N984DL, cancelled Nov 9, 2020
Service difficulty reports · 250
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 = 'N984DL' AND deregistration_id = 'N984DL-2020-11-09' 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 = 'N984DL' AND deregistration_id = 'N984DL-2020-11-09' 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 DALA2019062803910Connector · disconnectedEMEG LIGHTS INOP BETWEEN ROW 13 & 23. RECONNECTED CONNECTOR AT FLOOR AT SEAT 13 ED OPS CK GOOD. (LP5917986)SDR DALA2019031501702Bracket · brokenWHILE WORKING JOB CARD 0591-0301 FOUND AUX HYD PUMP WIRE HARNESS BRACKET BROKE. REF EA 09-457000-03AD FIG 2 ITEM 7. INSTALLED BRACKET TO WIRE HARNESS PER EA 09-457000-03AD FIG 2. A/C OK FOR SVC. BRACKET 9D0062-3S10-12. SDR REPORTED DUE TO BEING AD RELATED. (LPSDR DALA2018032401860Fire Warning · false activationRIGHT ENGINE LOOP B LIGHT ILLUMINATED DURING FLIGHT PER QRH LOOP A SELECTED. NORMAL FIRE TEST LOOP DETECTOR LEFT IN A POSITION FOR REMAINDER OF THE FLIGHT. SELECTED RT ENG FIRE LOOP TO BOTH AND RAN TEST OPS NORMAL NO FAULT NO HISTORY OK FOR SVC.SDR DALA2017082306345Battery Pack · not reportedOVERWING EMERGENCY EVACUATION LIGHT BATTERY PACK OPS CHECK. REPLACED OVERWING EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK IAW AMM 33-53-00 PERFORMED SATISFACTORY OPS CHECK.SDR DALA2017082106306Bearing · nickedLEFT ELEVATOR NR 1 HINGE BEARING NICKED. REMOVED THE HINGE BEARING HOUSING IAW OVERHAUL MANUAL 27-30-1. REMOVED AND REPLACED THE BEARING AND REINSTALLED HINGE HOUSING IAW CMM 27-30-1 AND SOPM 20-10-7.SDR DALA2017081806298Seal · damagedON INSTALLATION OF LEFT ELEVATOR TO HORIZONTAL STAB, DAMAGE WAS FOUND ON THE AFT SPAR REAR CAP, XE225. REPAIRED LT HORIZONTAL STAB T/E SPAR SEAL IAW ER/A 398032-14MA.SDR DALA2017081706296Cusp Web · crackedON REMOVAL OF THE RT SIDE FLOOR WEB, A CRACK WAS NOTICED AT FWD CORNER CUT OUT. REPAIRED THE CUSP WEB AT BS 807 IAW SRM 53-05, PAR 144, FIG 131A-21, DWG 9910151, REV BU, REV CH, AND DWG 9930538 REV CE.SDR DALA2017062604970Wire · damagedACFT DIVERTED, DURING CLIMB OUT, PASSING THROUGH 26K, A STRONG ACRID ODOR BECAME APPARENT IN THE COCKPIT. FLIGHT ATTENDANTS REPORTED SAME ODOR IN CABIN. BEGAN DESCENT DIVERSION. AFTER APPROXIMATELY 1-1.5 MINUTES BOTH OIL TEMP HIGH LIGHTS ILLUMINATED. THROTTSDR DALA2017060704535Structure · puncturedDURING A SERVICE CHECK, FOUND A DENT WITH A PUNCTURE ON BACKSIDE OF RT NR 1 SLAT, 45 INCHES FROM INBOARD, 2.25 X 1.87 L X .195 DEEP. REMOVED AND REPLACED THE SLAT IAW AMDS CARD 2700-4224-RH-01.SDR DALA2017012300562Skin · crackedHORIZONTAL STABILIZER UPPER RT AFT SKIN PANEL CRACKED. DRILLED END CRACK 0.250 DRILLED IAW SR09550028. ENLARGE STOP DRILL IAW SR09550028 STEP 42. HFEC INSP AREA IAW NDTM 