N981AT
Service difficulty reports · 199
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 = 'N981AT' 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 = 'N981AT' 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 DALA2024110110568Pan · crackedCRACK ON INNER PAN FWD/AFT UPPER CORNER AT FWD CARGO COMPRTMENT. SUMMARY OF NRC 00112: INNER PAN FWD/AFT UPPER CORNER AT FWD CARGO COMPARMENT WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0638113)SDR DALA2024061906217Battery · inoperativeEXIT SIGNS ABOVE LT & RT OVERWING FWD EXIT DOORS DO NOT ILLUMINATE. T/S PER B717 FIM 33-50-00-201. R&R B5-121 BATTERY ASSEMBLY PER B717 AMM 33-51-03. OPERATIONAL CHECK WAS GOOD. (LP #5891885)SDR DALA2024032303706Battery Pack · inoperativeTHE EMERGENCY OVERHEAD EXIT SIGN AT ROW 19 IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND POWER SUPPLY B5-120 REF B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE. (LP #5441945)SDR DALA2024011000450Unknown · unknownTHE CENTER AISLE OVERHEAD EMERGENCY EXIT LIGHT IS INOPERATIVE AT ROW 19. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY AT OVERHEAD BIN 8, ROW 17R IAW B717 AMM 33-51. LIGHT OPERATION CHECKS GOOD. (LP #5150194)SDR DALA2024011000449Unknown · unknownTHE EXIT MARKER AT THE AFT OVERWING EXIT AT STA 726L/726R IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK IN THE OVERHEAD BIN 10R, SEAT ROW 22R IAW B717 AMM 33-51. EXIT LIGHT OPERATIONALLY CHECKS GOOD. (LP #5150193)SDR DALA2023102608798Unknown · unknownSHIP 9548 -ATB/DE- THE FLIGHT WAS RETURNED TO ATL DUE TO THE LOSS OF THE PRIMARY STABILIZER TRIM. ON DEPARTURE CLIMB OUT, THE CAPT NOTICED THAT THERE WAS NOT ANY DOWN TRIM AVAILABLE. UP TRIM WORKED FINE. ALTERNATE TRIM WAS USED SUCCESSFULLY TO CORRECT PITCH DOSDR DALA2023101408453Unknown · unknownSHIP 9548 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC DUE TO A "STICK SHAKER PUSHER FAIL", FOLLOWED BY THE "SLAT DISAGREE" MESSAGE, AND AN AMBER X ON THE RIGHT WING CONFIG PAGE. CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE FLAP/SLAT HANDLE TRANSMSDR DALA2024022002332Seat Track · corrodedCORROSION IN I/B SEAT TRACK UNDER G-7 GALLEY- MARKED. REPAIRED SEAT TRACK REF B717-200 SRM 53-20-52-2R REPAIR 5. (LP #2967622)SDR DALA2023091407531Unknown · unknownCORROSION WAS FOUND AT FLOOR SUPPORT IN GALLEY. MARKED. SUMMARY SEE NRC 001-0010:2500-2647/095 00253: REPLACED FLOOR SUPPORT REF DAC DWG 9936534. (LP #2964169)SDR DALA2023060704645Unknown · unknownTHE EMERGENCY BATTERY PACK B5-120 DIES. MAINTENANCE REPLACED THE B5-120 EMERGENCY LIGHT BATTERY PACK PER B717 AMM 33-51. (LP #4688714)SDR DALA2023052204055Unknown · unknownTHE CABIN CREW NOTICED THAT THE EMERGENCY EXIT COVER DIFFUSER LENS WAS MISSING AT LOCATION 300. MAINTENANCE REPLACED THE MISSING EXIT COVER AT LOC 300. (LP #2778074)SDR DALA2023050903616Unknown · unknownEMERGENCY LIGHTING IS OUT AT 17C AND 18C. