIG 122, 51-10-3, PAR 14,21 AND ER/A 487747-14MA, REV A AND ER/A 493648-14MA, REV A.SDR DALA2016031101856Pan · crackedCRACK ON LT RING PAN UPPER FWD CORNER BETWEEN BS 769 TO 788. RING PAN WAS REPAIRED IAW SRM 51-30-5, 51-30-2 53-05, FIG 122, 51-10-3 PAR 14,21 AND ER/A 487747-14MA, REV A AND ER/A 493648-14MA, REV A.SDR DALA2016031101855Pan · crackedCRACKED LT RING PAN UPPER FWD CORNER BETWEEN BS 313-332 AND AFT LWR CORNER BETWEEN BS Y=427-446. RING PAN WAS REPAIRED IAW SRM 53-05, FIG 122, 51-30-2, 51-30-5, 51-10-3 PAR 14, 21 ON BS 427-446 AND BS 313-332 HFEC WAS ACCOMPLISHED ON RING PAN, UPPER FWD CORNESDR DALA2016031101852Pan · crackedCRACKED RT RING PAN AFT UPPER CORNER BETWEEN BS 750-769, 1117-1136, 1136-1155, 1174-1193, 1212-1231. RING PAN RT AFT UPPER CORNER BETWEEN BS 750-769, BS 1117-1136, BS 1136-1155, BS 1174-1193, BS 1212-1231 WERE REPAIRED IAW SRM 51-30-2, 51-30-5, SRM 53-05, FISDR DALA2016031101851Pan · crackedCRACKED RT RING PAN FWD LOWER CORNER BETWEEN BS 807-826, 1022-1041, 1079-1098. RING PAN RT FWD LWD CORNER BETWEEN BS 807-826, 1022-1041, 1079-1098 WERE REPAIRED IAW SRM 53-05, FIG 122 AND SRM 51-30-2, 51-30-05, ERA`S 493648-14MA REV A 487747-14MA, REV A.SDR DALA2016031101849Pan · crackedCRACKED RT RING PAN FWD UPPER CORNER BETWEEN BS 351-370, 370-389, 845-864. RING PAN RT FWD UPPER CORNER BETWEEN BS 351-370, 370-389, 845-864 WERE REPAIRED IAW SRM 53-05, FIG 122 AND 51-30-2, 51-30-05, ERA 487747-14MA, REV A 493648-14MA, REV A.SDR DALA2016031101848Seat Track · corrodedCORROSION ON PLUG AT SEAT TRACK X=-22, BS 1288-1291 AT FLOOR STRUCTURE. PLUG WAS REPLACED IAW SRM 51-30-1, 51-10-3, PAR 21 AND 14 AND 53-05, FIG 4A.SDR DALA2016031101847Skin · not reportedDISCREPANT AREA WAS FOUND ON FUSELAGE SKIN, EXTERNAL DOUBLER REPAIR AT BS 1418 AND BETWEEN LONGERON 1 AND 3 RT. THE ER/A 498486-14, REV. ORIGINAL WAS GENERATED AND FROM SECTION I: ER/A REVISION REQUIRED, AMOC IAW SID AD 2004-11-07.SDR DALA2016030701692Skin · wornWORN INBD AFT CORNER ON RT WING OTBD FLAP OTBD GUIDE VANE. INBD AFT CORNER ON RT WING OTBD FLAP OTBD GUIDE VANE WAS REPAIRED IAW SRM 57-03D, PAR II.SDR DALA2016020900940Structure · crackedLEFT WHEEL WELL FWD OF GEAR DOOR BELOW GEAR DOOR SENSOR IS CRACKED. PERFORMED REPAIR IAW ERA 543814-14, REV ORIG SECTION II PERMANENT REPAIR.SDR DALA2016020900939Channel · crackedRIGHT WHEEL WELL DOOR JAMB CHANNEL, FWD OF GEAR DOOR CRACKED BELOW DOOR SENSOR. REMOVED WHEEL WELL DOOR JAMB CHANNEL. DRILLED UP REPLACEMENT JAMB AND BEGAN INSTALLING WHEEL WELL DOOR JAMB. PERFORMED REPAIR AS PER ERA 543814-14 REV ORIG SECTION II PERMANENT REPSDR DALA2016020800930Wire · brokenTHE AFT EQUIPMENT BAY EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE RETERMINATED 2 CONNECTORS AND THE LIGHTS CHECKED OK.SDR DALA2015061703810Battery Pack · malfunctionedDURING LINE CHECK, MAINTENANCE FOUND THEY COULD NOT CONTROL THE EXTERIOR EMERGENCY LIGHTING AT THE OVERWING EXIT, IT WOULD REMAIN ON WHEN THE CONTROL SWITCH WAS TURNED OFF. MAINTENANCE REPLACED THE BATTERY PACK FOR THE NOTED LIGHT AND THE OPS CHECK WAS GOOD.SDR DALA2015033002479Power Supply · inoperativeMAINTENANCE FOUND RT AFT BATTERY POWER SUPPLY INOPERATIVE, EMERGENCY LIGHTING. BATTERY POWER SUPPLY WAS REPLACED IAW AMM 33-53.SDR DALA2015022401643Pin · pulledDURING CHECK, MAINTENANCE FOUND THE L-1 DOOR SLIDE PINS PULLED. MAINTENANCE R & R THE L-1 DOOR SLIDE.SDR DALA2015020400899Engine · failedFLIGHT RETURNED TO DEPARTURE WITH THE NR 1 ENGINE HAVING PROBLEMS. FLIGHT CREW REPORTED ALL PARAMETERS WENT TO -0-. THE NR 2 ENGINE WAS SHUTDOWN. MAINTENANCE FOUND METAL IN TAIL PIPE AND HAVE REPLACED THE ENGINE.SDR DALA2014081104478Connector · disconnectedDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 24DE INOPERATIVE. FOUND CONNECTOR IN THE WIRE HARNESS UNPLUGGED, CONNECTED AND FUNCTIONALLY CHECKED THE SYSTEM.SDR DALA14032730994Wire · brokenDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING FOR THE EQUIPMENT BAY IN THE TAIL COMPARTMENT WAS INOPERATIVE. MAINTENANCE FOUND WIRES BROKEN AT THE TERMINAL. THEY RETERMINATED THE WIRE AND THE SYSTEM RETURNED TO NORMAL OPERATION.SDR DALA2016111008683Doubler · corrodedRADIO ALTIMETER ANTENNA DOUBLER CORRODED, NEW DOUBLER FABRICATED AND INSTALLED.SDR DALA13065470994Battery Pack · inoperativeDURING LINE CHECK, NOTED LT & RT OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS AND OPS CHECKED GOOD.SDR DALA13016280994Coalescer Bag · odorAFTER DEPARTING, DURING CLIMBOUT, THE FLIGHT RETURNED WHEN F/A REPORTED STRONG ELECTRICAL ODOR THROUGHOUT THE CABIN BUT PRIMARILY NEAR THE FWD GALLEY. PILOT REPORT ALSO INDICATES "WE SMELLED POLLEN IN COCKPIT". MX ACCOMPLISHED AN ELECTRICAL SMOKE INSPECTION ISDR DALA13013430994Skin · scratchedBLEND OUT IN SKIN AT BS 207 S18L. BLEND SCRATCH, OUT OF LIMITS. REPAIRED IAW ERA 508147-14 AND SRM 53-04-5 AND 53-04-1.SDR DALA13013030994Threshold · corrodedDURING SCHEDULED MX, CORROSION ON CARGO DOOR THRESHOLD FROM BS 1155 - 1212. REMOVED CORROSION, FOUND TO BE IN LIMITS IAW SRM 53-01, 53-05, FIG 123, SHEET 2. R & R DAMAGED DOUBLERS, FABRICATED, AND INSTALLED IAW SRM 53-05, 51-30-4.SDR DALA13013020994Threshold · corrodedDURING SCHEDULED MX, CORROSION WAS FOUND ON THE MID CARGO BAY DOOR THRESHOLD PLATE AT BS 636-693. R & R CORRODED THRESHOLD PLATE IAW SRM 53-05.SDR DALA13013010994Threshold · corrodedDURING SCHEDULED MX, CORROSION WAS FOUND AT THE AFT CARGO BAY THRESHOLD BS 