06-1001.001 NO DEFECTS NOTED. ALODINED & PRIMED. SEALED AREA REINSTALLED FILLER AND APPLISDR DALA2017012300572Cam · no testTAILCONE RELEASE MECHANISM CAM FAILS TORQUE CHECK IAW STEP 12 OF AMDS 5350-01077-0101. ADJUSTED IAW AMM 53-53-02-201, OPS CHECKED GOOD, OK FOR SERVICE IAW AMDS 5350-01077-0101.SDR DALA2017010400078Apu · contaminatedDURING THE BOARDING PROCESS, THE CREW NOTIFIED MAINTENANCE OF A BURNING SMELL IN THE CABIN. THE APU WAS RUNNING AND THE PACKS WERE BEING OPERATED TO WARM THE CABIN. MAINTENANCE FOUND THE APU INLET CONTAMINATED WITH DE-ICE FLUID. THE APU INLET AND DOOR ASSEMBLYSDR DALA2016120109436Fastener · damaged1R DOOR GIRT BAR HOLDER DETACHED FROM DOOR. ACARS INBD WRITE UP. REPLACED FASTENERS ON GIRT BAR HOLDER. CKS GOOD.SDR DALA2015081604983Cusp Web · corrodedCORROSION ON CUSP WEB BS 715-718 BETWEEN X -54 TO -60 AT CABIN PAX IN REF CARD 149, ZONE 201. REPAIR WAS ACCOMPLISHED IAW SRM 53-05, FIG 131A -13.SDR DALA2015072804733Vane · damagedAFTER LANDING , WHEN FLAPS WERE RAISED TO 0 THE RT FLAP INDICATOR READS 5 AND LT FLAP INDICATOR READS 0, FELT SLIGHT BINDING WHEN ATTEMPTING TO RETRACT SLATS SO LT FLAPS OUT. INBD AND OTBD FLAP VANE GUIDE OF INBD FLAP WERE REPLACED FOR A SERVICIABLE FLAP VANSDR DALA2015072504706Heater Blanket · corrodedCORROSION ON RT WING HEATER BLANKET AROUND FUEL ACCESS PANEL CUTOUT. THE HEATER BLANKET WAS REPLACED IAW AMM 30-80-02-401. TESTED THE HEATER BLANKET, FOUND OK IAW AMM 30-80-02-501.SDR DALA2015072404640Bushing · corrodedCORROSION ON REPAIR BUSHINGS AND ELONGATED BUSHINGS ON RT HEATER BLANKET T/E. DAMAGE BUSHINGS WERE REPLACED IAW ER/A 537709-14AD, REV "A" AND EA: 09-070683-03, AD REV L. MAJOR REPAIR.SDR DALA2015072404637Skin · corrodedCORROSION FOUND BETWEEN FUSELAGE SKIN AND INBD DOUBLER AT AFT WASTE LAVATORY SERVICE PANEL. CORROSION WAS REMOVED IAW ETI-88-15-224, REV 1 AND ER/A 536427-14, REV ORIGINAL.SDR DALA2015072404630Skin · crackedA 0.187 INCH CRACK ON FUSELAGE SKIN, BS 1418 BETWEEN LONGERONS 2 - 3L AND A CRACK OF 0.531" BETWEEN LONGERON 1 AND 2R. FUSELAGE SKIN WAS REPAIRED IAW ER/A 536455-14AD, REV ORIGINAL AND ETI 88-15-204, REV 2.SDR DALA2015072304585Angle · crackedCRACKED SPLICE ANGLE ON CANTED FRAME STA Y=1463 AND RBL 18. REPAIRED IAW ERA 536514-14, REV.SDR DALA2015072304581Trunnion · corrodedCORROSION AND BLEND OUTS IN LT RETRACT ACTUATOR SUPPORT FITTING BUSHING BORE. CORROSION ON BUSHING BORE WAS REWORKED WITH FINAL DIMENTION: ID 2.2735" WITHIN LIMITS IAW DWG SR09570087, REV B FPI WAS ACCOMPLISHED LT RETRACT ACTUATOR SUPPORT FITTING BUSHING BORESDR DALA2015072304580Trunnion · corrodedCORROSION IN RT RETRACT ACTUATOR SUPPORT FITTING BUSHING BORE. CORROSION ON BUSHING BORE WAS REWORKED WITH FINAL DIMENTION