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY AT OVERHEAD BIN 18CDE (B5-120) AS PER B717 AMM 33-51. ALL CHECKS ARE NORMAL. (LP #9495086)SDR DALA2024071807235Skin · dentedDENT & 3/8" HOLE IN FLAP SKIN AFT OF LT MAIN LANDING GEAR. PER ERA 606778-14 REV ORIGINAL, SEC 1 ACCOMPLISHED DETAILED VISUAL INSPECTION, NO DAMAGE BEYOND PUNCTURE, NO LOOSE, MISSING, OR PULLED FASTNERS. COMPLIED WITH PERMANENT REPAIR OF FLAP OF ERA 606778-14 SDR DALA2023021401132Unknown · unknownREMOVED LT OUTER WING FIXED TRAILING EDGE REF ERA 604993-14 REV ORIG SECTION V. BLENDED DAMAGE AREA PER ERA 604993-14 REV A. PERFORMED HFEC OF CUTOUT PER STEP 5 OF ERA 604993-14 REV A SECTION 5. NO CRACK INDICATIONS NOTED. QC2013. FILLER & DOUBLER MADE, DRILLESDR DALA2022102706967None · noneTHE INTERIOR EMERGENCY LIGHTING FOR THE LEFT AND RIGHT AFT LOWER OVERWING EXITS ARE NOT WORKING. MAINTENANCE REPLACED THE BATTERY PACK FOR THE INTERIOR AFT LOWER OVERWING LIGHTS PER B717 AMM 33-51-06. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE. (LP #9192898)SDR DALA2022042102782Cover · missingTHE FORWARD EMERGENCY EXIT LIGHT COVER IS MISSING. THIS COULD PREVENT PROPER LOCATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE INSTALLED THE FORWARD EMERGENCY EXIT LIGHT COVER. THE AIRCRAFT IS OK FOR SERVICE. (LP #88SDR DALA2022041902667None · noneTHE INTERIOR EMERGENCY OVERWING LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #8828951)SDR DALA2021100506083None · noneCORROSION ON PAN BTW STA Y954 TO Y994 AT AFT CARGO COMPARTMENT JAMB. SUMMARY OF NRC 00158: CORROSION LEVEL 2. PAN BTW STA Y954 TO Y994 AT AFT CARGO COMPARTMENT JAMB WAS REPAIRED PER ER/A 594290-14 REV. ORIGINAL AND ETI-17-21-007 REV. ORIGINAL. ACCOMPLISH SECTISDR DALA2021092805821None · noneCRACKED CHANNEL AT LH MLG INBOARD DOOR INTERNAL SKIN, BETWEEN STA 790 TO 793. (PTAS). SUMMARY OF NRC 00266: FORWARD Z CHANNEL AT LH MLG DOOR WAS REPAIRED PER ER/A 594279-14 REV. ORIGINAL, SECTION I - PERMANENT REPAIR AND ETI-17-21-004 REV. 1 ASSOCIATED ER/A 14SDR DALA2021092805815None · noneCORROSION ON SPLICE ON AFT PRESSURE BULKHEAD STA 1053 BTW LONG 29LH-29RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00136: CORROSION LEVEL 2, SPLICE ON AFT PRESSURE BULKHEAD STA 1053 BTW LONG 29LH-29RH WAS REPLACED PER B717 SRM 53-20-08-0I, SRM 51-41-02-0G PAR 4SDR DALA2021092105636None · noneCORROSION ON JAMB BTW STA Y=370 TO Y=425 AT FWD CARGO COMPARTMENT JAMB AREA. SUMMARY OF NRC 00216: CORROSION LEVEL 2, SECTION OF JAMB BTW STA Y=370 TO Y=425 AT FWD CARGO COMPARTMENT WAS REPLACED PER B717 SRM 53-20-15-2R-6. (LP #1953156)SDR DALA2021091505495Web · corrodedCORROSION ON MEMBRANE