1179-1189. R & R IAW SRM 53-03.SDR DALA13008290994Battery Pack · inoperativeDURING SERVICE CHECK, FOUND COCKPIT/L1/R1 OVERHEAD EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM. OPERATION CHECKS GOOD.SDR DALA13005820994Skin · damagedFUSELAGE SKIN DAMAGE BETWEEN STA 598 AND STA 617 AND BETWEEN STR 29R AND 27R. ACCOMPLISHED SECTION 1 TIME LIMITED REPAIR INSTRUCTION IAW ERA 511149-14, REV O. INSTALLED REPAIR IAW PERMANENT REPAIR INSTRUCTIONS ON ERA 511149-14 REV O.SDR DALA13001270994Sill · corrodedC-1 CARGO DOOR SILL & PAN CORRODED. REPAIRED IAW SRM 53-05, FIG 44 AND ER/A 510399-14 REV ORIG.SDR DALA13001260994Threshold · corrodedCORROSION ON C-1 DOOR THRESHOLD. REPAIRED IAW SRM 53-05, FIG 44 AND ERA 510399-14 REV ORIG.SDR DALA13001280994Sill · corrodedC-1 DOOR SURROUND STRUCTURAL PAN & LOWER SILL CORRODED. PERM REPAIR PRI 510399-14, REV 0-REV 1. FINAL ER/A 510399-14, REV ORIG ALL STEPS C/W AND MATCH PRI 510399-14, REV 0-REV 1. ER/A 510399-14 REV ORIG READ AND MATCHED.SDR DALA12007950994Wire · brokenDURING SERVICE CHECK, MX FOUND EMERGENCY ESCAPE PATHWAY LIGHT ROW 12D INOPERATIVE. MX REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT UNDER SEAT 12D. OPS CHECKS GOOD.SDR DALA1238990994Unknown · odorJUST PRIOR TO LEVEL OFF, THE FLIGHT CREW NOTICED A DISTINCT ELECTRICAL ODOR THROUGHOUT THE AIRCRAFT. FLIGHT ATTENDANTS AND PILOTS REPORTED MILD EYE IRRITATION. ODOR DISSIPATED AFTER 10 MINUTES AND NO SECONDARY INDICATIONS OF SMOKE OR HAZE WERE NOTED. STILL SDR DALA1231620994Lamp · inoperativeFLIGHT CREW FOUND ON PDC, TAIL COMPARTMENT LIGHTS INOPERATIVE. TROUBLESHOT AND RELAMPED. OPS CHECKED GOOD.SDR DALA1214240994Inlet · contaminatedFLIGHT CREW REPORTED BURNING OIL SMELL IN CABIN WITH APU INLET WET AND APU LEAKING OIL. MAINTENANCE CHECKED APU FOR LEAKS AND OIL CAP SEAL CONDITION. NO LEAKS NOTED. PERFORMED DUCT BURNOUT. CLEANED INLET. AIRCRAFT OKAY FOR SERVICE.SDR DALA1212840994Trans Panel · damagedAFT CARGO BIN NR 6 HAS HOLE IN THE TRANSITION FLOOR AFT OF DOORWAY 3, IN BY 3/4 INCH. REPAIRED TRANSITION FLOOR PANEL UPPER SRM/DRD 53-24-0D. TIME LIMITED INSTRUCTIONS. REPAIR OF TRANSITION PANEL ACCOMPLISHED ON LOG # 244776006.SDR DALA13013210994Floor Panel · puncturedPUNCTURE HOLE AT TRANSITION FLOOR PANEL IN AFT BAG BIN. PUNCTURE IS 3 X 1.75. FABRICATED FWD CARGO BAY FLOOR PANEL NR 121NF, FROM 5040-400005GC2 ALUMINUM COMPOSITE LOT 1063129 IAW SRM 51-10-11, FIG 1 AND INSTALLED IAW AMM 25-52-01-201, SECT. 3. B. (1)(5). SDR DALA1169150994Skin · crackedFUSELAGE SKIN CRACKED AT STA 1418 S-2R. CRACK EMANATING AFT OF THE UPPER MOST FASTENER HOLE COMMON TO SHEAR TIE. REPAIRED PER ERA 498486-14 REV ORIG.
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