ID 2.377" WITHIN LIMITS IAW DWG SR09570087, REV B, FPI WAS ACCOMPLISHED RT RETRACT ACTUATOR SUPPORT FITTING BUSHING BORE NO CRACKS WERE SDR DALA2015072204555Frame · crackedCRACKED FRAME BS 1497 . FRAME WAS REPAIRED IAW ER/A 536485-14, REV ORIGINAL AND ETI-88-15-234, REV 2.SDR DALA2015072204547Pan · crackedCRACKED PAN ON PAX DOOR BETWEEN BEAM 8 AND FWD EDGE. THE DOOR WAS REPAIRED IAW SRM 52-05D, FIGURE 18A.SDR DALA2015072104509Cargo Track · corrodedCORROSION FOUND ON THE LT CARGO TRACK BS 1193 - 1250. THE CARGO TRACK WAS REPLACED.SDR DALA2015072104503Intercostal · crackedCRACKED INTERCOSTAL BETWEEN BS 1271 - 1288. THE INTERCOSTAL WAS REMOVED IAW SRM 51-30-2, FABRICATED IAW DWG 9936580, REV BT, AND INSTALLED IAW SRM 51-30-2.SDR DALA2015072004495Beam · corrodedCORROSION FOUND ON THE BEAM BETWEEN BS 685 - 690 OF THE MID CARGO LOWER DOOR FRAME. THE BEAM WAS REPAIRED IAW SRM 53-05, FIG 123. MAJOR REPAIR.SDR DALA2015072004490Longeron Splice · corrodedCORROSION ON THE LONGERON SPLICE, BS 1287 - 1309, LONGERON 30. THE LONGERON SPLICE WAS REPLACED IAW SRM 51-10-4, 51-10-3 PAR 14 AND 21, 51-30-2 AND 51-30-5.SDR DALA2015071904487Access Panel · corrodedCORROSION ON THE COUNTERSINK AND SETTLEMENT AREA OF THE FUEL ACCESS PANEL 1335C. THE CORROSION WAS REMOVED AND FOUND OUT OF LIMITS. THE ACCESS PANLE WAS REPLACED IAW SRM 51-22-2A.SDR DALA2015071904482Finger Doubler · corrodedCORROSION ON FUSELAGE SKIN FINGER DOUBLER BELOW LONGERON 26L, BS 579 - 598. THE FINGER DOUBLER WAS REPLACED IAW SRM 51-30-2, SRM 51-30-5, SRM 51-10-4, AND SRM 51-10-3 PAR 14, 21 & 33.SDR DALA2015071904475Intercostal · crackedCRACKED INTERCOSTAL BELOW HYD MANUAL PUMP AT LT MLG WHEEL WELL. THE INTERCOSTAL WAS REMOVED, REPAIRED, AND INSTALLED IAW SRM 51-30-2, 51-30-5, 51-10-3 PAR.21 AND 14, 51-10-2 AND 53-01.SDR DALA2015071904474Angle · crackedCRACKED ANGLE BEHIND LT SIDE WALL SUPPORT AT BS 1007, Z -6. THE ANGLE WAS REPAIRED IAW SRM 53-01, 51-30-2, 53-01, FIG 2, 51-10-3 PAR 14 AND 21.SDR DALA2015071904473Intercostal · corrodedCORROSION ON INTERCOSTAL FROM BS 1380 - 1390 LONGERON 26L. THE INTERCOSTAL WAS REPLACED IAW SRM 53-14-4, FIG 1, NDT SPM 04-00-07, FIG 3, PAR 5, SH 1 AND 2.SDR DALA2015071904472Angle · crackedCRACKED ANGLE BETWEEN VSS 2 - 26 TO -15 AT VERTICAL STABILIZER INNER STRUCTURE. THE ANGLE WAS REPLACED IAW SRM 51-30-05, 51-30-2, 51-10-3 PAR 21 AND 14 SRM 51-10-2 AND DWG 5912188, REV BD.SDR DALA2015071804467Beam · corrodedCORROSION ON THE UPPER DOOR FRAME BEAM BETWEEN BS 1174 - 1193 IN THE AFT CARGO BAY. THE BEAM WAS REPLACED IAW SRM 51-30-5, 51-10-4 AND 51-10-3 PARA 21, 14 AND 36.SDR DALA2015071804466Door Frame · corrodedCORROSION ON LOWER DOOR FRAME IN THE FWD CARGO BAY. REPAIRED IAW SRM 53-05, FIG 