BTW STA Y=190 TO STA Y=195 AND X=53 AT CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00191: CORROSION LEVEL 2. MEMBRANE BTW STA Y=190 TO STA Y=195 AND X=53 AT CABIN FLOOR STRUCTURE WAS REPAIRED PER B717-200 SRM 51-70-10-2R-2 AND SRM 53-00-55-1A-1SDR DALA2021091105376Cusp Web · crackedCRACK ON CUSP MEMBRANE STA Y=715 X=54 AT CPAX IN REF AMDS 5310-01436-01A. SUMMARY OF NRC 00174: CUSP MEMBRANE STA Y=715 X=54 AT CPAX WAS REPAIRED PER B717 SRM 53-00-55-2R-4 FIG. 212. (LP #1943839)SDR DALA2020081702804Battery Pack · inoperativeDURING SERVICE CHECK, THE EMERGENCY EXIT LIGHT AT ROW 19 EDC WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY B5-121 IAW B717 AMM 33-55. OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS RETURNED TO SERVICE.SDR DALA2020072302630Charger · inoperativeAFT CABIN OVERHEAD EMERGENCY EXIT SIGN INOPERATIVE. MAINTENCE REPLACED THE BATTERY CHARGER PER B717 AMM 33-51-03.SDR DALA2020060102432Battery Pack · dischargedTHE CENTER AISLE EMERGENCY ESCAPE LIGHTS AT ROW 15 - 18 AND THE EMERGENCY EXIT DOOR LIGHT ARE ALL INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK B5-120 IAW AMM 33-51-03. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE.SDR DALA2020021100067Panel · detachedGROUND AGENT FOUND A PANEL HAD FALLEN FROM AREA OF NUMBER 1 ENGINE. PANEL WAS HOT TO TOUCH. DETERMINED TO BE THE LEFT PACK FAN BYPASS CHECK VALVE FLAPPER DOOR. (LP #7215891)SDR DALA2019060903462Wire · pinchedON TAXI OUT WHEN CHECKING CONTROLS THE WHEEL BECAME STUCK FULL RIGHT. FOUND WIRING INTERNAL ON DUAL AILERON SERVO PINCHED AND WIRING EXSPOSED. DUAL AILERON SERVO WAS REPLACED PER B717 AMM 22-12. FAILED AILERON RTS TEST. REPLACED THE SERVO A SECOND TIME PER B71SDR DALA2017102407747Frame · crackedCRACK ON FRAME ANGLE BS 1022, LONGERON 7L. REPAIRED IAW ETI-17-17-187, REV 1, AND ER/A 562354-14.SDR DALA2017102407746Frame · crackedCRACK ON FRAME ANGLE BS 1022, LONGERON 7R. REPAIRED IAW ETI-17-17-187, REV 1, AND ER/A 562354-14.SDR DALA2017102407745Frame · crackedCRACK ON FRAME ANGLE BS 1022, LONGERON 6R. REPAIRED IAW ETI-17-17-187, REV 1, AND ER/A 562354-14.SDR DALA2017101907640Pin · out of positionOUT OF POSITION SAFETY PIN HOLE AND PIN AT L1 DOOR SLIDE. REPLACED THE SLIDE.SDR DALA2017101707577Skin · crackedSKIN BS 1076, BETWEEN LONGERONS 13 - 14R CRACKED. THE SKIN WAS REPAIRED IAW ETI 17-17-184, REV 1, AND ER/A 560957-14, REV ORIGINAL.SDR DALA2017101707573Frame Angle · corrodedCORROSION ON FRAME ANGLE BS 908, BETWEEN LONGERONS 25R TO 26L. THE FRAME ANGLE WAS REPLACED IAW SRM 51-41-02, AND DWG 9912243, REV JS.SDR DALA2017101707572Skin · crackedSKIN CRACKED BS 1022, LONGERON 14L. THE SKIN WAS REPAIRED IAW ER/A 590959-14, REV ORIGINAL, AND ETI-17-17-182, REV 1.SDR DALA2017101607504Frame Angle · crackedCRACK ON FRAME ANGLE, BS 1053 BETWEEN LONGERONS 17 - 18L. THE FRAME ANGLE WAS REPLACED IAW SRM 51-41-02, 51-41-05, AND DWG S2912293S, REV DL.SDR DALA2017101607524Skin · corrodedEXCESSIVE CORROSION ON THE FUSELAGE SKIN, UNDER FILLET FAIRINGS BETWEEN BS 849 - 856, LONGERONS 29R TO 28L. THE SKIN WAS REPAIRED IAW SRM 53-20-70-2R.SDR DALA2017101607522Longeron · crackedCRACKED LONGERON 7R, BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R.SDR DALA2017101507511Structure · corrodedAFTER A CORRODED NUT WAS REMOVED, CORROSION AND SCRATCHES AT BORES WERE FOUND. BORE OF BARREL NUT NR 27 WAS REPAIRED IAW ETI-17-17-190, REV 1, AND ER/A 562336-14, REV ORIGINAL.SDR DALA2017101407508Floorbeam · crackedCRACKED FLOORBEAM BS 737, LBL 54. THE FLOORBEAM WAS REPLACED IAW SRM 51-41-05, AND 51-41-02.SDR DALA2017101207450Intercostal · crackedCRACK ON THE INTERCOSTAL BETWEEN BS 617 - 636, BL 0 (CEILING AREA) IN THE FWD CARGO BAY. THE INTERCOSTAL WAS REPAIRED IAW SRM 53-00-00-2R-1, 51-41-02, AND 51-41-05.SDR DALA2017101207449Web · corrodedCORROSION ON THE WEB AT BS 201, LBL 54 OF THE L1 DOOR FRAME. THE WEB WAS REPLACED IAW SRM 51-41-01-0G, 51-41-02-0G, 51-41-05, 51-41-08, AND 53-10-15-01-2, FIG.1.SDR DALA2017101107421Floor Panel · crackedCRACK ON THE FLOOR PANEL 221SF. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-00-2R-1, FIG 201.SDR DALA2017101107412Frame · crackedCRACKED FRAME BS 1037, LONGERON 17R. THE FRAME WAS REPAIRED IAW SRM 53-20-07-2R, PRCEDURE 4. ET, HFEC ACCOMPLISHED IAW NDT SPM 06-10-01.001 NO CRACKS FOUND AFTER DAMAGED WAS REMOVED.SDR DALA2017101107419Floor Panel · crackedCRACK ON UPPER SURFACE OF FLOOR PANEL 222AQF. THE FLOOR PANEL WAS REPAIRED IAW SRM 51-41-02, AND SRM 53-00-00-2R-1, FIG 201.SDR DALA2017101007417Splice · crackedCRACKED SPLICE ON LEADING EDGE XRS 267, LT WING . THE SPLICE WAS REMOVED AND A NEW SPLICE WAS INSTALLED IAW SRM 57-40-01-01, FIG 1, SRM 51-41-02, AND SRM 51-41-05.SDR DALA2017101007416Beam · crackedCRACK ON THE RT DOOR FRAME BEAM BS 48 AT THE NLG WHEEL WELL. THE DAMAGE WAS REMOVED, HFEC INSPECTION WAS ACCOMPLISHED IAW NDT SPM 06-10-01.001. NO CRACKS WERE FOUND AFTER CUT OUT. REPAIRED IAW SRM 53-10-14, REPAIR 2.SDR DALA2017101007415Beam · crackedCRACK ON THE LT DOOR FRAME BEAM BS 48 AT THE NLG WHEEL WELL. THE DAMAGE WAS REMOVED, ET, HFEC INSPECTION WAS ACCOMPLISHED IAW NDT SPM 06-10-01.001. NO CRACKS WERE FOUND AFTER CUT OUT. REPAIRED IAW SRM 53-10-14, REPAIR 2.SDR DALA2017101007391Web · corrodedCORROSION AT FLOOR WEB BS 200 BETWEEN LBL 8 - RBL 8. THE WEB WAS REPAIRED IAW SRM 51-70-10-2R, FIG 2.SDR DALA2017100907376Support · corrodedCORROSION ON PANEL SUPPORT BS 148 RBL 54. THE SUPPORT WAS REPLACED IAW SRM 51-41-02, AND SRM 51-41-08.
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