44A.SDR DALA2015071804465Doubler · crackedCRACKED INNER PRODUCTION DOUBLER, BS 693 BETWEEN LONGERONS 23-24R. THE DOUBLER WAS REWORKED IAW SRM 53-05, FIG 109. TREATED AND PAINTED IAW SRM 51-10-3, PAR 14, 21.SDR DALA2015071704444Door Frame · crackedCRACK ON UPPER DOOR FRAME FOR THE RT AFT OVERWING EMERGENCY DOOR. THE DOOR FRAME WAS REPAIRED IAW SRM 53-05, FIG 32 AND 51-01, PAR 4, 21.SDR DALA2015071704436Tab · dentedRT ELEVATOR GEARED TAB, DENTED ON UPPER SURFACE. THE TAB WAS REPAIRED IAW SRM 55-04.SDR DALA2015071704431Longeron · corrodedCORROSION FOUND ON LONGERON 24L BETWEEN BS 1338 - 1380. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.SDR DALA2015071704430Frame · crackedWEAR AND A CRACK WAS FOUND ON FRAME BS 1343 LONGERONS 26L - 26R. THE FRAME WAS REPAIRED IAW ERA 094719-14MA, REV A.SDR DALA2015071504376Floor Panel · delaminatedDELAMINATED FLOOR PANEL IN CABIN PAX. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.SDR DALA2015071504375Rib · crackedCRACKED RIB XFS 30.00 IN VERTICAL STABILIZER L/E INNER STRUCTURE. RIB REMOVED IAW SRM 51-30-2 AND 51-30-5 AND A NEW RIB WAS DRILLED IAW SRM 51-10-4, AND REPAIRED IAW SRM 55-02, FIG 27. NEW RIB INSTALLED IAW SRM 51-30-2 AND 51-30-5.SDR DALA2015071404356Frame · corrodedCORROSION ON FRAME AND FRAME CLIP AT BS 1287 BETWEEN LONGERONS 28LT AND 28RT IN AFT CARGO COMPARTMENT. SUMMARY CORROSION WAS REMOVED IAW SRM 51-10-3 THEN NDT SPM 04-00-01 WITH AN ORIGINAL THICK OF 0.063" ON FRAME 1287 AND REM. THICK 0.004 AND IT IS OUT OF LIMSDR DALA2015071404355Rib · crackedCRACKED LT RIB BS ZFS 36.50 AT VERTICAL STABILIZER L/E INNER STRUCTURE. RIB WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4, 51-10-3, PAR 14, 21.SDR DALA2015071404354Rib · crackedCRACKED RIB STA ZFS 49.62 AT VERTICAL STABILIZER. L/E INNER STRUCTURE, RIBS WERE REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-3 PAR 14, 21 51-10-4.SDR DALA2015071304335Cusp Web · damagedWAVINESS IN LEFT CUSP WEB BETWEEN X 44 - 54, BS 1174 - 1250. CUSP WEB WAS REPAIRED IAW SRM 51-30-1, SRM 51-30-2, SRM 53-05, FIG 131A-6, SRM 51-10-3, PAR 14 & 21 AND SRM 51-30-5.SDR DALA2015071304334Seat Track · wornWEAR ON THE LEFT SEAT TRACK X 44 BETWEEN BS 1188 - 1196. THE SEAT TRACK WAS REPLACED IAW SRM 51-30-1, SRM 53-05, FIG 4B-1, NDT SPM 04-00-07, PAR 5, FIG 3 SH-1AND 2, SRM 53-05, FIG 4F, SRM 51-10-4, SRM 51-10-3, PAR 14 AND 21, AND SRM 51-30-5.SDR DALA2015071404353Door Frame · corrodedCORROSION ON REPAIR OF LWR DOOR JAMB AT AFT CARGO COMPARTMENT. DOUBLER WAS REPLACE IAW SRM 53-05, FIG 123. PRIMARY STRUCTURE.SDR DALA2015071304331Intercostal · crackedCRACKED INTERCOSTAL AT BS 886 - 905 LONGERON 17L. THE INTERCOSTAL WAS REPAIRED IAW SRM 53-01, FIG 2.
Back to N984DL, cancelled Nov 9, 2020